command: 
 /usr/local/libexec/code_saturne/cs_solver --param s4_std_ke_2.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:                lun 22 giu 2015 15:45:15 CEST
  System:              Linux 3.19.0-22-generic
  Machine:             celsius
  Processor:           model name	: Intel(R) Xeon(R) CPU E3-1225 v3 @ 3.20GHz
  Memory:              15934 MB
  User:                claudio (claudio)
  Directory:           /home/claudio/Documents/Atos/DP4/1L5/06_CFD/DP4_1L5_PA_mod_p40_test/S4_STD_KE/RESU/20150622-1545
  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         )


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

    STEADY ALGORITHM

 --- Global parameters

       IDTVAR =             -1 (-1: steady algorithm        )
       RELXST =    0.90000E+00 (Reference relaxation coeff. )


 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per variable relaxation coefficient

-----------------------------
 Variable          RELAXV
-----------------------------
 Velocity          0.9000E+00
 Pressure          0.1000E+00
 k                 0.9000E+00
 epsilon           0.9000E+00
----------------------------

       RELAXV =  [0.,1.]       (relaxation coefficient      )


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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       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
total_pressure
         --           --

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

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

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 epsilon                        0
        10 TurbVisc                    -999
        13 total_pressure              -999
         --           --                --

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


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


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

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


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


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

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


 Reading file:        mesh_input

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

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


 Reading file:        mesh_input

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

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


 Reading file:        mesh_input

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

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


 Reading file:        mesh_input

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

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


 Reading file:        mesh_input

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

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


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

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition

 Extended neighborhood structures definition
 Number of cells:                                      281798

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

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


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

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

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

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

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

 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

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

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

  Histogram of the interior faces warping before unwarping algorithm:

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

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

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

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

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

  Histogram of the interior faces warping after unwarping algorithm:

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

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

 End unwarping algorithm


 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

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

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

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


 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

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

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

  Histogram of the interior faces warping before unwarping algorithm:

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

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

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

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

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

  Histogram of the interior faces warping after unwarping algorithm:

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

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

 End unwarping algorithm


 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

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

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

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


 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

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

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

  Histogram of the interior faces warping before unwarping algorithm:

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

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

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

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

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

  Histogram of the interior faces warping after unwarping algorithm:

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

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

 End unwarping algorithm


 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

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

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

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


 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

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

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

  Histogram of the interior faces warping before unwarping algorithm:

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

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

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

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

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

  Histogram of the interior faces warping after unwarping algorithm:

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

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

 End unwarping algorithm


 Renumbering mesh:

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

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

   renumbering for boundary faces:
     numbering:                           none

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

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

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

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

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

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

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

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

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

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

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

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

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

 Computing geometric quantities (2.48 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
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E+01   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.8800E+03  0.8800E+03
  molecular_viscos  0.3960E-01  0.3960E-01
  turbulent_viscos  0.5389E+00  0.5389E+00
 -----------------------------------------



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

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


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



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

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


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.71516E-05 0.46005E-02
   Dimensionless distance   yplus :  0.91255E-09 0.25844E+00
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :      41000
   Total number of wall faces                   :      41000
------------------------------------------------------------


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

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


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



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

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



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



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


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




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


 INSTANT    0.100000000E+01   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.8800E+03  0.8800E+03
  molecular_viscos  0.3960E-01  0.3960E-01
  turbulent_viscos  0.5389E+00  0.5389E+00
 -----------------------------------------



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

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


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



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet         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         0.442491722E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18815E+00 0.55279E+01
   Friction velocity        uet   :  0.13811E-02 0.93245E+00
   Friction velocity        uk    :  0.13881E-02 0.17076E+01
   Dimensionless distance   yplus :  0.95906E-05 0.89993E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        113
   Nb of faces within the viscous sub-layer     :      33911
   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     0.37508E+00     142   0.18027E+00   0.96899E+02 0.10907E+04 
c  Velocity[X]                                      0.20880E+02 
c  Velocity[Y]                                      0.30939E+02 
c  Velocity[Z]                                      0.45079E+02 
c  Pressure     0.49536E-01    1310   0.88035E-01   0.94278E+00 0.19654E+07 
c  k            0.34130E-01     146   0.57332E-01   0.83266E+01 0.11728E+05 
c  epsilon      0.56396E+03     147   0.46382E-01   0.65101E+10 0.20434E+05 
-----------------------------------------------------------------------------
  
  

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

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


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]           -0.67623          4.8336        0.086575        0.051009
v  Velocity[Y]            -3.5892          5.4625         0.13028         0.11791
v  Velocity[Z]            -6.1797          3.4419       -0.010724     -0.00088621
v  ǁVelocityǁ          5.4648e-07          7.4503         0.28681         0.91434
v  Pressure               -3141.7           12973            8766          7247.2
v  k                    6.167e-06          3.4342       0.0063851        0.015905
v  epsilon             5.2713e-05      1.8268e+05          55.955          38.773
v  TurbVisc            0.00015796         0.53888          0.3929          0.2888
v  total_pressure      4.9686e+05      5.1297e+05      5.0877e+05      5.0725e+05


 TIME FOR THE TIME STEP                2:        0.11249E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.256362199E-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 : -0.94142E+00 0.16942E+01
   Friction velocity        uet   :  0.16521E-02 0.10820E+01
   Friction velocity        uk    :  0.16520E-02 0.12450E+01
   Dimensionless distance   yplus :  0.82452E-05 0.73849E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        269
   Nb of faces within the viscous sub-layer     :      34790
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26124E+00     146   0.19837E+00   0.61474E+02 0.60206E+03 
c  Velocity[X]                                      0.14926E+02 
c  Velocity[Y]                                      0.24770E+02 
c  Velocity[Z]                                      0.21778E+02 
c  Pressure     0.53536E-01    1014   0.68667E-01   0.86170E+00 0.71224E+05 
c  k            0.27249E-01      72   0.56985E+00   0.27338E+01 0.14720E+05 
c  epsilon      0.16838E+04      57   0.81387E+00   0.19901E+10 0.60602E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -9.356e-05                             8
a  epsilon        -0.22203                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.2439          3.7049         0.11201        0.050931
v  Velocity[Y]             -3.231          6.4383         0.13414         0.11703
v  Velocity[Z]            -7.5088          5.2767         -0.0238     -7.3825e-05
v  ǁVelocityǁ          6.0691e-07          8.3246         0.35283         0.92045
v  Pressure               -6578.9           11640          7869.3          6507.1
v  k                   2.2624e-07         0.51935       0.0015352       0.0048532
v  epsilon             5.2798e-05           21282          7.3654          5.4364
v  TurbVisc             1.103e-08         0.53845         0.10002       0.0083377
v  total_pressure      4.9342e+05      5.1164e+05      5.0787e+05      5.0651e+05


 TIME FOR THE TIME STEP                3:        0.10251E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.486262485E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15662E+01 0.15670E+01
   Friction velocity        uet   :  0.41059E-02 0.11171E+01
   Friction velocity        uk    :  0.41056E-02 0.11819E+01
   Dimensionless distance   yplus :  0.86759E-05 0.71597E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        452
   Nb of faces within the viscous sub-layer     :      34883
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25603E+00     140   0.17032E+00   0.45626E+02 0.50735E+03 
c  Velocity[X]                                      0.12380E+02 
c  Velocity[Y]                                      0.18896E+02 
c  Velocity[Z]                                      0.14350E+02 
c  Pressure     0.49895E-01    1129   0.42177E-01   0.81953E+00 0.24951E+05 
c  k            0.97692E-02      79   0.16214E+00   0.49180E-01 0.22812E+04 
c  epsilon      0.22966E+03      37   0.57109E+00   0.20393E+08 0.26470E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -6.513e-06                            12
a  epsilon        -0.04773                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.6002          3.9216         0.12897        0.050431
v  Velocity[Y]             -3.622          6.1509         0.13843         0.11723
v  Velocity[Z]            -7.3511          6.5697        -0.03002     -0.00019389
v  ǁVelocityǁ          6.6531e-07           8.347         0.39888         0.92847
v  Pressure               -7635.7           11364          7644.2            6352
v  k                   9.2861e-08         0.26842      0.00085579       0.0033199
v  epsilon              5.291e-05          5134.5          1.7317          1.3741
v  TurbVisc            3.7393e-11         0.53738        0.079532       0.0066075
v  total_pressure      4.9236e+05      5.1136e+05      5.0764e+05      5.0635e+05


 TIME FOR THE TIME STEP                4:        0.10621E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.219228655E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491688E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15517E+01 0.16494E+01
   Friction velocity        uet   :  0.39987E-02 0.10990E+01
   Friction velocity        uk    :  0.39985E-02 0.12842E+01
   Dimensionless distance   yplus :  0.90877E-05 0.78750E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        583
   Nb of faces within the viscous sub-layer     :      34795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25870E+00     139   0.16511E+00   0.42120E+02 0.49982E+03 
c  Velocity[X]                                      0.13100E+02 
c  Velocity[Y]                                      0.15777E+02 
c  Velocity[Z]                                      0.13242E+02 
c  Pressure     0.51706E-01    1020   0.45776E-01   0.83711E+00 0.15255E+05 
c  k            0.85567E-02      78   0.25013E-01   0.65754E-02 0.87117E+03 
c  epsilon      0.11886E+03      50   0.10854E+00   0.99829E+06 0.70916E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3383e-05                            36
a  epsilon     -8.5128e-05                             1


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7066          4.0776         0.14349        0.050267
v  Velocity[Y]            -4.3734          6.0911         0.14134         0.11736
v  Velocity[Z]            -7.7147          7.6357       -0.033871      7.0148e-05
v  ǁVelocityǁ          6.6634e-07          8.6048         0.43562         0.93499
v  Pressure               -6970.4           11366          7602.2          6342.1
v  k                   4.0341e-09         0.47046      0.00093118       0.0035133
v  epsilon              5.291e-05           10597          1.7086          1.1243
v  TurbVisc            3.8914e-11         0.53523        0.065389       0.0060618
v  total_pressure      4.9303e+05      5.1137e+05       5.076e+05      5.0634e+05


 TIME FOR THE TIME STEP                5:        0.10048E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.974506644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491732E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15362E+01 0.13741E+01
   Friction velocity        uet   :  0.31657E-02 0.12570E+01
   Friction velocity        uk    :  0.31632E-02 0.12550E+01
   Dimensionless distance   yplus :  0.90935E-05 0.80894E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        588
   Nb of faces within the viscous sub-layer     :      34779
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26162E+00     138   0.16437E+00   0.35093E+02 0.45250E+03 
c  Velocity[X]                                      0.10829E+02 
c  Velocity[Y]                                      0.12965E+02 
c  Velocity[Z]                                      0.11299E+02 
c  Pressure     0.52116E-01     844   0.46604E-01   0.84779E+00 0.11994E+05 
c  k            0.81038E-02      78   0.27531E-01   0.64674E-02 0.80163E+03 
c  epsilon      0.54823E+02      66   0.14635E+00   0.83710E+06 0.74892E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.1515e-05                            39
a  epsilon       -0.019923                             7


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.5699          4.8497         0.15586        0.050115
v  Velocity[Y]             -3.959          5.7466         0.14223         0.11766
v  Velocity[Z]            -8.5692          7.9574       -0.037546      -0.0002833
v  ǁVelocityǁ          6.8121e-07          9.8823         0.46735         0.94178
v  Pressure               -6790.9           11379          7563.8          6338.6
v  k                   6.7528e-10         0.29754       0.0010914       0.0038532
v  epsilon             2.2467e-05          4705.6          2.0047          1.2456
v  TurbVisc            4.3471e-13         0.53157        0.054451       0.0058528
v  total_pressure      4.9321e+05      5.1138e+05      5.0756e+05      5.0634e+05


 TIME FOR THE TIME STEP                6:        0.89736E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.144494198E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491728E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16524E+01 0.13962E+01
   Friction velocity        uet   :  0.34650E-02 0.13682E+01
   Friction velocity        uk    :  0.34649E-02 0.13658E+01
   Dimensionless distance   yplus :  0.91855E-05 0.80691E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        591
   Nb of faces within the viscous sub-layer     :      34662
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26434E+00     136   0.16609E+00   0.27135E+02 0.39384E+03 
c  Velocity[X]                                      0.82997E+01 
c  Velocity[Y]                                      0.10126E+02 
c  Velocity[Z]                                      0.87094E+01 
c  Pressure     0.52504E-01     786   0.40822E-01   0.85272E+00 0.11802E+05 
c  k            0.82662E-02      79   0.85387E-02   0.51368E-02 0.79965E+03 
c  epsilon      0.53114E+02      67   0.26155E-01   0.75717E+06 0.80384E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.5489e-05                            44
a  epsilon       -0.023377                            16


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.3381          5.4676         0.16689        0.049986
v  Velocity[Y]            -4.2722          5.7518         0.14183         0.11795
v  Velocity[Z]            -8.9094          6.7023       -0.040759     -0.00036032
v  ǁVelocityǁ          6.8483e-07          9.9509         0.49542         0.94825
v  Pressure               -6765.7           11314          7468.5          6290.6
v  k                   2.7226e-11         0.44135       0.0012551       0.0040906
v  epsilon             4.3102e-06           11571          2.4889          1.3733
v  TurbVisc            2.2604e-14         0.52627        0.045956        0.005724
v  total_pressure      4.9323e+05      5.1131e+05      5.0747e+05      5.0629e+05


 TIME FOR THE TIME STEP                7:        0.78381E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.212105553E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491693E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17318E+01 0.15582E+01
   Friction velocity        uet   :  0.34363E-02 0.14683E+01
   Friction velocity        uk    :  0.34363E-02 0.14656E+01
   Dimensionless distance   yplus :  0.92025E-05 0.80376E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        615
   Nb of faces within the viscous sub-layer     :      34551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26605E+00     133   0.16330E+00   0.21596E+02 0.34797E+03 
c  Velocity[X]                                      0.66111E+01 
c  Velocity[Y]                                      0.84092E+01 
c  Velocity[Z]                                      0.65759E+01 
c  Pressure     0.47381E-01    1169   0.37916E-01   0.76004E+00 0.12775E+05 
c  k            0.84668E-02      77   0.69528E-02   0.46221E-02 0.96197E+03 
c  epsilon      0.57022E+02      54   0.21480E-01   0.10005E+07 0.12040E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.4527e-05                            44
a  epsilon       -0.018596                            17


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1105          6.7006         0.17706         0.04987
v  Velocity[Y]            -4.6689          5.6965         0.14008         0.11817
v  Velocity[Z]            -8.3599          7.2708       -0.043488     -0.00051816
v  ǁVelocityǁ          7.1288e-07          9.7484         0.52091         0.95412
v  Pressure               -7549.3           11151          7306.4          6186.9
v  k                   4.8009e-12         0.35865       0.0013896       0.0042419
v  epsilon             6.1801e-07           10832          2.9745          1.4676
v  TurbVisc             1.373e-15         0.51914        0.039231       0.0055981
v  total_pressure      4.9245e+05      5.1115e+05      5.0731e+05      5.0619e+05


 TIME FOR THE TIME STEP                8:        0.10455E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.966520172E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491688E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21149E+01 0.16045E+01
   Friction velocity        uet   :  0.37654E-02 0.15538E+01
   Friction velocity        uk    :  0.37653E-02 0.15512E+01
   Dimensionless distance   yplus :  0.93986E-05 0.80040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        636
   Nb of faces within the viscous sub-layer     :      34426
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26749E+00     131   0.16991E+00   0.17286E+02 0.31425E+03 
c  Velocity[X]                                      0.51599E+01 
c  Velocity[Y]                                      0.66906E+01 
c  Velocity[Z]                                      0.54356E+01 
c  Pressure     0.45628E-01     764   0.30457E-01   0.71604E+00 0.10599E+05 
c  k            0.86328E-02      76   0.60352E-02   0.43295E-02 0.92936E+03 
c  epsilon      0.60749E+02      52   0.16949E-01   0.13464E+07 0.11417E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.6272e-05                            30
a  epsilon       -0.046566                            19


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.6437          5.2336         0.18699        0.049771
v  Velocity[Y]            -4.6918           5.428          0.1376         0.11845
v  Velocity[Z]            -7.8424          7.3705       -0.045896     -0.00041362
v  ǁVelocityǁ          8.2028e-07          9.3517         0.54452         0.95897
v  Pressure               -8427.9           10939          7117.1          6055.6
v  k                   5.8378e-12           0.515       0.0015131       0.0043479
v  epsilon              7.045e-08           14933          3.4423          1.5442
v  TurbVisc            1.0571e-16         0.51021          0.0338        0.005472
v  total_pressure      4.9157e+05      5.1094e+05      5.0712e+05      5.0606e+05


 TIME FOR THE TIME STEP                9:        0.82168E+02

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.221531422E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491699E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13489E+01 0.16406E+01
   Friction velocity        uet   :  0.45890E-02 0.16209E+01
   Friction velocity        uk    :  0.45889E-02 0.16184E+01
   Dimensionless distance   yplus :  0.10113E-04 0.79541E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        668
   Nb of faces within the viscous sub-layer     :      34331
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26769E+00     130   0.16834E+00   0.14518E+02 0.29087E+03 
c  Velocity[X]                                      0.42632E+01 
c  Velocity[Y]                                      0.56014E+01 
c  Velocity[Z]                                      0.46538E+01 
c  Pressure     0.43762E-01     809   0.25715E-01   0.67943E+00 0.77097E+04 
c  k            0.87820E-02      78   0.57998E-02   0.52204E-02 0.91056E+03 
c  epsilon      0.65107E+02      65   0.21452E-01   0.10530E+07 0.88276E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.589e-06                            14
a  epsilon       -0.083864                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.7275           5.307         0.19689        0.049711
v  Velocity[Y]            -4.5358          5.2352         0.13482          0.1187
v  Velocity[Z]            -7.7646          7.2792       -0.048132      -0.0002965
v  ǁVelocityǁ          1.0206e-06          9.3605         0.56703         0.96309
v  Pressure               -9312.2           10756          6959.6          5944.4
v  k                   9.1615e-13         0.46118        0.001642       0.0044254
v  epsilon             8.3372e-09           10108          4.0279           1.629
v  TurbVisc            1.1201e-15         0.49956        0.029322       0.0053508
v  total_pressure      4.9069e+05      5.1076e+05      5.0696e+05      5.0594e+05


 TIME FOR THE TIME STEP               10:        0.76687E+02

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


 INSTANT    0.110000000E+02   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         0.413378383E-18
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 : -0.14614E+01 0.16725E+01
   Friction velocity        uet   :  0.29483E-02 0.16647E+01
   Friction velocity        uk    :  0.29716E-02 0.16623E+01
   Dimensionless distance   yplus :  0.11318E-04 0.78224E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        692
   Nb of faces within the viscous sub-layer     :      34233
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26777E+00     129   0.16636E+00   0.12123E+02 0.26719E+03 
c  Velocity[X]                                      0.34974E+01 
c  Velocity[Y]                                      0.45810E+01 
c  Velocity[Z]                                      0.40444E+01 
c  Pressure     0.42035E-01     952   0.22098E-01   0.64625E+00 0.47066E+04 
c  k            0.89286E-02      74   0.59584E-02   0.27746E-02 0.67134E+03 
c  epsilon      0.68124E+02      51   0.16935E-01   0.41011E+06 0.62500E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.351e-06                             9
a  epsilon       -0.036399                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.5253          5.1865         0.20652         0.04955
v  Velocity[Y]            -4.6612          5.0793         0.13219          0.1189
v  Velocity[Z]            -7.6198          7.1669       -0.050236     -0.00029096
v  ǁVelocityǁ          1.3128e-06          9.2082         0.58853         0.96675
v  Pressure                -10118           10616            6844          5860.8
v  k                   9.0512e-14         0.48863       0.0017278       0.0044829
v  epsilon             1.8751e-08           10827          4.3606          1.6729
v  TurbVisc            1.1228e-16         0.48732         0.02555       0.0052367
v  total_pressure      4.8988e+05      5.1062e+05      5.0684e+05      5.0586e+05


 TIME FOR THE TIME STEP               11:        0.73967E+02

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


 INSTANT    0.120000000E+02   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         0.127089205E-18
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 : -0.14525E+01 0.17552E+01
   Friction velocity        uet   :  0.55600E-02 0.16799E+01
   Friction velocity        uk    :  0.55592E-02 0.16778E+01
   Dimensionless distance   yplus :  0.12854E-04 0.76877E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        713
   Nb of faces within the viscous sub-layer     :      34140
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26737E+00     128   0.17090E+00   0.10303E+02 0.24817E+03 
c  Velocity[X]                                      0.28432E+01 
c  Velocity[Y]                                      0.38660E+01 
c  Velocity[Z]                                      0.35937E+01 
c  Pressure     0.39354E-01    1132   0.18511E-01   0.61034E+00 0.43394E+04 
c  k            0.90459E-02      74   0.49365E-02   0.28876E-02 0.79745E+03 
c  epsilon      0.69226E+02      59   0.89322E-02   0.11543E+07 0.16916E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1912e-05                             9
a  epsilon       -0.038418                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.5821          5.2494         0.21582        0.049552
v  Velocity[Y]            -4.4673          5.0551         0.12979         0.11903
v  Velocity[Z]            -7.7081          6.9602       -0.052145     -0.00035996
v  ǁVelocityǁ          1.6599e-06          9.0418         0.60889         0.96986
v  Pressure                -10787           10511          6754.2          5798.3
v  k                   4.1936e-14         0.50847       0.0018236       0.0045269
v  epsilon             6.5904e-09           29659          5.1678          1.7307
v  TurbVisc            1.0954e-17         0.47381        0.022377       0.0051333
v  total_pressure      4.8921e+05      5.1051e+05      5.0675e+05       5.058e+05


 TIME FOR THE TIME STEP               12:        0.95969E+02

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.933935009E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14386E+01 0.16919E+01
   Friction velocity        uet   :  0.28366E-02 0.16929E+01
   Friction velocity        uk    :  0.28366E-02 0.16909E+01
   Dimensionless distance   yplus :  0.14450E-04 0.76019E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        720
   Nb of faces within the viscous sub-layer     :      34044
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26712E+00     127   0.16868E+00   0.88094E+01 0.23084E+03 
c  Velocity[X]                                      0.24045E+01 
c  Velocity[Y]                                      0.33226E+01 
c  Velocity[Z]                                      0.30823E+01 
c  Pressure     0.36685E-01     906   0.16705E-01   0.57741E+00 0.35024E+04 
c  k            0.91554E-02      76   0.44945E-02   0.28045E-02 0.81261E+03 
c  epsilon      0.69563E+02      61   0.16843E-01   0.11495E+07 0.15087E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -9.037e-06                            10
a  epsilon       -0.023904                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.5956          5.2296         0.22467        0.049592
v  Velocity[Y]            -4.5687          4.9673         0.12778         0.11914
v  Velocity[Z]            -7.5193          6.8066       -0.054201     -0.00038367
v  ǁVelocityǁ          2.0436e-06          8.9013         0.62822         0.97254
v  Pressure                -11444           10418          6684.8          5743.7
v  k                   1.9897e-10         0.50699       0.0019005       0.0045588
v  epsilon             8.8936e-09           11639          5.1374          1.7754
v  TurbVisc            4.9216e-18          0.4593        0.019646       0.0050387
v  total_pressure      4.8856e+05      5.1042e+05      5.0668e+05      5.0574e+05


 TIME FOR THE TIME STEP               13:        0.89617E+02

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


 INSTANT    0.140000000E+02   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        -0.881943103E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13984E+01 0.18540E+01
   Friction velocity        uet   :  0.76529E-02 0.16935E+01
   Friction velocity        uk    :  0.76529E-02 0.16916E+01
   Dimensionless distance   yplus :  0.16017E-04 0.74593E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        727
   Nb of faces within the viscous sub-layer     :      33954
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26668E+00     126   0.16532E+00   0.76947E+01 0.21858E+03 
c  Velocity[X]                                      0.20584E+01 
c  Velocity[Y]                                      0.29441E+01 
c  Velocity[Z]                                      0.26922E+01 
c  Pressure     0.34367E-01     989   0.14868E-01   0.54610E+00 0.31991E+04 
c  k            0.92378E-02      73   0.46138E-02   0.25864E-02 0.66658E+03 
c  epsilon      0.71893E+02      54   0.83796E-02   0.53585E+06 0.85017E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.9012e-05                            10
a  epsilon       -0.043394                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.6408          5.2263          0.2332        0.049626
v  Velocity[Y]            -4.5464          4.8719         0.12622         0.11921
v  Velocity[Z]            -7.5508          6.6497       -0.056481     -0.00029837
v  ǁVelocityǁ          2.4417e-06          8.8522         0.64674         0.97485
v  Pressure                -11997           10371          6645.6          5714.9
v  k                   4.8035e-09         0.49899       0.0019719       0.0045821
v  epsilon             4.3295e-06           14851          5.5226          1.8117
v  TurbVisc            5.7972e-12         0.44423        0.017284       0.0049541
v  total_pressure        4.88e+05      5.1037e+05      5.0665e+05      5.0571e+05


 TIME FOR THE TIME STEP               14:        0.93325E+02

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


 INSTANT    0.150000000E+02   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.941286073E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491687E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14004E+01 0.19557E+01
   Friction velocity        uet   :  0.48569E-02 0.17037E+01
   Friction velocity        uk    :  0.48559E-02 0.16982E+01
   Dimensionless distance   yplus :  0.17479E-04 0.73395E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        722
   Nb of faces within the viscous sub-layer     :      33861
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26689E+00     125   0.16547E+00   0.67451E+01 0.20538E+03 
c  Velocity[X]                                      0.17776E+01 
c  Velocity[Y]                                      0.25825E+01 
c  Velocity[Z]                                      0.23850E+01 
c  Pressure     0.32855E-01     711   0.14632E-01   0.52647E+00 0.43987E+04 
c  k            0.93244E-02      73   0.45294E-02   0.27727E-02 0.74606E+03 
c  epsilon      0.73537E+02      52   0.11680E-01   0.64520E+06 0.78200E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.9198e-05                            12
a  epsilon       -0.054383                            15


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.7079          5.0964         0.24126        0.049594
v  Velocity[Y]            -4.5424          5.0652         0.12522         0.11929
v  Velocity[Z]            -7.3932          6.8376       -0.058891     -0.00022593
v  ǁVelocityǁ          2.7939e-06          8.6941         0.66428         0.97697
v  Pressure                -12327           10337          6623.5          5695.6
v  k                   1.5155e-08         0.50608       0.0020395       0.0045994
v  epsilon             7.1106e-06           16915          5.8824          1.8415
v  TurbVisc            3.0164e-12         0.42838        0.015261       0.0048784
v  total_pressure      4.8767e+05      5.1034e+05      5.0662e+05       5.057e+05


 TIME FOR THE TIME STEP               15:        0.79207E+02

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


 INSTANT    0.160000000E+02   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         0.102606892E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491700E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13196E+01 0.19934E+01
   Friction velocity        uet   :  0.58793E-02 0.17180E+01
   Friction velocity        uk    :  0.58774E-02 0.17149E+01
   Dimensionless distance   yplus :  0.18663E-04 0.72803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        724
   Nb of faces within the viscous sub-layer     :      33792
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26695E+00     125   0.16506E+00   0.59826E+01 0.19475E+03 
c  Velocity[X]                                      0.15827E+01 
c  Velocity[Y]                                      0.22342E+01 
c  Velocity[Z]                                      0.21657E+01 
c  Pressure     0.32077E-01     861   0.13638E-01   0.51485E+00 0.35829E+04 
c  k            0.93917E-02      73   0.40043E-02   0.20080E-02 0.57133E+03 
c  epsilon      0.75044E+02      57   0.81847E-02   0.40732E+06 0.77429E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -5.706e-06                             9
a  epsilon       -0.027646                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.7732          4.9675         0.24882        0.049425
v  Velocity[Y]            -4.6552          4.9697         0.12463         0.11926
v  Velocity[Z]            -7.3675          6.5889       -0.061579     -0.00021553
v  ǁVelocityǁ          3.1306e-06          8.6931         0.68126         0.97893
v  Pressure                -12647           10376            6610          5683.6
v  k                   1.3108e-08         0.50448       0.0020998       0.0046153
v  epsilon             8.2093e-06           21358          6.2072          1.8702
v  TurbVisc            1.7831e-12         0.41173        0.013525       0.0048118
v  total_pressure      4.8735e+05      5.1038e+05      5.0661e+05      5.0568e+05


 TIME FOR THE TIME STEP               16:        0.89621E+02

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


 INSTANT    0.170000000E+02   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         0.176035660E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491691E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13084E+01 0.20183E+01
   Friction velocity        uet   :  0.55663E-02 0.17263E+01
   Friction velocity        uk    :  0.55547E-02 0.17243E+01
   Dimensionless distance   yplus :  0.19716E-04 0.72436E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        729
   Nb of faces within the viscous sub-layer     :      33721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26765E+00     124   0.16691E+00   0.53985E+01 0.18579E+03 
c  Velocity[X]                                      0.14301E+01 
c  Velocity[Y]                                      0.20136E+01 
c  Velocity[Z]                                      0.19549E+01 
c  Pressure     0.32047E-01     700   0.12723E-01   0.51037E+00 0.30815E+04 
c  k            0.94492E-02      74   0.38017E-02   0.19920E-02 0.51119E+03 
c  epsilon      0.76155E+02      58   0.70600E-02   0.20189E+06 0.37823E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3493e-05                            10
a  epsilon       -0.067741                            13


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.8355            4.85         0.25589        0.049316
v  Velocity[Y]            -4.5628          5.0096         0.12435         0.11926
v  Velocity[Z]            -7.3045          6.8234       -0.064315     -0.00020823
v  ǁVelocityǁ          3.4157e-06          8.6093         0.69745         0.98092
v  Pressure                -12959           10467          6607.4          5680.7
v  k                   1.0559e-08          0.5089       0.0021609        0.004628
v  epsilon             3.0002e-06           21998           6.537          1.8981
v  TurbVisc            1.1956e-12         0.39479        0.012013       0.0047552
v  total_pressure      4.8704e+05      5.1047e+05      5.0661e+05      5.0568e+05


 TIME FOR THE TIME STEP               17:        0.78920E+02

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


 INSTANT    0.180000000E+02   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.264730113E-18
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 : -0.12633E+01 0.20483E+01
   Friction velocity        uet   :  0.69141E-02 0.17469E+01
   Friction velocity        uk    :  0.68986E-02 0.17352E+01
   Dimensionless distance   yplus :  0.20557E-04 0.72315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        729
   Nb of faces within the viscous sub-layer     :      33655
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26796E+00     123   0.16376E+00   0.50047E+01 0.18012E+03 
c  Velocity[X]                                      0.13096E+01 
c  Velocity[Y]                                      0.18121E+01 
c  Velocity[Z]                                      0.18830E+01 
c  Pressure     0.32049E-01     644   0.11863E-01   0.50786E+00 0.37067E+04 
c  k            0.95024E-02      72   0.43526E-02   0.26886E-02 0.63060E+03 
c  epsilon      0.76493E+02      53   0.92352E-02   0.35909E+06 0.47323E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5438e-05                            15
a  epsilon       -0.038008                            17


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.8946           4.825         0.26223        0.049219
v  Velocity[Y]            -4.4734          4.9354         0.12443          0.1192
v  Velocity[Z]            -7.2587          6.6299       -0.067208      -0.0002363
v  ǁVelocityǁ          3.6608e-06          8.5681         0.71265         0.98276
v  Pressure                -13190           10541          6609.9          5680.4
v  k                   8.9186e-09         0.51766        0.002218       0.0046429
v  epsilon             6.0608e-06           23234          6.8967          1.9281
v  TurbVisc            9.0412e-13         0.37733         0.01068       0.0047056
v  total_pressure      4.8681e+05      5.1054e+05      5.0661e+05      5.0568e+05


 TIME FOR THE TIME STEP               18:        0.79240E+02

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


 INSTANT    0.190000000E+02   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         0.170788270E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12327E+01 0.20730E+01
   Friction velocity        uet   :  0.52347E-02 0.17502E+01
   Friction velocity        uk    :  0.52226E-02 0.17464E+01
   Dimensionless distance   yplus :  0.21261E-04 0.72764E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        727
   Nb of faces within the viscous sub-layer     :      33572
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26893E+00     122   0.16197E+00   0.45648E+01 0.17112E+03 
c  Velocity[X]                                      0.12481E+01 
c  Velocity[Y]                                      0.16625E+01 
c  Velocity[Z]                                      0.16542E+01 
c  Pressure     0.31874E-01     678   0.11679E-01   0.50276E+00 0.41832E+04 
c  k            0.95677E-02      73   0.35068E-02   0.24024E-02 0.66479E+03 
c  epsilon      0.77628E+02      56   0.77813E-02   0.62424E+06 0.91606E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.1958e-05                            12
a  epsilon         -2.6518                            17


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.9403          4.7667         0.26786        0.049156
v  Velocity[Y]            -4.5852          5.0531         0.12486         0.11912
v  Velocity[Z]            -7.2215          6.3315       -0.070049     -0.00023613
v  ǁVelocityǁ          3.8595e-06          8.5033         0.72699         0.98469
v  Pressure                -13356           10631          6630.7            5694
v  k                   7.9263e-09         0.52313         0.00227        0.004657
v  epsilon             9.0642e-06           23708           7.238          1.9571
v  TurbVisc            7.5854e-13         0.35911       0.0094909       0.0046642
v  total_pressure      4.8664e+05      5.1063e+05      5.0663e+05      5.0569e+05


 TIME FOR THE TIME STEP               19:        0.83531E+02

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


 INSTANT    0.200000000E+02   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.438094427E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491699E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.20838E+01
   Friction velocity        uet   :  0.79796E-02 0.17916E+01
   Friction velocity        uk    :  0.79641E-02 0.17577E+01
   Dimensionless distance   yplus :  0.21815E-04 0.73443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        730
   Nb of faces within the viscous sub-layer     :      33480
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26946E+00     122   0.16420E+00   0.42438E+01 0.16495E+03 
c  Velocity[X]                                      0.11283E+01 
c  Velocity[Y]                                      0.15767E+01 
c  Velocity[Z]                                      0.15388E+01 
c  Pressure     0.32465E-01     758   0.11291E-01   0.50648E+00 0.33834E+04 
c  k            0.96120E-02      72   0.40791E-02   0.27974E-02 0.84605E+03 
c  epsilon      0.78620E+02      53   0.11422E-01   0.10993E+07 0.11600E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.0565e-05                            14
a  epsilon       -0.094738                            16


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -1.9893          4.8498          0.2728        0.049099
v  Velocity[Y]            -4.4613          5.0156         0.12558         0.11907
v  Velocity[Z]             -7.212          6.5223       -0.072678     -0.00018616
v  ǁVelocityǁ          4.0053e-06          8.5708         0.74047         0.98653
v  Pressure                -13446           10703          6656.2            5713
v  k                   7.3341e-09         0.55483       0.0023246       0.0046701
v  epsilon             3.2279e-06           23908          7.5021          1.9823
v  TurbVisc            6.8868e-13          0.3405        0.008411       0.0046277
v  total_pressure      4.8655e+05       5.107e+05      5.0666e+05      5.0571e+05


 TIME FOR THE TIME STEP               20:        0.63934E+02

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


 INSTANT    0.210000000E+02   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        -0.113112733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491697E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12024E+01 0.20887E+01
   Friction velocity        uet   :  0.66402E-02 0.18009E+01
   Friction velocity        uk    :  0.66234E-02 0.17714E+01
   Dimensionless distance   yplus :  0.22212E-04 0.74168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        734
   Nb of faces within the viscous sub-layer     :      33389
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27034E+00     121   0.16494E+00   0.39568E+01 0.15934E+03 
c  Velocity[X]                                      0.10634E+01 
c  Velocity[Y]                                      0.14559E+01 
c  Velocity[Z]                                      0.14376E+01 
c  Pressure     0.33365E-01     766   0.11376E-01   0.51512E+00 0.13816E+04 
c  k            0.96830E-02      72   0.35767E-02   0.17224E-02 0.45107E+03 
c  epsilon      0.79406E+02      55   0.60558E-02   0.13809E+06 0.27132E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.9703e-05                            13
a  epsilon         -2.4229                            16


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.0371          4.7265         0.27726        0.049057
v  Velocity[Y]            -4.2721           5.008         0.12647         0.11889
v  Velocity[Z]            -7.2765          6.2112       -0.075166     -0.00032463
v  ǁVelocityǁ          4.1039e-06          8.5043         0.75293         0.98833
v  Pressure                -13545           10738          6653.8          5712.4
v  k                   6.9939e-09         0.54467       0.0023729       0.0046853
v  epsilon              7.859e-06           23979          7.6596          2.0108
v  TurbVisc            6.6177e-13         0.31985       0.0074325       0.0045967
v  total_pressure      4.8646e+05      5.1074e+05      5.0665e+05      5.0571e+05


 TIME FOR THE TIME STEP               21:        0.62461E+02

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


 INSTANT    0.220000000E+02   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         0.125539138E-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 : -0.12483E+01 0.20943E+01
   Friction velocity        uet   :  0.76117E-02 0.17797E+01
   Friction velocity        uk    :  0.76111E-02 0.17503E+01
   Dimensionless distance   yplus :  0.22477E-04 0.75050E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        729
   Nb of faces within the viscous sub-layer     :      33308
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27104E+00     120   0.16243E+00   0.37374E+01 0.15348E+03 
c  Velocity[X]                                      0.10382E+01 
c  Velocity[Y]                                      0.13920E+01 
c  Velocity[Z]                                      0.13071E+01 
c  Pressure     0.32409E-01     747   0.11342E-01   0.50044E+00 0.60884E+03 
c  k            0.97228E-02      71   0.36270E-02   0.22631E-02 0.68611E+03 
c  epsilon      0.79806E+02      52   0.68227E-02   0.54117E+06 0.82536   Rel velocity at the wall uiptn : -0.12024E+01 0.20887E+01
   Friction velocity        uet   :  0.66402E-02 0.18009E+01
   Friction velocity        uk    :  0.66234E-02 0.17714E+01
   Dimensionless distance   yplus :  0.22212E-04 0.74168E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        734
   Nb of faces within the viscous sub-layer     :      33389
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27034E+00     121   0.16494E+00   0.39568E+01 0.15934E+03 
c  Velocity[X]                                      0.10634E+01 
c  Velocity[Y]                                      0.14559E+01 
c  Velocity[Z]                                      0.14376E+01 
c  Pressure     0.33365E-01     766   0.11376E-01   0.51512E+00 0.13816E+04 
c  k            0.96830E-02      72   0.35767E-02   0.17224E-02 0.45107E+03 
c  epsilon      0.79406E+02      55   0.60558E-02   0.13809E+06 0.27132E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.9703e-05                            13
a  epsilon         -2.4229                            16


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.0371          4.7265         0.27726        0.049057
v  Velocity[Y]            -4.2721           5.008         0.12647         0.11889
v  Velocity[Z]            -7.2765          6.2112       -0.075166     -0.00032463
v  ǁVelocityǁ          4.1039e-06          8.5043         0.75293         0.98833
v  Pressure                -13545           10738          6653.8          5712.4
v  k                   6.9939e-09         0.54467       0.0023729       0.0046853
v  epsilon              7.859e-06           23979          7.6596          2.0108
v  TurbVisc            6.6177e-13         0.31985       0.0074325     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12766E+01 0.20976E+01
   Friction velocity        uet   :  0.54443E-02 0.18314E+01
   Friction velocity        uk    :  0.54439E-02 0.17910E+01
   Dimensionless distance   yplus :  0.22786E-04 0.75828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        731
   Nb of faces within the viscous sub-layer     :      33228
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27187E+00     119   0.16655E+00   0.34427E+01 0.14707E+03 
c  Velocity[X]                                      0.97582E+00 
c  Velocity[Y]                                      0.12756E+01 
c  Velocity[Z]                                      0.11912E+01 
c  Pressure     0.32327E-01     655   0.11179E-01   0.49765E+00 0.14656E+04 
c  k            0.97774E-02      71   0.35053E-02   0.19868E-02 0.58626E+03 
c  epsilon      0.81213E+02      54   0.83491E-02   0.38259E+06 0.59625E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6287e-05                            11
a  epsilon        -0.99725                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1261          4.9689         0.28496        0.048896
v  Velocity[Y]            -4.3101          4.9834         0.12818         0.11868
v  Velocity[Z]            -7.3399          6.1037       -0.079639     -0.00034562
v  ǁVelocityǁ          4.2691e-06          8.6067         0.77499         0.99167
v  Pressure                -13643           10777            6660          5725.2
v  k                   6.7838e-09         0.57018       0.0024761       0.0047099
v  epsilon             9.3228e-06           24070          8.2911          2.0594
v  TurbVisc             2.596e-13         0.27481       0.0057231       0.0045418
v  total_pressure      4.8636e+05      5.1078e+05      5.0666e+05      5.0573e+05


 TIME FOR THE TIME STEP               23:        0.82735E+02

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


 INSTANT    0.240000000E+02   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         0.325743175E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491700E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12887E+01 0.21024E+01
   Friction velocity        uet   :  0.84898E-02 0.18564E+01
   Friction velocity        uk    :  0.85212E-02 0.18147E+01
   Dimensionless distance   yplus :  0.22949E-04 0.76517E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        730
   Nb of faces within the viscous sub-layer     :      33136
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27223E+00     119   0.16504E+00   0.33118E+01 0.14345E+03 
c  Velocity[X]                                      0.92797E+00 
c  Velocity[Y]                                      0.12261E+01 
c  Velocity[Z]                                      0.11578E+01 
c  Pressure     0.32088E-01     766   0.10------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12766E+01 0.20976E+01
   Friction velocity        uet   :  0.54443E-02 0.18314E+01
   Friction velocity        uk    :  0.54439E-02 0.17910E+01
   Dimensionless distance   yplus :  0.22786E-04 0.75828E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        731
   Nb of faces within the viscous sub-layer     :      33228
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27187E+00     119   0.16655E+00   0.34427E+01 0.14707E+03 
c  Velocity[X]                                      0.97582E+00 
c  Velocity[Y]                                      0.12756E+01 
c  Velocity[Z]                                      0.11912E+01 
c  Pressure     0.32327E-01     655   0.11179E-01   0.49765E+00 0.14656E+04 
c  k            0.97774E-02      71   0.35053E-02   0.19868E-02 0.58626E+03 
c  epsilon      0.81213E+02      54   0.83491E-02   0.38259E+06 0.59625E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6287e-05                            11
a  epsilon        -0.99725                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1261          4.9689         0.28496        0.048896
v  Velocity[Y]            -4.3101          4.9834         0.12818         0.11868
v  Velocity[Z]            -7.3399          6.1037       -0.079639     -0.00034562
v  ǁVelocityǁ          4.2691e-06          8.6067         0.77499         0.99167
v  Pressure                -13643           10777            6660          5725.2
v  k                   6.7838e-09         0.57018       0.0024761       0.0047099
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12854E+01 0.21021E+01
   Friction velocity        uet   :  0.74844E-02 0.18639E+01
   Friction velocity        uk    :  0.74787E-02 0.18214E+01
   Dimensionless distance   yplus :  0.23255E-04 0.77166E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        729
   Nb of faces within the viscous sub-layer     :      33075
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27300E+00     119   0.16253E+00   0.31104E+01 0.13740E+03 
c  Velocity[X]                                      0.86237E+00 
c  Velocity[Y]                                      0.11738E+01 
c  Velocity[Z]                                      0.10742E+01 
c  Pressure     0.32019E-01     789   0.11266E-01   0.49228E+00 0.24419E+04 
c  k            0.98453E-02      69   0.31890E-02   0.15919E-02 0.60878E+03 
c  epsilon      0.81758E+02      50   0.77798E-02   0.56456E+06 0.72760E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6183e-05                            11
a  epsilon         -1.9923                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1829          4.7315         0.29132        0.048827
v  Velocity[Y]            -4.1194          4.8882          0.1298         0.11849
v  Velocity[Z]            -7.4069          6.0421       -0.083647     -0.00034562
v  ǁVelocityǁ           4.447e-06          8.6365         0.79311         0.99453
v  Pressure                -13877           10793            6651          5728.3
v  k                   9.2928e-10         0.57541        0.002562       0.0047289
v  epsilon             5.8572e-06           24173          8.8751          2.0944
v  TurbVisc            4.0689e-14         0.22661       0.0043248       0.0045011
v  total_pressure      4.8612e+05      5.1079e+05      5.0665e+05      5.0573e+05


 TIME FOR THE TIME STEP               25:        0.83537E+02

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


 INSTANT    0.260000000E+02   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        -0.141078929E-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 : -0.13335E+01 0.20991E+01
   Friction velocity        uet   :  0.56252E-02 0.18817E+01
   Friction velocity        uk    :  0.56220E-02 0.18382E+01
   Dimensionless distance   yplus :  0.23469E-04 0.77548E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        735
   Nb of faces within the viscous sub-layer     :      33021
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27358E+00     118   0.16363E+00   0.28759E+01 0.13164E+03 
c  Velocity[X]                                      0.81782E+00 
c  Velocity[Y]      ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12854E+01 0.21021E+01
   Friction velocity        uet   :  0.74844E-02 0.18639E+01
   Friction velocity        uk    :  0.74787E-02 0.18214E+01
   Dimensionless distance   yplus :  0.23255E-04 0.77166E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        729
   Nb of faces within the viscous sub-layer     :      33075
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27300E+00     119   0.16253E+00   0.31104E+01 0.13740E+03 
c  Velocity[X]                                      0.86237E+00 
c  Velocity[Y]                                      0.11738E+01 
c  Velocity[Z]                                      0.10742E+01 
c  Pressure     0.32019E-01     789   0.11266E-01   0.49228E+00 0.24419E+04 
c  k            0.98453E-02      69   0.31890E-02   0.15919E-02 0.60878E+03 
c  epsilon      0.81758E+02      50   0.77798E-02   0.56456E+06 0.72760E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6183e-05                            11
a  epsilon         -1.9923                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.1829          4.7315         0.29132        0.048827
v  Velocity[Y]            -4.1194          4.8882          0.1298         0.11849
v  Velocity[Z]            -7.4069          6.0421       -0.083647     -0.00034562
v  ǁVelocityǁ           4.447e-06          8.6365     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13585E+01 0.20972E+01
   Friction velocity        uet   :  0.58861E-02 0.18792E+01
   Friction velocity        uk    :  0.58816E-02 0.18358E+01
   Dimensionless distance   yplus :  0.23976E-04 0.77736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        735
   Nb of faces within the viscous sub-layer     :      32960
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27404E+00     118   0.16455E+00   0.28146E+01 0.12889E+03 
c  Velocity[X]                                      0.77045E+00 
c  Velocity[Y]                                      0.10432E+01 
c  Velocity[Z]                                      0.10010E+01 
c  Pressure     0.31106E-01     700   0.10573E-01   0.47761E+00 0.22103E+04 
c  k            0.98987E-02      68   0.26985E-02   0.13595E-02 0.62453E+03 
c  epsilon      0.83004E+02      48   0.58250E-02   0.67103E+06 0.81590E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00061693                            15
a  epsilon         -1.6128                            13


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.2324          4.8383         0.29642        0.048841
v  Velocity[Y]            -4.0516          4.8541         0.13149         0.11831
v  Velocity[Z]            -7.3856          6.7065       -0.087406     -0.00043124
v  ǁVelocityǁ           4.792e-06          8.6999         0.80789         0.99686
v  Pressure                -14030           10769          6623.4          5715.4
v  k                   8.2881e-09         0.57012       0.0026357       0.0047441
v  epsilon             1.2819e-05           24024          9.2998          2.1246
v  TurbVisc            8.7858e-14         0.19525       0.0032298       0.0044729
v  total_pressure      4.8597e+05      5.1077e+05      5.0662e+05      5.0572e+05


 TIME FOR THE TIME STEP               27:        0.79752E+02

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


 INSTANT    0.280000000E+02   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        -0.660802944E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491695E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13190E+01 0.20946E+01
   Friction velocity        uet   :  0.70757E-02 0.18944E+01
   Friction velocity        uk    :  0.70618E-02 0.18502E+01
   Dimensionless distance   yplus :  0.24430E-04 0.77705E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        730
   Nb of faces within the viscous sub-layer     :      32923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13585E+01 0.20972E+01
   Friction velocity        uet   :  0.58861E-02 0.18792E+01
   Friction velocity        uk    :  0.58816E-02 0.18358E+01
   Dimensionless distance   yplus :  0.23976E-04 0.77736E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        735
   Nb of faces within the viscous sub-layer     :      32960
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27404E+00     118   0.16455E+00   0.28146E+01 0.12889E+03 
c  Velocity[X]                                      0.77045E+00 
c  Velocity[Y]                                      0.10432E+01 
c  Velocity[Z]                                      0.10010E+01 
c  Pressure     0.31106E-01     700   0.10573E-01   0.47761E+00 0.22103E+04 
c  k            0.98987E-02      68   0.26985E-02   0.13595E-02 0.62453E+03 
c  epsilon      0.83004E+02      48   0.58250E-02   0.67103E+06 0.81590E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00061693                            15
a  epsilon         -1.6128                            13


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.2324          4.8383         0.29642        0.048841
v  Velocity[Y]            -4Symmetry                  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 : -0.12696E+01 0.20905E+01
   Friction velocity        uet   :  0.53357E-02 0.18903E+01
   Friction velocity        uk    :  0.53319E-02 0.18463E+01
   Dimensionless distance   yplus :  0.25098E-04 0.77375E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        728
   Nb of faces within the viscous sub-layer     :      32886
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27431E+00     116   0.16223E+00   0.24425E+01 0.11856E+03 
c  Velocity[X]                                      0.69122E+00 
c  Velocity[Y]                                      0.92869E+00 
c  Velocity[Z]                                      0.82255E+00 
c  Pressure     0.30263E-01     710   0.10314E-01   0.46566E+00 0.25200E+04 
c  k            0.99295E-02      67   0.30301E-02   0.12508E-02 0.47669E+03 
c  epsilon      0.83670E+02      45   0.48874E-02   0.19714E+06 0.28635E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7808e-05                            16
a  epsilon         -1.4031                            15


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.2889          4.6959         0.30043        0.048792
v  Velocity[Y]            -4.0462          4.8752         0.13309         0.11827
v  Velocity[Z]            -7.4337          6.7734       -0.090987     -0.00045528
v  ǁVelocityǁ          5.2555e-06           8.663         0.81964         0.99856
v  Pressure                -14137           10752          6592.2          5700.1
v  k                   1.0623e-08         0.57212       0.0026927       0.0047506
v  epsilon             1.6333e-05           23864           9.645          2.1455
v  TurbVisc            8.6119e-14          0.1647        0.002406       0.0044471
v  total_pressure      4.8586e+05      5.1075e+05      5.0659e+05       5.057e+05


 TIME FOR THE TIME STEP               29:        0.74787E+02

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


 INSTANT    0.300000000E+02   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.981802470E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13536E+01 0.20900E+01
   Friction velocity        uet   :  0.59224E-02 0.18986E+01
   Friction velocity        uk    :  0.59169E-02 0.18540E+01
   Dimensionless distance   yplus :  0.25663E-04 0.77315E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        723
   Nb of faces within the viscous sub-layer     :      32858
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------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 : -0.12696E+01 0.20905E+01
   Friction velocity        uet   :  0.53357E-02 0.18903E+01
   Friction velocity        uk    :  0.53319E-02 0.18463E+01
   Dimensionless distance   yplus :  0.25098E-04 0.77375E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        728
   Nb of faces within the viscous sub-layer     :      32886
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27431E+00     116   0.16223E+00   0.24425E+01 0.11856E+03 
c  Velocity[X]                                      0.69122E+00 
c  Velocity[Y]                                      0.92869E+00 
c  Velocity[Z]                                      0.82255E+00 
c  Pressure     0.30263E-01     710   0.10314E-01   0.46566E+00 0.25200E+04 
c  k            0.99295E-02      67   0.30301E-02   0.12508E-02 0.47669E+03 
c  epsilon      0.83670E+02      45   0.48874E-02   0.19714E+06 0.28635E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7808e-05                            16
a  epsilon         -1.4031                            15


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

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.613560595E-18
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 : -0.12600E+01 0.20815E+01
   Friction velocity        uet   :  0.53971E-02 0.18877E+01
   Friction velocity        uk    :  0.53886E-02 0.18436E+01
   Dimensionless distance   yplus :  0.26265E-04 0.77026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        714
   Nb of faces within the viscous sub-layer     :      32824
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27451E+00     115   0.16240E+00   0.22233E+01 0.11188E+03 
c  Velocity[X]                                      0.63077E+00 
c  Velocity[Y]                                      0.77627E+00 
c  Velocity[Z]                                      0.81626E+00 
c  Pressure     0.29986E-01     894   0.90141E-02   0.45842E+00 0.13449E+04 
c  k            0.99758E-02      65   0.27761E-02   0.16153E-02 0.64057E+03 
c  epsilon      0.85125E+02      44   0.70667E-02   0.53205E+06 0.61321E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.3693e-05                            12
a  epsilon         -1.2346                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.3183          4.7339         0.30327         0.04879
v  Velocity[Y]            -3.9561          4.7598         0.13438         0.11831
v  Velocity[Z]            -7.3668          6.1964       -0.094283     -0.00049817
v  ǁVelocityǁ          5.6839e-06          8.6096         0.82878         0.99988
v  Pressure                -14232           10729          6569.2          5685.4
v  k                   1.4257e-08         0.57524       0.0027481       0.0047552
v  epsilon              2.319e-05           23623          10.172          2.1682
v  TurbVisc            1.0239e-13         0.13507       0.0018144       0.0044317
v  total_pressure      4.8577e+05      5.1073e+05      5.0657e+05      5.0569e+05


 TIME FOR THE TIME STEP               31:        0.94306E+02

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


 INSTANT    0.320000000E+02   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        -0.133808819E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13104E+01 0.20818E+01
   Friction velocity        uet   :  0.50465E-02 0.18935E+01
   Friction velocity        uk    :  0.50423E-02 0.18490E+01
   Dimensionless distance   yplus :  0.26768E-04 0.76748E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        711
   Nb of faces within the viscous sub-layer     :      32794
   Total nuInlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.613560595E-18
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 : -0.12600E+01 0.20815E+01
   Friction velocity        uet   :  0.53971E-02 0.18877E+01
   Friction velocity        uk    :  0.53886E-02 0.18436E+01
   Dimensionless distance   yplus :  0.26265E-04 0.77026E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        714
   Nb of faces within the viscous sub-layer     :      32824
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27451E+00     115   0.16240E+00   0.22233E+01 0.11188E+03 
c  Velocity[X]                                      0.63077E+00 
c  Velocity[Y]                                      0.77627E+00 
c  Velocity[Z]                                      0.81626E+00 
c  Pressure     0.29986E-01     894   0.90141E-02   0.45842E+00 0.13449E+04 
c  k            0.99758E-02      65   0.27761E-02   0.16153E-02 0.64057E+03 
c  epsilon      0.85125E+02      44   0.70667E-02   0.53205E+06 0.61321E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.3693e-05                            12
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.134670285E-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 : -0.13273E+01 0.20778E+01
   Friction velocity        uet   :  0.55699E-02 0.18895E+01
   Friction velocity        uk    :  0.55664E-02 0.18450E+01
   Dimensionless distance   yplus :  0.27318E-04 0.76563E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32792
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27474E+00     114   0.16033E+00   0.20327E+01 0.10704E+03 
c  Velocity[X]                                      0.57490E+00 
c  Velocity[Y]                                      0.69785E+00 
c  Velocity[Z]                                      0.75990E+00 
c  Pressure     0.28427E-01     713   0.78413E-02   0.43530E+00 0.13732E+04 
c  k            0.99884E-02      64   0.32603E-02   0.97907E-03 0.34245E+03 
c  epsilon      0.85338E+02      41   0.62820E-02   0.95766E+05 0.16476E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.5753e-05                            12
a  epsilon         -1.4982                            18


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.354          4.6513         0.30524        0.048773
v  Velocity[Y]            -4.0066          4.9002         0.13512         0.11833
v  Velocity[Z]             -7.358           6.196       -0.097276     -0.00048228
v  ǁVelocityǁ          6.0188e-06          8.5893         0.83591          1.0009
v  Pressure                -14325           10739          6562.3          5681.7
v  k                   1.8915e-08         0.59495       0.0027682       0.0047559
v  epsilon             3.3002e-05           23581           10.31          2.1745
v  TurbVisc            1.2967e-13         0.11253       0.0013984       0.0044202
v  total_pressure      4.8567e+05      5.1074e+05      5.0656e+05      5.0568e+05


 TIME FOR THE TIME STEP               33:        0.79721E+02

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


 INSTANT    0.340000000E+02   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        -0.149340621E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491692E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13055E+01 0.20743E+01
   Friction velocity        uet   :  0.56306E-02 0.18934E+01
   Friction velocity        uk    :  0.56269E-02 0.18488E+01
   Dimensionless distance   yplus :  0.27622E-04 0.76428E+01
   ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.134670285E-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 : -0.13273E+01 0.20778E+01
   Friction velocity        uet   :  0.55699E-02 0.18895E+01
   Friction velocity        uk    :  0.55664E-02 0.18450E+01
   Dimensionless distance   yplus :  0.27318E-04 0.76563E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32792
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27474E+00     114   0.16033E+00   0.20327E+01 0.10704E+03 
c  Velocity[X]                                      0.57490E+00 
c  Velocity[Y]                                      0.69785E+00 
c  Velocity[Z]                                      0.75990E+00 
c  Pressure     0.28427E-01     713   0.78413E-02   0.43530E+00 0.13732E+04 
c  k            0.99884E-02      64   0.32603E-02   0.97907E-03 0.34245E+03 
c  epsilon      0.85338E+02      41   0.62820E-02   0.95766E+05 0.16476E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.121816918E-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 : -0.12204E+01 0.20709E+01
   Friction velocity        uet   :  0.21404E-02 0.18870E+01
   Friction velocity        uk    :  0.21506E-02 0.18427E+01
   Dimensionless distance   yplus :  0.28057E-04 0.76374E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        697
   Nb of faces within the viscous sub-layer     :      32797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27509E+00     113   0.16006E+00   0.18635E+01 0.10173E+03 
c  Velocity[X]                                      0.51406E+00 
c  Velocity[Y]                                      0.66561E+00 
c  Velocity[Z]                                      0.68385E+00 
c  Pressure     0.26750E-01     698   0.64602E-02   0.41208E+00 0.85611E+03 
c  k            0.10015E-01      63   0.28255E-02   0.92533E-03 0.34964E+03 
c  epsilon      0.86167E+02      43   0.45507E-02   0.89354E+05 0.17403E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -5.228e-05                            11
a  epsilon         -1.4761                            18


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.3635          4.7095         0.30648        0.048747
v  Velocity[Y]            -4.0326          4.8646         0.13534         0.11837
v  Velocity[Z]            -7.3617          6.6437       -0.099876     -0.00041756
v  ǁVelocityǁ          6.3131e-06          8.6139         0.84166          1.0017
v  Pressure                -14354           10729          6560.1          5680.8
v  k                   2.3989e-08         0.58652       0.0027879       0.0047541
v  epsilon             4.3703e-05           23399          10.506          2.1827
v  TurbVisc            1.6126e-13         0.11253       0.0011071       0.0044119
v  total_pressure      4.8565e+05      5.1073e+05      5.0656e+05      5.0568e+05


 TIME FOR THE TIME STEP               35:        0.80925E+02

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


 INSTANT    0.360000000E+02   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        -0.817406723E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491690E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+01 0.20748E+01
   Friction velocity        uet   :  0.4149 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.121816918E-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 : -0.12204E+01 0.20709E+01
   Friction velocity        uet   :  0.21404E-02 0.18870E+01
   Friction velocity        uk    :  0.21506E-02 0.18427E+01
   Dimensionless distance   yplus :  0.28057E-04 0.76374E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        697
   Nb of faces within the viscous sub-layer     :      32797
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27509E+00     113   0.16006E+00   0.18635E+01 0.10173E+03 
c  Velocity[X]                                      0.51406E+00 
c  Velocity[Y]                                      0.66561E+00 
c  Velocity[Z]                                      0.68385E+00 
c  Pressure     0.26750E-01     698   0.64602E-02   0.41208E+00 0.85611E+03 
c  k            0.10015E-01      63   0.28255E-02   0.92533E-03 0.34964E+03 
c  epsilon      0.86167E+02      43   0.45507E-02   0.89354E+05 0.17403E+04 
----------------------------------- TIME FOR THE TIME STEP               36:        0.74587E+02

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


 INSTANT    0.370000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.367130302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12832E+01 0.20733E+01
   Friction velocity        uet   :  0.57636E-02 0.18911E+01
   Friction velocity        uk    :  0.57572E-02 0.18467E+01
   Dimensionless distance   yplus :  0.28676E-04 0.76317E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        700
   Nb of faces within the viscous sub-layer     :      32795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27546E+00     113   0.15958E+00   0.18121E+01 0.99195E+02 
c  Velocity[X]                                      0.52332E+00 
c  Velocity[Y]                                      0.62119E+00 
c  Velocity[Z]                                      0.66756E+00 
c  Pressure     0.25168E-01     587   0.61237E-02   0.39002E+00 0.97009E+03 
c  k            0.10036E-01      64   0.25688E-02   0.10380E-02 0.40315E+03 
c  epsilon      0.86766E+02      47   0.46170E-02   0.13638E+06 0.21905E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.2735e-05                            11
a  epsilon        -0.81707                            21


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.3851          4.6042         0.30735        0.048683
v  Velocity[Y]             -4.005           4.875         0.13525         0.11838
v  Velocity[Z]            -7.3099          6.7535        -0.10227     -0.00043816
v  ǁVelocityǁ          6.5505e-06          8.5005         0.84647          1.0025
v  Pressure                -14374           10697          6538.1          5666.5
v  k                   2.8782e-08         0.58518       0.0028036       0.0047514
v  epsilon             1.5162e-05           23461          10.656          2.1901
v  TurbVisc             1.914e-13         0.11253      0.00090199       0.0044053
v  total_pressure      4.8563e+05       5.107e+05      5.0654e+05      5.0567e+05


 TIME FOR THE TIME STEP               37:        0.72466E+02

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


 INSTANT    0.380000000E+02   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         0.677122857E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491697E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                    TIME FOR THE TIME STEP               36:        0.83929E+02

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


 INSTANT    0.370000000E+02   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.367130302E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12832E+01 0.20733E+01
   Friction velocity        uet   :  0.57636E-02 0.18911E+01
   Friction velocity        uk    :  0.57572E-02 0.18467E+01
   Dimensionless distance   yplus :  0.28676E-04 0.76317E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        700
   Nb of faces within the viscous sub-layer     :      32795
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27546E+00     113   0.15958E+00   0.18121E+01 0.99195E+02 
c  Velocity[X]                                      0.52332E+00 
c  Velocity[Y]                                      0.62119E+00 
c  Velocity[Z]                                      0.66756E+00 
c  Pressure     0.25168E-01     587   0.61237E-02   0.39002E+00 0.97009E+03 
c  k            0.10036v  TurbVisc            2.0457e-13         0.11253      0.00082398       0.0044024
v  total_pressure       4.856e+05      5.1068e+05      5.0653e+05      5.0566e+05


 TIME FOR THE TIME STEP               38:        0.69840E+02

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


 INSTANT    0.390000000E+02   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         0.398631689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491692E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12231E+01 0.20743E+01
   Friction velocity        uet   :  0.56774E-02 0.18900E+01
   Friction velocity        uk    :  0.56740E-02 0.18454E+01
   Dimensionless distance   yplus :  0.29254E-04 0.75910E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        696
   Nb of faces within the viscous sub-layer     :      32800
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27540E+00     112   0.15885E+00   0.17906E+01 0.99366E+02 
c  Velocity[X]                                      0.51602E+00 
c  Velocity[Y]                                      0.59518E+00 
c  Velocity[Z]                                      0.67937E+00 
c  Pressure     0.24295E-01     655   0.55691E-02   0.37834E+00 0.13582E+04 
c  k            0.10061E-01      62   0.24512E-02   0.58504E-03 0.24473E+03 
c  epsilon      0.87351E+02      48   0.36172E-02   0.38872E+05 0.10533E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1351e-05                            14
a  epsilon         -1.1636                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4077          4.7472         0.30798        0.048591
v  Velocity[Y]            -3.9391          4.7652         0.13517         0.11835
v  Velocity[Z]            -7.2676          6.2382        -0.10434     -0.00044183
v  ǁVelocityǁ          6.7771e-06          8.5873         0.85056          1.0029
v  Pressure                -14451           10672          6511.5          5650.1
v  k                   1.1364e-09         0.58316       0.0028158       0.0047496
v  epsilon             6.3596e-05           23462           10.76          2.1951
v  TurbVisc            2.1617e-13         0.11253      0.00075919       0.0044002
v  total_pressure      4.8555e+05      5.1067e+05      5.0651e+05      5.0565e+05


 TIME FOR THE TIME STEP               39:        0.80052E+02

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


 INSTANT    0.400000000E+02   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        -0.122699734E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY Cv  TurbVisc            2.0457e-13         0.11253      0.00082398       0.0044024
v  total_pressure       4.856e+05      5.1068e+05      5.0653e+05      5.0566e+05


 TIME FOR THE TIME STEP               38:        0.77937E+02

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


 INSTANT    0.390000000E+02   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         0.398631689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491692E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12231E+01 0.20743E+01
   Friction velocity        uet   :  0.56774E-02 0.18900E+01
   Friction velocity        uk    :  0.56740E-02 0.18454E+01
   Dimensionless distance   yplus :  0.29254E-04 0.75910E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        696
   Nb of faces within the viscous sub-layer     :      32800
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27540E+00     112   0.15885E+00   0.17906E+01 0.99366E+02 
c  Velocity[X]                                      0.51602E+00 
c  Velocity[Y]                                      0.59518E+00 
cv  k                   9.1513e-09         0.58702       0.0028244       0.0047493
v  epsilon             6.8398e-05           23690          10.835          2.1979
v  TurbVisc            9.7899e-14         0.11253      0.00070522       0.0043984
v  total_pressure      4.8551e+05      5.1068e+05      5.0652e+05      5.0566e+05


 TIME FOR THE TIME STEP               40:        0.80192E+02

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


 INSTANT    0.410000000E+02   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        -0.100939383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491723E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13369E+01 0.20811E+01
   Friction velocity        uet   :  0.65159E-02 0.18916E+01
   Friction velocity        uk    :  0.65103E-02 0.18472E+01
   Dimensionless distance   yplus :  0.29800E-04 0.75345E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        692
   Nb of faces within the viscous sub-layer     :      32781
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27528E+00     112   0.15586E+00   0.17015E+01 0.96212E+02 
c  Velocity[X]                                      0.49166E+00 
c  Velocity[Y]                                      0.56165E+00 
c  Velocity[Z]                                      0.64816E+00 
c  Pressure     0.23299E-01     785   0.56674E-02   0.36174E+00 0.93991E+03 
c  k            0.10072E-01      61   0.20777E-02   0.57045E-03 0.24202E+03 
c  epsilon      0.87366E+02      42   0.27333E-02   0.32225E+05 0.91017E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8956e-05                            15
a  epsilon          -1.153                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4259          4.7503         0.30838        0.048532
v  Velocity[Y]            -3.9835          4.7855         0.13517         0.11831
v  Velocity[Z]            -7.3262          6.4744        -0.10639     -0.00038722
v  ǁVelocityǁ          6.9787e-06          8.6091         0.85427          1.0032
v  Pressure                -14447           10659          6503.7          5646.6
v  k                   1.8007e-08         0.58397       0.0028306       0.0047481
v  epsilon             6.4245e-06           23641          10.879          2.1998
v  TurbVisc            2.3421e-13         0.11253      0.00066083       0.0043968
v  total_pressure      4.8555e+05      5.1066e+05       5.065e+05      5.0565e+05


 TIME FOR THE TIME STEP               41:        0.73251E+02

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


 INSTANT    0.420000000E+02   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.724384309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491692E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0       v  k                   9.1513e-09         0.58702       0.0028244       0.0047493
v  epsilon             6.8398e-05           23690          10.835          2.1979
v  TurbVisc            9.7899e-14         0.11253      0.00070522       0.0043984
v  total_pressure      4.8551e+05      5.1068e+05      5.0652e+05      5.0566e+05


 TIME FOR THE TIME STEP               40:        0.76944E+02

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


 INSTANT    0.410000000E+02   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        -0.100939383E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491723E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13369E+01 0.20811E+01
   Friction velocity        uet   :  0.65159E-02 0.18916E+01
   Friction velocity        uk    :  0.65103E-02 0.18472E+01
   Dimensionless distance   yplus :  0.29800E-04 0.75345E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        692
   Nb of faces within the viscous sub-layer     :      32781
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27528E+00     112   0.15v  ǁVelocityǁ          7.1075e-06          8.5924         0.85589          1.0032
v  Pressure                -14384           10650          6498.7          5644.6
v  k                   1.3698e-08         0.58714       0.0028298       0.0047474
v  epsilon             7.7621e-05           23713          10.876          2.1968
v  TurbVisc             2.408e-13         0.11253      0.00062397       0.0043954
v  total_pressure      4.8562e+05      5.1065e+05       5.065e+05      5.0564e+05


 TIME FOR THE TIME STEP               42:        0.71103E+02

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


 INSTANT    0.430000000E+02   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        -0.493210392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491719E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12496E+01 0.20814E+01
   Friction velocity        uet   :  0.44286E-02 0.18886E+01
   Friction velocity        uk    :  0.44279E-02 0.18444E+01
   Dimensionless distance   yplus :  0.30254E-04 0.74602E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        685
   Nb of faces within the viscous sub-layer     :      32785
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27536E+00     111   0.15984E+00   0.17043E+01 0.96202E+02 
c  Velocity[X]                                      0.50642E+00 
c  Velocity[Y]                                      0.56611E+00 
c  Velocity[Z]                                      0.63174E+00 
c  Pressure     0.22072E-01     578   0.53236E-02   0.34344E+00 0.27467E+03 
c  k            0.10062E-01      60   0.19698E-02   0.43472E-03 0.21657E+03 
c  epsilon      0.87184E+02      39   0.26557E-02   0.27228E+05 0.90373E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3381e-05                            13
a  epsilon         -1.4344                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4332          4.7027         0.30831        0.048426
v  Velocity[Y]            -4.0341          4.8805         0.13526         0.11826
v  Velocity[Z]            -7.2689          6.1578        -0.10827      -0.0004048
v  ǁVelocityǁ           7.184e-06          8.5529         0.85735          1.0031
v  Pressure                -14389           10645            6492          5640.8
v  k                   9.8873e-09         0.58185       0.0028332       0.0047466
v  epsilon             1.3953e-05           23654          10.891          2.1983
v  TurbVisc            2.4592e-13         0.11253       0.0005936       0.0043943
v  total_pressure      4.8561e+05      5.1065e+05      5.0649e+05      5.0564e+05


 TIME FOR THE TIME STEP               43:        0.76729E+02

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


 INSTANT    0.440000000E+02   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        -0.360916158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491721E+00
Free inlv  ǁVelocityǁ          7.1075e-06          8.5924         0.85589          1.0032
v  Pressure                -14384           10650          6498.7          5644.6
v  k                   1.3698e-08         0.58714       0.0028298       0.0047474
v  epsilon             7.7621e-05           23713          10.876          2.1968
v  TurbVisc             2.408e-13         0.11253      0.00062397       0.0043954
v  total_pressure      4.8562e+05      5.1065e+05       5.065e+05      5.0564e+05


 TIME FOR THE TIME STEP               42:        0.68544E+02

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


 INSTANT    0.430000000E+02   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        -0.493210392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491719E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12496E+01 0.20814E+01
   Friction velocity        uet   :  0.44286E-02 0.18886E+01
   Friction velocity        uk    :  0.44279E-02 0.18444E+01
   Dimensionless distance   yplus :  0.30254E-04 0.74602E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        685
   Nb of faces within the viscous sub-layer     :      32785
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_itev  Velocity[Y]            -4.0257          4.8066         0.13532          0.1182
v  Velocity[Z]            -7.3221           7.333        -0.10917     -0.00036849
v  ǁVelocityǁ          7.2975e-06          8.5612         0.85882          1.0031
v  Pressure                -14397           10633          6484.1          5637.4
v  k                   3.8424e-08         0.58568       0.0028461       0.0047473
v  epsilon             1.2001e-05           23695          10.999          2.2038
v  TurbVisc             2.498e-13         0.11253      0.00056841       0.0043932
v  total_pressure       4.856e+05      5.1063e+05      5.0648e+05      5.0564e+05


 TIME FOR THE TIME STEP               44:        0.73918E+02

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


 INSTANT    0.450000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.127308399E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12794E+01 0.20784E+01
   Friction velocity        uet   :  0.85055E-02 0.18914E+01
   Friction velocity        uk    :  0.84897E-02 0.18470E+01
   Dimensionless distance   yplus :  0.30697E-04 0.74305E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        687
   Nb of faces within the viscous sub-layer     :      32756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27504E+00     111   0.15720E+00   0.17027E+01 0.96664E+02 
c  Velocity[X]                                      0.49462E+00 
c  Velocity[Y]                                      0.54793E+00 
c  Velocity[Z]                                      0.66014E+00 
c  Pressure     0.20325E-01     673   0.46364E-02   0.31820E+00 0.14269E+04 
c  k            0.10080E-01      59   0.30484E-02   0.90600E-03 0.36207E+03 
c  epsilon      0.87841E+02      42   0.42526E-02   0.12756E+06 0.24279E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5995e-05                            14
a  epsilon         -1.1182                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4458            4.62         0.30794        0.048469
v  Velocity[Y]            -4.0342          4.8968          0.1354          0.1182
v  Velocity[Z]            -7.1436          6.2523        -0.11008     -0.00041207
v  ǁVelocityǁ          7.3568e-06          8.3786         0.86007          1.0029
v  Pressure                -14387           10627          6462.7          5622.4
v  k                    3.894e-08         0.58298       0.0028532       0.0047494
v  epsilon             9.9677e-07           23588          11.071          2.2097
v  TurbVisc            2.5268e-13         0.11253      0.00054732       0.0043922
v  total_pressure      4.8561e+05      5.1063e+05      5.0646e+05      5.0562e+05


 TIME FOR THE TIME STEP               45:        0.64592E+02

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


 INSTANT    0.460000000E+02   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         0.175107983E-17
Rough wall                6         v  Velocity[Y]            -4.0257          4.8066         0.13532          0.1182
v  Velocity[Z]            -7.3221           7.333        -0.10917     -0.00036849
v  ǁVelocityǁ          7.2975e-06          8.5612         0.85882          1.0031
v  Pressure                -14397           10633          6484.1          5637.4
v  k                   3.8424e-08         0.58568       0.0028461       0.0047473
v  epsilon             1.2001e-05           23695          10.999          2.2038
v  TurbVisc             2.498e-13         0.11253      0.00056841       0.0043932
v  total_pressure       4.856e+05      5.1063e+05      5.0648e+05      5.0564e+05


 TIME FOR THE TIME STEP               44:        0.76811E+02

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


 INSTANT    0.450000000E+02   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.127308399E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12794E+01 0.20784E+01
   Friction velocity        uet   :  0.85055E-02 0.18914E+01
   Friction velocity        uk    :  0.84897E-02 0.18470E+01
   Dimensionless distance   yplus :  0.30697E-04 0.74305E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        687
   Nb of faces within the viscous sub-layer     :      32756
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMAT-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4449          4.7034         0.30768        0.048455
v  Velocity[Y]            -4.0953          4.9231         0.13546         0.11811
v  Velocity[Z]            -7.1687          7.2163        -0.11098     -0.00039276
v  ǁVelocityǁ          7.4292e-06          8.3832         0.86132           1.003
v  Pressure                -14361           10628          6469.6          5629.5
v  k                   3.9312e-08         0.58584       0.0028499       0.0047483
v  epsilon             7.4284e-05           23654          11.031          2.2052
v  TurbVisc            2.5467e-13         0.11253      0.00053001       0.0043918
v  total_pressure      4.8564e+05      5.1063e+05      5.0647e+05      5.0563e+05


 TIME FOR THE TIME STEP               46:        0.71558E+02

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


 INSTANT    0.470000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.181141977E-18
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 : -0.11846E+01 0.20758E+01
   Friction velocity        uet   :  0.85512E-02 0.18863E+01
   Friction velocity        uk    :  0.85370E-02 0.18422E+01
   Dimensionless distance   yplus :  0.30981E-04 0.73903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        679
   Nb of faces within the viscous sub-layer     :      32744
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27515E+00     111   0.15833E+00   0.16632E+01 0.95190E+02 
c  Velocity[X]                                      0.49184E+00 
c  Velocity[Y]                                      0.55126E+00 
c  Velocity[Z]                                      0.62007E+00 
c  Pressure     0.19370E-01     637   0.43054E-02   0.30299E+00 0.14789E+04 
c  k            0.10089E-01      59   0.18433E-02   0.33070E-03 0.18850E+03 
c  epsilon      0.88191E+02      39   0.24357E-02   0.18931E+05 0.68273E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0667e-05                            18
a  epsilon         -1.3457                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4488          4.6106         0.30737        0.048454
v  Velocity[Y]            -4.0843           4.784         0.13557          0.1181
v  Velocity[Z]            -7.1435          6.3007        -0.11191     -0.00039316
v  ǁVelocityǁ           7.478e-06          8.3933         0.86247          1.0028
v  Pressure                -14380           10610          6460.2          5625.5
v  k                   1.2237e-08         0.58157       0.0028565         0.00475
v  epsilon             1.2627e-05           23503          11.072          2.2103
v  TurbVisc            2.5599e-13         0.11253      0.00051553        0.004391
v  total_pressure      4.8562e+05      5.1061e+05      5.0646e+05      5.0563e+05


 TIME FOR THE TIME STEP               47:        0.72379E+02

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


 INSTANT    0.480000000E+02   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4449          4.7034         0.30768        0.048455
v  Velocity[Y]            -4.0953          4.9231         0.13546         0.11811
v  Velocity[Z]            -7.1687          7.2163        -0.11098     -0.00039276
v  ǁVelocityǁ          7.4292e-06          8.3832         0.86132           1.003
v  Pressure                -14361           10628          6469.6          5629.5
v  k                   3.9312e-08         0.58584       0.0028499       0.0047483
v  epsilon             7.4284e-05           23654          11.031          2.2052
v  TurbVisc            2.5467e-13         0.11253      0.00053001       0.0043918
v  total_pressure      4.8564e+05      5.1063e+05      5.0647e+05      5.0563e+05


 TIME FOR THE TIME STEP               46:        0.83029E+02

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


 INSTANT    0.470000000E+02   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.181141977E-18
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 : -0.11846E+01 0.20758E+01
   Friction velocity        uet   :  0.85512E-02 0.18863E+01
   Friction velocity        uk    :  0.85370E-02 0.18422E+01
   Dimensionless distance   yplus :  0.30981E-04 0.73903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        679
   Nb of faces within the viscous sub-layer     :      3
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4486          4.7422         0.30712        0.048561
v  Velocity[Y]            -3.9801          4.9172         0.13567         0.11808
v  Velocity[Z]            -7.1784          7.4363        -0.11265     -0.00035399
v  ǁVelocityǁ           7.509e-06          8.4029         0.86357          1.0027
v  Pressure                -14352           10603          6454.1          5622.6
v  k                   2.5624e-08         0.58552       0.0028578       0.0047491
v  epsilon             1.7264e-05           23680          11.099           2.208
v  TurbVisc            2.5686e-13         0.11253      0.00050366       0.0043906
v  total_pressure      4.8565e+05       5.106e+05      5.0645e+05      5.0562e+05


 TIME FOR THE TIME STEP               48:        0.63113E+02

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


 INSTANT    0.490000000E+02   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         0.867709571E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491723E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11903E+01 0.20817E+01
   Friction velocity        uet   :  0.74593E-02 0.18911E+01
   Friction velocity        uk    :  0.74489E-02 0.18468E+01
   Dimensionless distance   yplus :  0.31166E-04 0.73751E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        683
   Nb of faces within the viscous sub-layer     :      32751
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27461E+00     112   0.15815E+00   0.16134E+01 0.94277E+02 
c  Velocity[X]                                      0.49336E+00 
c  Velocity[Y]                                      0.52227E+00 
c  Velocity[Z]                                      0.59777E+00 
c  Pressure     0.18296E-01     693   0.39476E-02   0.28663E+00 0.30226E+03 
c  k            0.10083E-01      61   0.20532E-02   0.45194E-03 0.23804E+03 
c  epsilon      0.88007E+02      47   0.33857E-02   0.45073E+05 0.10674E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8044e-05                            15
a  epsilon         -1.1618                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4478          4.5973         0.30685        0.048563
v  Velocity[Y]             -4.084          4.8097          0.1358         0.11802
v  Velocity[Z]            -7.2352          6.2036        -0.11353     -0.00036778
v  ǁVelocityǁ          7.5441e-06          8.4598         0.86457          1.0025
v  Pressure                -14324           10588          6448.9          5620.1
v  k                   3.9833e-08         0.58258       0.0028605       0.0047487
v  epsilon              5.938e-05           23686          11.111          2.2101
v  TurbVisc            2.5724e-13         0.11253      0.00049342       0.0043899
v  total_pressure      4.8568e+05      5.1059e+05      5.0645e+05      5.0562e+05


 TIME FOR THE TIME STEP               49:        0.78398E+02

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


 INSTANT    0.500000000E+02   TIME STEP NUMBER              50
 ============================================================= 




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

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4486          4.7422         0.30712        0.048561
v  Velocity[Y]            -3.9801          4.9172         0.13567         0.11808
v  Velocity[Z]            -7.1784          7.4363        -0.11265     -0.00035399
v  ǁVelocityǁ           7.509e-06          8.4029         0.86357          1.0027
v  Pressure                -14352           10603          6454.1          5622.6
v  k                   2.5624e-08         0.58552       0.0028578       0.0047491
v  epsilon             1.7264e-05           23680          11.099           2.208
v  TurbVisc            2.5686e-13         0.11253      0.00050366       0.0043906
v  total_pressure      4.8565e+05       5.106e+05      5.0645e+05      5.0562e+05


 TIME FOR THE TIME STEP               48:        0.78349E+02

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


 INSTANT    0.490000000E+02   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         0.867709571E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491723E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11903E+01 0.20817E+01
   Friction velocity        uet   :  0.74593E-02 0.18911E+01
   Friction velocity        uk    :  0.74489E-02 0.18468E+01
   Dimensionless distance   yplus :  0.31166E-04 0-  -------  --------------  --------------  ------------  ------------
a  k           -2.2998e-05                            14
a  epsilon         -1.8998                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4389          4.7718         0.30664        0.048585
v  Velocity[Y]            -4.0741          4.9278         0.13594         0.11799
v  Velocity[Z]             -7.221          7.2612        -0.11431     -0.00032812
v  ǁVelocityǁ           7.648e-06          8.4558         0.86568          1.0024
v  Pressure                -14313           10590          6454.7          5626.8
v  k                   3.9871e-08         0.58469       0.0028623       0.0047496
v  epsilon             7.5877e-05           23714           11.11          2.2107
v  TurbVisc            2.5732e-13         0.11253      0.00048473       0.0043893
v  total_pressure      4.8569e+05      5.1059e+05      5.0645e+05      5.0563e+05


 TIME FOR THE TIME STEP               50:        0.78107E+02

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


 INSTANT    0.510000000E+02   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        -0.122520672E-18
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 : -0.12150E+01 0.20786E+01
   Friction velocity        uet   :  0.75226E-02 0.18909E+01
   Friction velocity        uk    :  0.75212E-02 0.18466E+01
   Dimensionless distance   yplus :  0.31469E-04 0.73465E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        681
   Nb of faces within the viscous sub-layer     :      32734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27443E+00     111   0.15922E+00   0.15850E+01 0.94554E+02 
c  Velocity[X]                                      0.48271E+00 
c  Velocity[Y]                                      0.49827E+00 
c  Velocity[Z]                                      0.60399E+00 
c  Pressure     0.16880E-01     608   0.36789E-02   0.26545E+00 0.11897E+04 
c  k            0.10097E-01      58   0.21234E-02   0.33427E-03 0.14756E+03 
c  epsilon      0.88186E+02      40   0.36881E-02   0.23915E+05 0.56167E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9307e-05                            17
a  epsilon         -1.3918                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4477          4.5735         0.30639        0.048557
v  Velocity[Y]            -4.0451          4.9449         0.13618         0.11798
v  Velocity[Z]            -7.1218          6.3462        -0.11504     -0.00033992
v  ǁVelocityǁ          7.6882e-06          8.3338         0.86665          1.0023
v  Pressure                -14249           10580          6439.3            5617
v  k                   3.9866e-08         0.58184       0.0028673       0.0047511
v  epsilon             8.5856e-05           23583          11.139           2.216
v  TurbVisc            2.5723e-13         0.11253      0.00047743       0.0043887
v  total_pressure      4.8575e+05      5.1058e+05      5.0644e+05      5.0562e+05


 TIME FOR THE TIME STEP               51:        0.77771E+02

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


 INSTANT    0.520000000E+02   TIME STEP NUMBER              52
 -  -------  --------------  --------------  ------------  ------------
a  k           -2.2998e-05                            14
a  epsilon         -1.8998                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4389          4.7718         0.30664        0.048585
v  Velocity[Y]            -4.0741          4.9278         0.13594         0.11799
v  Velocity[Z]             -7.221          7.2612        -0.11431     -0.00032812
v  ǁVelocityǁ           7.648e-06          8.4558         0.86568          1.0024
v  Pressure                -14313           10590          6454.7          5626.8
v  k                   3.9871e-08         0.58469       0.0028623       0.0047496
v  epsilon             7.5877e-05           23714           11.11          2.2107
v  TurbVisc            2.5732e-13         0.11253      0.00048473       0.0043893
v  total_pressure      4.8569e+05      5.1059e+05      5.0645e+05      5.0563e+05


 TIME FOR THE TIME STEP               50:        0.81285E+02

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


 INSTANT    0.510000000E+02   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        -0.122520672E-18
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 : -0.12150E+01 0.20786E+01
   Friction velocity        u
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8753e-05                            14
a  epsilon         -1.6637                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4578          4.7631          0.3062        0.048588
v  Velocity[Y]             -4.059          4.8416         0.13642         0.11796
v  Velocity[Z]            -7.1539          7.3015         -0.1156     -0.00029891
v  ǁVelocityǁ          7.7528e-06          8.4091         0.86768          1.0023
v  Pressure                -14254           10576          6439.6          5619.4
v  k                   3.9829e-08         0.58418       0.0028692       0.0047509
v  epsilon             8.1846e-05           23683          11.149          2.2136
v  TurbVisc            2.5696e-13         0.11253      0.00047122       0.0043882
v  total_pressure      4.8575e+05      5.1058e+05      5.0644e+05      5.0562e+05


 TIME FOR THE TIME STEP               52:        0.77946E+02

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


 INSTANT    0.530000000E+02   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        -0.440874770E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.20781E+01
   Friction velocity        uet   :  0.63878E-02 0.18893E+01
   Friction velocity        uk    :  0.63777E-02 0.18451E+01
   Dimensionless distance   yplus :  0.31679E-04 0.73264E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        688
   Nb of faces within the viscous sub-layer     :      32737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27426E+00     111   0.15605E+00   0.15791E+01 0.95213E+02 
c  Velocity[X]                                      0.47955E+00 
c  Velocity[Y]                                      0.51018E+00 
c  Velocity[Z]                                      0.58937E+00 
c  Pressure     0.16247E-01     786   0.32701E-02   0.25667E+00 0.65425E+03 
c  k            0.10091E-01      60   0.17134E-02   0.20768E-03 0.12915E+03 
c  epsilon      0.88105E+02      45   0.20928E-02   0.88411E+04 0.47330E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2605e-05                            14
a  epsilon         -1.3888                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4608          4.5968         0.30597        0.048525
v  Velocity[Y]            -4.0348          4.9187         0.13664         0.11791
v  Velocity[Z]            -7.0914          6.2926        -0.11627      -0.0003508
v  ǁVelocityǁ          7.7566e-06          8.3378         0.86859          1.0022
v  Pressure                -14204           10584          6432.3          5614.5
v  k                    3.978e-08          0.5813       0.0028715        0.004751
v  epsilon             7.1335e-05           23598          11.161          2.2158
v  TurbVisc            2.5656e-13         0.11253      0.00046545       0.0043875
v  total_pressure       4.858e+05      5.1058e+05      5.0643e+05      5.0561e+05


 TIME FOR THE TIME STEP               53:        
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8753e-05                            14
a  epsilon         -1.6637                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4578          4.7631          0.3062        0.048588
v  Velocity[Y]             -4.059          4.8416         0.13642         0.11796
v  Velocity[Z]            -7.1539          7.3015         -0.1156     -0.00029891
v  ǁVelocityǁ          7.7528e-06          8.4091         0.86768          1.0023
v  Pressure                -14254           10576          6439.6          5619.4
v  k                   3.9829e-08         0.58418       0.0028692       0.0047509
v  epsilon             8.1846e-05           23683          11.149          2.2136
v  TurbVisc            2.5696e-13         0.11253      0.00047122       0.0043882
v  total_pressure      4.8575e+05      5.1058e+05      5.0644e+05      5.0562e+05


 TIME FOR THE TIME STEP               52:        0.75581E+02

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


 INSTANT    0.530000000E+02   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        -0.440874770E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         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  epsilon      0.88151E+02      42   0.28542E-02   0.29029E+05 0.60056E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9715e-05                            14
a  epsilon         -1.9255                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.452          4.8048         0.30588        0.048606
v  Velocity[Y]            -4.0706          4.9513         0.13692         0.11794
v  Velocity[Z]            -7.2662          7.2517        -0.11678      -0.0003231
v  ǁVelocityǁ          7.7903e-06          8.5516         0.86954          1.0021
v  Pressure                -14165           10573          6429.3          5613.7
v  k                   3.9708e-08         0.58611       0.0028774       0.0047517
v  epsilon             7.3862e-05           23642          11.204          2.2193
v  TurbVisc            2.5619e-13         0.11253      0.00046037       0.0043868
v  total_pressure      4.8584e+05      5.1057e+05      5.0643e+05      5.0561e+05


 TIME FOR THE TIME STEP               54:        0.75873E+02

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


 INSTANT    0.550000000E+02   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         0.333568334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11785E+01 0.20763E+01
   Friction velocity        uet   :  0.46581E-02 0.18856E+01
   Friction velocity        uk    :  0.46509E-02 0.18417E+01
   Dimensionless distance   yplus :  0.31766E-04 0.73287E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        684
   Nb of faces within the viscous sub-layer     :      32714
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27428E+00     109   0.15553E+00   0.15421E+01 0.94002E+02 
c  Velocity[X]                                      0.45782E+00 
c  Velocity[Y]                                      0.52224E+00 
c  Velocity[Z]                                      0.56207E+00 
c  Pressure     0.15226E-01     595   0.29475E-02   0.24036E+00 0.83721E+03 
c  k            0.10114E-01      58   0.27589E-02   0.40542E-03 0.17825E+03 
c  epsilon      0.88785E+02      38   0.49718E-02   0.22248E+05 0.58855E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1021e-05                            13
a  epsilon         -1.2672                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.456          4.6114          0.3058        0.048637
v  Velocity[Y]            -4.1246          4.8407         0.13724         0.11786
v  Velocity[Z]            -7.0858          6.5362        -0.11725     -0.00033535
v  ǁVelocityǁ          7.7747e-06          8.3168         0.87046          1.0022
v  Pressure                -14120           10570          6425.7          5613.6
v  k                   3.9626e-08         0.58173        0.002881       0.0047513
v  epsilon             7.0568e-05           23558          11.218          2.2228
v  TurbVisc            2.5568e-13         0.11253     c  epsilon      0.88151E+02      42   0.28542E-02   0.29029E+05 0.60056E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9715e-05                            14
a  epsilon         -1.9255                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.452          4.8048         0.30588        0.048606
v  Velocity[Y]            -4.0706          4.9513         0.13692         0.11794
v  Velocity[Z]            -7.2662          7.2517        -0.11678      -0.0003231
v  ǁVelocityǁ          7.7903e-06          8.5516         0.86954          1.0021
v  Pressure                -14165           10573          6429.3          5613.7
v  k                   3.9708e-08         0.58611       0.0028774       0.0047517
v  epsilon             7.3862e-05           23642          11.204          2.2193
v  TurbVisc            2.5619e-13         0.11253      0.00046037       0.0043868
v  total_pressure      4.8584e+05      5.1057e+05      5.0643e+05      5.0561e+05


 TIME FOR THE TIME STEP               54:        0.77668E+02

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


 INSTANT    0.550000000E+02   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         0.333568334E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
 c  Pressure     0.14967E-01     515   0.30596E-02   0.23726E+00 0.32857E+03 
c  k            0.10104E-01      60   0.17857E-02   0.20769E-03 0.11948E+03 
c  epsilon      0.88626E+02      44   0.20516E-02   0.59073E+04 0.37068E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0484e-05                            13
a  epsilon         -1.8589                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4471          4.7907         0.30577        0.048657
v  Velocity[Y]            -4.0456          4.9238         0.13759         0.11788
v  Velocity[Z]            -7.1627          7.3452        -0.11771      -0.0003141
v  ǁVelocityǁ            7.85e-06          8.3789         0.87141          1.0022
v  Pressure                -14077           10580          6425.9          5613.6
v  k                   2.6472e-08         0.58409       0.0028816       0.0047506
v  epsilon              6.744e-05           23677          11.227           2.221
v  TurbVisc            2.5516e-13         0.11253      0.00045131        0.004385
v  total_pressure      4.8592e+05      5.1058e+05      5.0643e+05      5.0561e+05


 TIME FOR THE TIME STEP               56:        0.72498E+02

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


 INSTANT    0.570000000E+02   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        -0.366740661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11867E+01 0.20817E+01
   Friction velocity        uet   :  0.71890E-02 0.18926E+01
   Friction velocity        uk    :  0.71798E-02 0.18483E+01
   Dimensionless distance   yplus :  0.31893E-04 0.73515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        688
   Nb of faces within the viscous sub-layer     :      32705
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27429E+00     109   0.15704E+00   0.15448E+01 0.94227E+02 
c  Velocity[X]                                      0.46606E+00 
c  Velocity[Y]                                      0.48137E+00 
c  Velocity[Z]                                      0.59736E+00 
c  Pressure     0.14639E-01     804   0.28615E-02   0.23176E+00 0.12725E+04 
c  k            0.10116E-01      59   0.18042E-02   0.35130E-03 0.16121E+03 
c  epsilon      0.88663E+02      43   0.22911E-02   0.12093E+05 0.46703E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1321e-05                            15
a  epsilon         -1.3607                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4481          4.7044         0.30576        0.048654
v  Velocity[Y]            -4.0402          4.8355         0.13788         0.11783
v  Velocity[Z]            -7.1522          6.4446        -0.11814     -0.00033007
v  ǁVelocityǁ          7.8571e-06           8.371         0.87227          1.0023
v  Pressure                -14075           10557          6412.7          5606.3
v  k                     1.53e-08         0.58117       0.002885c  Pressure     0.14967E-01     515   0.30596E-02   0.23726E+00 0.32857E+03 
c  k            0.10104E-01      60   0.17857E-02   0.20769E-03 0.11948E+03 
c  epsilon      0.88626E+02      44   0.20516E-02   0.59073E+04 0.37068E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0484e-05                            13
a  epsilon         -1.8589                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4471          4.7907         0.30577        0.048657
v  Velocity[Y]            -4.0456          4.9238         0.13759         0.11788
v  Velocity[Z]            -7.1627          7.3452        -0.11771      -0.0003141
v  ǁVelocityǁ            7.85e-06          8.3789         0.87141          1.0022
v  Pressure                -14077           10580          6425.9          5613.6
v  k                   2.6472e-08         0.58409       0.0028816       0.0047506
v  epsilon              6.744e-05           23677          11.227           2.221
v  TurbVisc            2.5516e-13         0.11253      0.00045131        0.004385
v  total_pressure      4.8592e+05      5.1058e+05      5.0643e+05      5.0561e+05


 TIME FOR THE TIME STEP               56:        0.74329E+02

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


 INSTANT    0.570000000E+02   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        -0.366740661E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0    c  Velocity[X]                                      0.45952E+00 
c  Velocity[Y]                                      0.47347E+00 
c  Velocity[Z]                                      0.57123E+00 
c  Pressure     0.14418E-01     610   0.27030E-02   0.22719E+00 0.72411E+03 
c  k            0.10111E-01      61   0.18098E-02   0.33359E-03 0.16810E+03 
c  epsilon      0.88821E+02      49   0.24780E-02   0.16334E+05 0.63796E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.4624e-05                            16
a  epsilon         -1.9282                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4468          4.7702         0.30584        0.048692
v  Velocity[Y]            -4.0906          4.9479         0.13817         0.11787
v  Velocity[Z]            -7.1723          7.5115        -0.11841     -0.00026038
v  ǁVelocityǁ          7.8751e-06          8.4732         0.87313          1.0024
v  Pressure                -14030           10555          6408.9          5604.4
v  k                   3.9362e-08         0.58547       0.0028858       0.0047517
v  epsilon             5.9613e-05           23815          11.254          2.2256
v  TurbVisc             2.542e-13         0.11253      0.00044393       0.0043834
v  total_pressure      4.8597e+05      5.1055e+05      5.0641e+05       5.056e+05


 TIME FOR THE TIME STEP               58:        0.72843E+02

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


 INSTANT    0.590000000E+02   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        -0.795809085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11445E+01 0.20796E+01
   Friction velocity        uet   :  0.63396E-02 0.18874E+01
   Friction velocity        uk    :  0.63298E-02 0.18435E+01
   Dimensionless distance   yplus :  0.31936E-04 0.73437E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        696
   Nb of faces within the viscous sub-layer     :      32693
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27474E+00     108   0.15819E+00   0.14929E+01 0.92641E+02 
c  Velocity[X]                                      0.46406E+00 
c  Velocity[Y]                                      0.48275E+00 
c  Velocity[Z]                                      0.54612E+00 
c  Pressure     0.14262E-01     519   0.28191E-02   0.22562E+00 0.65263E+03 
c  k            0.10166E-01      58   0.35968E-02   0.20749E-02 0.40128E+03 
c  epsilon      0.90587E+02      41   0.13570E-01   0.66593E+06 0.24431E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.7671e-05                            12
a  epsilon         -1.3187                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4463          4.7231         0.30592        0.048679
v  Velocity[Y]            -4.0288          4.9588          0.1385         0.11782
v  Velocity[Z]            -7.0979          7.2002        -0.11871     -0.00034863
v  ǁVelocityǁ          7.8939e-06c  Velocity[X]                                      0.45952E+00 
c  Velocity[Y]                                      0.47347E+00 
c  Velocity[Z]                                      0.57123E+00 
c  Pressure     0.14418E-01     610   0.27030E-02   0.22719E+00 0.72411E+03 
c  k            0.10111E-01      61   0.18098E-02   0.33359E-03 0.16810E+03 
c  epsilon      0.88821E+02      49   0.24780E-02   0.16334E+05 0.63796E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.4624e-05                            16
a  epsilon         -1.9282                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4468          4.7702         0.30584        0.048692
v  Velocity[Y]            -4.0906          4.9479         0.13817         0.11787
v  Velocity[Z]            -7.1723          7.5115        -0.11841     -0.00026038
v  ǁVelocityǁ          7.8751e-06          8.4732         0.87313          1.0024
v  Pressure                -14030           10555          6408.9          5604.4
v  k                   3.9362e-08         0.58547       0.0028858       0.0047517
v  epsilon             5.9613e-05           23815          11.254          2.2256
v  TurbVisc             2.542e-13         0.11253      0.00044393       0.0043834
v  total_pressure      4.8597e+05      5.1055e+05      5.0641e+05       5.056e+05


 TIME FOR THE TIME STEP               58:        0.78916E+02

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


 INSTANT    0.590000000E+02   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        -0.795809085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet      -----------------------------------------------------------------------------
c  Velocity     0.27465E+00     109   0.15778E+00   0.15484E+01 0.95816E+02 
c  Velocity[X]                                      0.47501E+00 
c  Velocity[Y]                                      0.46289E+00 
c  Velocity[Z]                                      0.61047E+00 
c  Pressure     0.13547E-01     718   0.26502E-02   0.21382E+00 0.10738E+04 
c  k            0.10219E-01      57   0.12099E-01   0.67467E-03 0.19355E+03 
c  epsilon      0.95810E+02      39   0.64818E-01   0.23031E+06 0.12040E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.7898e-05                            17
a  epsilon          -1.843                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.444          4.7841         0.30603        0.048658
v  Velocity[Y]            -4.0924          4.8585         0.13881         0.11782
v  Velocity[Z]             -7.187          7.4022        -0.11891     -0.00034047
v  ǁVelocityǁ          7.9061e-06          8.4341         0.87477          1.0028
v  Pressure                -14012           10553          6398.3          5598.9
v  k                   3.6537e-08         0.58416       0.0028914       0.0047511
v  epsilon             2.8416e-05           23688          11.323          2.2314
v  TurbVisc            2.5329e-13         0.11253      0.00043764       0.0043815
v  total_pressure      4.8599e+05      5.1055e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               60:        0.81171E+02

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


 INSTANT    0.610000000E+02   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         0.177633577E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11794E+01 0.20801E+01
   Friction velocity        uet   :  0.47373E-02 0.18891E+01
   Friction velocity        uk    :  0.47316E-02 0.18451E+01
   Dimensionless distance   yplus :  0.32004E-04 0.73515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        690
   Nb of faces within the viscous sub-layer     :      32698
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27440E+00     108   0.15440E+00   0.15166E+01 0.93782E+02 
c  Velocity[X]                                      0.45472E+00 
c  Velocity[Y]                                      0.49300E+00 
c  Velocity[Z]                                      0.56887E+00 
c  Pressure     0.13248E-01     728   0.24886E-02   0.20914E+00 0.34153E+03 
c  k            0.10205E-01      59   0.17340E-02   0.32190E-03 0.24070E+03 
c  epsilon      0.93581E+02      42   0.27486E-02   0.56625E+05 0.16825E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2646e-05                            12
a  epsilon         -1.3742                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4452          4.7917         0.30614        0.048662
v  Velocity[Y]            -4.0418          4-----------------------------------------------------------------------------
c  Velocity     0.27465E+00     109   0.15778E+00   0.15484E+01 0.95816E+02 
c  Velocity[X]                                      0.47501E+00 
c  Velocity[Y]                                      0.46289E+00 
c  Velocity[Z]                                      0.61047E+00 
c  Pressure     0.13547E-01     718   0.26502E-02   0.21382E+00 0.10738E+04 
c  k            0.10219E-01      57   0.12099E-01   0.67467E-03 0.19355E+03 
c  epsilon      0.95810E+02      39   0.64818E-01   0.23031E+06 0.12040E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.7898e-05                            17
a  epsilon          -1.843                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.444          4.7841         0.30603        0.048658
v  Velocity[Y]            -4.0924          4.8585         0.13881         0.11782
v  Velocity[Z]             -7.187          7.4022        -0.11891     -0.00034047
v  ǁVelocityǁ          7.9061e-06          8.4341         0.87477          1.0028
v  Pressure                -14012           10553          6398.3          5598.9
v  k                   3.6537e-08         0.58416       0.0028914       0.0047511
v  epsilon             2.8416e-05           23688          11.323          2.2314
v  TurbVisc            2.5329e-13         0.11253      0.00043764       0.0043815
v  total_pressure      4.8599e+05      5.1055e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               60:        0.76636E+02

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


 INSTANT    0.610000000E+02   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         0.177633577E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11794E+01 0.20801E+01
   Friction velocity        uet   :  0.47373E-02 0.18891E+01
   Friction velocity        uk    :  0.47316E-02 0.18451E+01
   Dimensionless distance   yplus :  0.32004E-04 0.73515E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        690
   Nb of faces within the viscous sub-layer     :      32698
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27440E+00     108   0.15440E+00   0.15166E+01 0.93782E+02 
c  Velocity[X]                                      0.45472E+00 
c  Velocity[Y]                                      0.49300E+00 
c  Velocity[Z]                                      0.56887E+00 
c  Pressure     0.13248E-01     728   0.24886E-02   0.20914E+00 0.34153E+03 
c  k            0.10205E-01      59   0.17340E-02   0.32190E-03 0.24070E+03 
c  epsilon      0.93581E+02      42   0.27486E-02   0.56625E+05 0.16825E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2646e-05                            12
a  epsilon         -1.3742                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4452          4.7917         0.30614        0.048662
v  Velocity[Y]            -4.0418          4.9371         0.13907         0.11775
v  Velocity[Z]            -7.0762          6.9364          -0.119     -0.00029373
v  ǁVelocityǁ           7.875e-06          8.2639         0.87546          1.0029
v  Pressure                -13943           10550            6392            5594
v  k                   1.1517e-08         0.58007       0.0028935       0.0047516
v  epsilon             5.2276e-05           23655          11.358          2.2329
v  TurbVisc            2.5282e-13         0.11253       0.0004347       0.0043809
v  total_pressure      4.8606e+05      5.1055e+05      5.0639e+05      5.0559e+05


 TIME FOR THE TIME STEP               61:        0.78042E+02

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


 INSTANT    0.620000000E+02   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         0.197923301E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491728E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11248E+01 0.20819E+01
   Friction velocity        uet   :  0.23896E-02 0.18949E+01
   Friction velocity        uk    :  0.23868E-02 0.18506E+01
   Dimensionless distance   yplus :  0.31937E-04 0.73281E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        693
   Nb of faces within the viscous sub-layer     :      32693
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27476E+00     108   0.15341E+00   0.14371E+01 0.92066E+02 
c  Velocity[X]                                      0.42767E+00 
c  Velocity[Y]                                      0.47729E+00 
c  Velocity[Z]                                      0.53218E+00 
c  Pressure     0.12541E-01     678   0.24230E-02   0.19857E+00 0.65111E+03 
c  k            0.10190E-01      58   0.18027E-02   0.17272E-03 0.11063E+03 
c  epsilon      0.93417E+02      40   0.24051E-02   0.74578E+04 0.42806E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6833e-05                            14
a  epsilon         -2.0161                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4563          4.8286         0.30633        0.048681
v  Velocity[Y]            -4.0635          4.9594         0.13927         0.11783
v  Velocity[Z]            -7.1427          7.5817        -0.11915     -0.00033333
v  ǁVelocityǁ          7.9231e-06          8.4679         0.87627          1.0032
v  Pressure                -13894           10562          6405.6          5604.9
v  k                   3.9025e-08          0.5849       0.0028925       0.0047508
v  epsilon             5.1654e-05           23739          11.354          2.2301
v  TurbVisc            2.5238e-13         0.11253      0.00043197       0.0043804
v  total_pressure      4.8611e+05      5.1056e+05      5.0641e+05       5.056e+05


 TIME FOR THE TIME STEP               62:        0.75853E+02

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


 INSTANT    0.630000000E+02   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-----------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27505E+00     107   0.15755E+00   0.14696E+01 0.93536E+02 
c  Velocity[X]                                      0.46703E+00 
c  Velocity[Y]                                      0.44706E+00 
c  Velocity[Z]                                      0.55547E+00 
c  Pressure     0.11928E-01     599   0.23942E-02   0.18849E+00 0.34701E+03 
c  k            0.10206E-01      57   0.15697E-02   0.25951E-03 0.17979E+03 
c  epsilon      0.93809E+02      40   0.26201E-02   0.20983E+05 0.73263E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7661e-05                            17
a  epsilon         -1.8176                            34


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.442           4.886         0.30658        0.048671
v  Velocity[Y]            -4.0423          4.9452         0.13963         0.11778
v  Velocity[Z]             -7.222          7.5374        -0.11924     -0.00031215
v  ǁVelocityǁ          7.9183e-06          8.4501         0.87738          1.0037
v  Pressure                -13903           10544          6397.3          5599.6
v  k                   3.5492e-08         0.58413       0.0028917       0.0047506
v  epsilon             9.4653e-06           23738          11.364          2.2322
v  TurbVisc            2.5164e-13         0.11253      0.00042681       0.0043793
v  total_pressure       4.861e+05      5.1054e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               64:        0.69075E+02

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


 INSTANT    0.650000000E+02   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         0.574498382E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12246E+01 0.20837E+01
   Friction velocity        uet   :  0.51412E-02 0.18857E+01
   Friction velocity        uk    :  0.51347E-02 0.18419E+01
   Dimensionless distance   yplus :  0.32024E-04 0.73276E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        699
   Nb of faces within the viscous sub-layer     :      32705
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27510E+00     107   0.15797E+00   0.14938E+01 0.93700E+02 
c  Velocity[X]                                      0.45344E+00 
c  Velocity[Y]                                      0.46796E+00 
c  Velocity[Z]                                      0.57238E+00 
c  Pressure     0.11800E-01     649   0.24876E-02   0.18637E+00 0.35036E+03 
c  k            0.10214E-01      57   0.18513E-02   0.31216E-03 0.14630E+03 
c  epsilon      0.93926E+02      39   0.22877E-02   0.10135E+05 0.42198E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9958e-05                            13
a  epsilon          -1.485                            23


  **   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27505E+00     107   0.15755E+00   0.14696E+01 0.93536E+02 
c  Velocity[X]                                      0.46703E+00 
c  Velocity[Y]                                      0.44706E+00 
c  Velocity[Z]                                      0.55547E+00 
c  Pressure     0.11928E-01     599   0.23942E-02   0.18849E+00 0.34701E+03 
c  k            0.10206E-01      57   0.15697E-02   0.25951E-03 0.17979E+03 
c  epsilon      0.93809E+02      40   0.26201E-02   0.20983E+05 0.73263E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7661e-05                            17
a  epsilon         -1.8176                            34


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.442           4.886         0.30658        0.048671
v  Velocity[Y]            -4.0423          4.9452         0.13963         0.11778
v  Velocity[Z]             -7.222          7.5374        -0.11924     -0.00031215
v  ǁVelocityǁ          7.9183e-06          8.4501         0.87738          1.0037
v  Pressure                -13903           10544          6397.3          5599.6
v  k                   3.5492e-08         0.58413       0.0028917       0.0047506
v  epsilon             9.4653e-06           23738          11.364          2.2322
v  TurbVisc            2.5164e-13         0.11253      0.00042681       0.0043793
v  total_pressure       4.861e+05      5.1054e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               64:        0.67435E+02

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


 INSTANT    0.650000000E+02   TIME STEP NUMBER              65
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      -----------------------------   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        704
   Nb of faces within the viscous sub-layer     :      32721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27534E+00     105   0.15691E+00   0.14952E+01 0.94157E+02 
c  Velocity[X]                                      0.44915E+00 
c  Velocity[Y]                                      0.48113E+00 
c  Velocity[Z]                                      0.56490E+00 
c  Pressure     0.11239E-01     681   0.25237E-02   0.17740E+00 0.19525E+03 
c  k            0.10213E-01      58   0.16269E-02   0.26417E-03 0.14559E+03 
c  epsilon      0.93568E+02      39   0.21600E-02   0.14183E+05 0.53030E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9653e-05                            15
a  epsilon         -1.9221                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.428          4.8972         0.30677        0.048621
v  Velocity[Y]            -4.0645          4.8556          0.1399         0.11777
v  Velocity[Z]            -7.0971          6.7211        -0.11922     -0.00030905
v  ǁVelocityǁ          7.9368e-06          8.4169          0.8782          1.0041
v  Pressure                -13844           10552          6398.2          5601.9
v  k                   3.8127e-08         0.58508       0.0028865       0.0047505
v  epsilon             5.8425e-05           23827          11.347           2.232
v  TurbVisc            2.5092e-13         0.11253      0.00042195       0.0043784
v  total_pressure      4.8616e+05      5.1055e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               66:        0.78311E+02

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


 INSTANT    0.670000000E+02   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         0.580498790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491729E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11335E+01 0.20800E+01
   Friction velocity        uet   :  0.49184E-02 0.18866E+01
   Friction velocity        uk    :  0.49108E-02 0.18428E+01
   Dimensionless distance   yplus :  0.32065E-04 0.73370E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        701
   Nb of faces within the viscous sub-layer     :      32712
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27536E+00     106   0.15503E+00   0.14903E+01 0.93345E+02 
c  Velocity[X]                                      0.46394E+00 
c  Velocity[Y]                                      0.45389E+00 
c  Velocity[Z]                                      0.57243E+00 
c  Pressure     0.11232E-01     564   0.24256E-02   0.17742E+00 0.16859E+03 
c  k            0.10218E-01      57   0.15593E-02   0.32291E-03 0.19255E+03 
c  epsilon      0.94004E+02      38   0.25103E-02   0.24290E+05 0.71403E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        704
   Nb of faces within the viscous sub-layer     :      32721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27534E+00     105   0.15691E+00   0.14952E+01 0.94157E+02 
c  Velocity[X]                                      0.44915E+00 
c  Velocity[Y]                                      0.48113E+00 
c  Velocity[Z]                                      0.56490E+00 
c  Pressure     0.11239E-01     681   0.25237E-02   0.17740E+00 0.19525E+03 
c  k            0.10213E-01      58   0.16269E-02   0.26417E-03 0.14559E+03 
c  epsilon      0.93568E+02      39   0.21600E-02   0.14183E+05 0.53030E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9653e-05                            15
a  epsilon         -1.9221                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.428          4.8972         0.30677        0.048621
v  Velocity[Y]            -4.0645          4.8556          0.1399         0.11777
v  Velocity[Z]            -7.0971          6.7211        -0.11922     -0.00030905
v  ǁVelocityǁ          7.9368e-06          8.4169          0.8782          1.0041
v  Pressure                -13844           10552          6398.2          5601.9
v  k                   3.8127e-08         0.58508       0.0028865       0.0047505
v  epsilon             5.8425e-05           23827          11.347           2.232
v  TurbVisc            2.5092e-13         0.11253      0.00042195       0.0043784
v  total_pressure      4.8616e+05      5.1055e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               66:        0.78405E+02

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


 INSTANT    0.670000000E+02   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         0.580498790E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491729E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11335E+01 0.20800E+01
   Friction velocity        uet   :  0.49184E-02 0.18866E+01
   Friction velocity        uk    :  0.49108E-02 0.18428E+01
   Dimensionless distance   yplus :  0.32065E-04 0.73370E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        701
   Nb of faces within the viscous sub-layer     :      32712
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27536E+00     106   0.15503E+00   0.14903E+01 0.93345E+02 
c  Velocity[X]                                      0.46394E+00 
c  Velocity[Y]                                      0.45389E+00 
c  Velocity[Z]                                      0.57243E+00 
c  Pressure     0.11232E-01     564   0.24256E-02   0.17742E+00 0.16859E+03 
c  k            0.10218E-01      57   0.15593E-02   0.32291E-03 0.19255E+03 
c  epsilon      0.94004E+02      38   0.25103E-02   0.24290E+05 0.71403E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6429e-05                            12
a  epsilon         -1.4241                            30


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4303          4.8807         0.30686        0.048677
v  Velocity[Y]             -4.115          4.9455         0.13999         0.11779
v  Velocity[Z]            -7.2939          7.4216        -0.11922     -0.00036167
v  ǁVelocityǁ          7.9252e-06          8.5684         0.87866          1.0044
v  Pressure                -13835           10553          6400.6          5604.3
v  k                   3.8646e-08         0.58207       0.0028887       0.0047516
v  epsilon             2.3814e-05           23659          11.368          2.2349
v  TurbVisc            2.5051e-13         0.11253      0.00041947       0.0043782
v  total_pressure      4.8616e+05      5.1055e+05       5.064e+05       5.056e+05


 TIME FOR THE TIME STEP               67:        0.74131E+02

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


 INSTANT    0.680000000E+02   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        -0.200104386E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491697E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12607E+01 0.20806E+01
   Friction velocity        uet   :  0.52508E-02 0.18931E+01
   Friction velocity        uk    :  0.52426E-02 0.18490E+01
   Dimensionless distance   yplus :  0.32038E-04 0.73221E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        707
   Nb of faces within the viscous sub-layer     :      32712
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27553E+00     105   0.15720E+00   0.14415E+01 0.92075E+02 
c  Velocity[X]                                      0.45349E+00 
c  Velocity[Y]                                      0.44608E+00 
c  Velocity[Z]                                      0.54194E+00 
c  Pressure     0.11116E-01     609   0.25893E-02   0.17549E+00 0.30336E+03 
c  k            0.10226E-01      57   0.20189E-02   0.30142E-03 0.18107E+03 
c  epsilon      0.94072E+02      38   0.29799E-02   0.18685E+05 0.59049E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.0038e-05                            17
a  epsilon         -1.9546                            35


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4441          4.9407         0.30694        0.048615
v  Velocity[Y]            -4.1016          4.9993         0.13999          0.1178
v  Velocity[Z]            -7.1652          6.8616        -0.11914     -0.00030216
v  ǁVelocityǁ          7.9644e-06          8.4114         0.87914          1.0047
v  Pressure                -13784           10561          6405.3          5608.8
v  k                   3.3516e-08         0.58412       0.0028869       0.0047525
v  epsilon             5.3672e-05           23701          11.359          2.2347
v  TurbVisc            2.5009e-13         0.11253      0.00041725       0.0043778
v  total_pressure      4.8622e+05      5.1056e+05                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13193E+01 0.20833E+01
   Friction velocity        uet   :  0.34549E-02 0.18917E+01
   Friction velocity        uk    :  0.34506E-02 0.18477E+01
   Dimensionless distance   yplus :  0.32105E-04 0.73545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32708
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27587E+00     106   0.15586E+00   0.14397E+01 0.92360E+02 
c  Velocity[X]                                      0.45170E+00 
c  Velocity[Y]                                      0.46407E+00 
c  Velocity[Z]                                      0.52395E+00 
c  Pressure     0.10341E-01     538   0.22292E-02   0.16333E+00 0.80980E+03 
c  k            0.10231E-01      57   0.16668E-02   0.36115E-03 0.18316E+03 
c  epsilon      0.94222E+02      44   0.24963E-02   0.21241E+05 0.62303E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7858e-05                            14
a  epsilon         -1.9832                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4436          4.9387         0.30706        0.048579
v  Velocity[Y]            -4.0488          4.9817         0.13996          0.1178
v  Velocity[Z]            -7.2174          7.8346        -0.11898     -0.00031456
v  ǁVelocityǁ          7.9715e-06          8.4117         0.87996          1.0052
v  Pressure                -13769           10559          6401.7          5606.8
v  k                   5.2051e-09         0.58535       0.0028851       0.0047539
v  epsilon             2.6806e-05           23771          11.355          2.2367
v  TurbVisc            2.4935e-13         0.11253      0.00041276       0.0043773
v  total_pressure      4.8623e+05      5.1056e+05       5.064e+05      5.0561e+05


 TIME FOR THE TIME STEP               70:        0.67164E+02

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


 INSTANT    0.710000000E+02   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        -0.184275507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491725E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12518E+01 0.20821E+01
   Friction velocity        uet   :  0.35168E-02 0.18859E+01
   Friction velocity        uk    :  0.35125E-02 0.18422E+01
   Dimensionless distance   yplus :  0.32134E-04 0.73451E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27577E+00     106   0.15845E+00   0.14467E+01 0.92468E+02 
c  Velocity[X]                                      0.44810E+00 
c  Velocity[Y]                                      0.47355E+00 
c  Velocity[Z]                                      0.52503E+00 
c  Pressure     0.10212E-01     750   0.20492E-02   0.16112E+00 0.69090E+03 
c  k            0.10232E-0                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13193E+01 0.20833E+01
   Friction velocity        uet   :  0.34549E-02 0.18917E+01
   Friction velocity        uk    :  0.34506E-02 0.18477E+01
   Dimensionless distance   yplus :  0.32105E-04 0.73545E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32708
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27587E+00     106   0.15586E+00   0.14397E+01 0.92360E+02 
c  Velocity[X]                                      0.45170E+00 
c  Velocity[Y]                                      0.46407E+00 
c  Velocity[Z]                                      0.52395E+00 
c  Pressure     0.10341E-01     538   0.22292E-02   0.16333E+00 0.80980E+03 
c  k            0.10231E-01      57   0.16668E-02   0.36115E-03 0.18316E+03 
c  epsilon      0.94222E+02      44   0.24963E-02   0.21241E+05 0.62303E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7858e-05                            14
a  epsilon         -1.9832                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4436          4.9387         0.30706        0.048579
v  Velocity[Y]            -4.0488          4.9817         0.13996          0.1178
v  Velocity[Z]            -7.2174          7.8346        -0.11898     -0.00031456
v  ǁVelocityǁ          7.9715e-06          8.4117         0.87996          1.0052
v  Pressure                -13769           10559          6401.7          5606.8
v  k                   5.2051e-09         0.58535       0.0028851       0.0047539
v  epsilon             2.6806e-05           23771          11.355    ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11243E+01 0.20843E+01
   Friction velocity        uet   :  0.44088E-02 0.18942E+01
   Friction velocity        uk    :  0.44068E-02 0.18499E+01
   Dimensionless distance   yplus :  0.32174E-04 0.73776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        707
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27603E+00     103   0.15487E+00   0.14591E+01 0.92556E+02 
c  Velocity[X]                                      0.45840E+00 
c  Velocity[Y]                                      0.44922E+00 
c  Velocity[Z]                                      0.55146E+00 
c  Pressure     0.10071E-01     533   0.22140E-02   0.15862E+00 0.20994E+03 
c  k            0.10230E-01      59   0.14862E-02   0.23887E-03 0.16888E+03 
c  epsilon      0.94204E+02      41   0.22581E-02   0.18277E+05 0.65151E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.1152e-05                            17
a  epsilon         -1.6428                            32


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4383          4.9482         0.30721        0.048497
v  Velocity[Y]            -4.1322          4.8662         0.13986         0.11774
v  Velocity[Z]            -7.2728           7.541        -0.11887      -0.0003349
v  ǁVelocityǁ          7.9945e-06          8.4826         0.88088          1.0056
v  Pressure                -13698           10572          6413.7          5617.1
v  k                   1.2209e-08         0.58474       0.0028788       0.0047545
v  epsilon             4.4649e-05           23793           11.34          2.2356
v  TurbVisc            2.4872e-13         0.11253      0.00040832       0.0043766
v  total_pressure       4.863e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               72:        0.74199E+02

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


 INSTANT    0.730000000E+02   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         0.600487967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491699E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12529E+01 0.20821E+01
   Friction velocity        uet   :  0.33396E-02 0.18863E+01
   Friction velocity        uk    :  0.33354E-02 0.18426E+01
   Dimensionless distance   yplus :  0.32182E-04 0.73644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        716
   Nb of faces within the viscous sub-layer     :      32720
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27604E+00     105   0.15555E+00   0.14066E+01 0.90927E+02 
c  Velocity[X]                                      0.44816E+00 
c  Velocity[Y]                                      0.44048E+00 
c  Velocity[Z]          ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11243E+01 0.20843E+01
   Friction velocity        uet   :  0.44088E-02 0.18942E+01
   Friction velocity        uk    :  0.44068E-02 0.18499E+01
   Dimensionless distance   yplus :  0.32174E-04 0.73776E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        707
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27603E+00     103   0.15487E+00   0.14591E+01 0.92556E+02 
c  Velocity[X]                                      0.45840E+00 
c  Velocity[Y]                                      0.44922E+00 
c  Velocity[Z]                                      0.55146E+00 
c  Pressure     0.10071E-01     533   0.22140E-02   0.15862E+00 0.20994E+03 
c  k            0.10230E-01      59   0.14862E-02   0.23887E-03 0.16888E+03 
c  epsilon      0.94204E+02      41   0.22581E-02   0.18277E+05 0.65151E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.1152e-05                            17
a  epsilon         -1.6428                            32


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4383          4.9482         0.30721        0.048497
v  Velocity[Y]            -4.1322          4.8662         0.13986         0.11774
v  Velocity[Z]            -7.2728           7.541        -0.11887      -0.0003349
v  ǁVelocityǁ          7.9945e-06          8.4826         0.88088          1.0056
v  Pressure                -13698           10572          6413.7          5617.1
v  k                   1.2209e-08         0.58474       0.0028788       0.0047545
v  epsilon             4.4649e-05           23793           11.34          2.2356
v  TurbVisc            2.4872e-13         0.11253      0.00040832       0.0043766
v  total_pressure       4.863e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               72:        0.73999E+02

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


 INSTANT    0.730000000E+02   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         0.600487967E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491699E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12529E+01 0.20821E+01
   Friction velocity        uet   :  0.33396E-02 0.18863E+01
   Friction velocity        uk    :  0.33354E-02 0.18426E+01
   Dimensionless distance   yplus :  0.32182E-04 0.73644E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        716
   Nb of faces within the viscous sub-layer     :      32720
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27604E+00     105   0.15555E+00   0.14066E+01 0.90927E+02 
c  Velocity[X]                                      0.44816E+00 
c  Velocity[Y]                                      0.44048E+00 
c  Velocity[Z]                                      0.51793E+00 
c  Pressure     0.99221E-02     720   0.21168E-02   0.15661E+00 0.34424E+03 
c  k            0.10240E-01      58   0.14164E-02   0.20218E-03 0.14238E+03 
c  epsilon      0.94185E+02      39   0.19719E-02   0.15327E+05 0.58390E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.0709e-05                            14
a  epsilon         -1.4045                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4429          4.9331         0.30735        0.048571
v  Velocity[Y]            -4.1335          4.9711          0.1398         0.11777
v  Velocity[Z]            -7.2771           6.946        -0.11887     -0.00038496
v  ǁVelocityǁ          7.9932e-06          8.4911         0.88137          1.0059
v  Pressure                -13727           10579          6416.6          5620.4
v  k                   4.6921e-09         0.58059       0.0028778       0.0047554
v  epsilon             1.8435e-05           23697          11.342          2.2374
v  TurbVisc            2.4838e-13         0.11253      0.00040617       0.0043764
v  total_pressure      4.8627e+05      5.1058e+05      5.0642e+05      5.0562e+05


 TIME FOR THE TIME STEP               73:        0.81727E+02

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


 INSTANT    0.740000000E+02   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.174755874E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491687E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12477E+01 0.20836E+01
   Friction velocity        uet   :  0.56378E-02 0.18943E+01
   Friction velocity        uk    :  0.56308E-02 0.18501E+01
   Dimensionless distance   yplus :  0.32177E-04 0.73624E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        721
   Nb of faces within the viscous sub-layer     :      32718
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27626E+00     104   0.15730E+00   0.14235E+01 0.91155E+02 
c  Velocity[X]                                      0.44033E+00 
c  Velocity[Y]                                      0.45406E+00 
c  Velocity[Z]                                      0.52911E+00 
c  Pressure     0.96478E-02     665   0.20317E-02   0.15178E+00 0.34818E+03 
c  k            0.10239E-01      56   0.16368E-02   0.31267E-03 0.22701E+03 
c  epsilon      0.94350E+02      38   0.28192E-02   0.40145E+05 0.12344E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9884e-05                            16
a  epsilon         -2.0306                            31


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4451          4.9412         0.30748        0.048495
v  Velocity[Y]             -4.115          5.0156         0.13968         0.11777
v  Velocity[Z]            -7.1833          7.4256         -0.1188     -0.00032605
v  ǁVelocityǁ          8.0283e-06          8.4342         0.88184           1.006
v  Pressure                -13713           10583          6414.1          5618.6
v  k                   7.3044e-09         0.58553       0.0028777       0.0047557
v  epsilon             4.2554e-05           23768          11.367          2.2373
v  TurbVisc            2.4802e-13         0.22259      0.00040483       0.0043764
v  total_pressure      4.8629e+05      5.1058e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               74:        0.76428E+02

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


 INSTANT    0.750000000E+02   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        -0.164037471E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11923E+01 0.20839E+01
   Friction velocity        uet   :  0.48355E-02 0.18934E+01
   Friction velocity        uk    :  0.48294E-02 0.18492E+01
   Dimensionless distance   yplus :  0.32256E-04 0.73847E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        717
   Nb of faces within the viscous sub-layer     :      32726
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27622E+00     104   0.15661E+00   0.14854E+01 0.93604E+02 
c  Velocity[X]                                      0.45908E+00 
c  Velocity[Y]                                      0.45231E+00 
c  Velocity[Z]                                      0.57396E+00 
c  Pressure     0.96568E-02     630   0.19048E-02   0.15248E+00 0.21866E+03 
c  k            0.10231E-01      56   0.22036E-02   0.41399E-03 0.21107E+03 
c  epsilon      0.94193E+02      38   0.41581E-02   0.35101E+05 0.83413E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.7408e-05                            12
a  epsilon          -1.565                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4392          4.9426         0.30757        0.048527
v  Velocity[Y]            -4.1074          4.9324         0.13962         0.11772
v  Velocity[Z]             -7.162          7.0365        -0.11879     -0.00038379
v  ǁVelocityǁ          8.0339e-06          8.3755         0.88233          1.0062
v  Pressure                -13741           10586          6415.4          5620.3
v  k                   4.7671e-09         0.58166        0.002874       0.0047553
v  epsilon             4.0095e-05           23730          11.353          2.2354
v  TurbVisc            2.4772e-13         0.11253       0.0004019        0.004376
v  total_pressure      4.8626e+05      5.1059e+05      5.0642e+05      5.0562e+05


 TIME FOR THE TIME STEP               75:        0.76260E+02

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


 INSTANT    0.760000000E+02   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        -0.384685592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491689E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11758E+01 0.20881E+01
   Friction velocity        uet   :  0.14939E-02 0.18954E+01
   Friction velocity        uk    :  0.14923E-02 0.18512E+01
   Dimensionless distance   yplus :  0.32261E-04 0.73886E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        725
   Nb of faces within the viscous sub-layer     :      32706
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27643E+00     105   0.16168E+00   0.14602E+01 0.92544E+02 
c  Velocity[X]                                      0.47537E+00 
c  Velocity[Y]                                      0.44769E+00 
c  Velocity[Z]                                      0.53718E+00 
c  Pressure     0.93473E-02     482   0.20262E-02   0.14685E+00 0.23994E+03 
c  k            0.10242E-01      56   0.15859E-02   0.32128E-03 0.17166E+03 
c  epsilon      0.94564E+02      38   0.21356E-02   0.16350E+05 0.59687E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.3021e-05                            16
a  epsilon         -1.7606                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4331           4.937         0.30774        0.048483
v  Velocity[Y]            -4.1628          4.9833         0.13949         0.11775
v  Velocity[Z]             -7.155          7.3182        -0.11885     -0.00030055
v  ǁVelocityǁ          8.0306e-06          8.4007         0.88287          1.0063
v  Pressure                -13689           10590          6415.6          5620.6
v  k                   1.5845e-09         0.58432       0.0028767       0.0047574
v  epsilon             2.4375e-05           23881          11.381          2.2399
v  TurbVisc            2.4737e-13         0.11253      0.00039977       0.0043757
v  total_pressure      4.8631e+05      5.1059e+05      5.0642e+05      5.0562e+05


 TIME FOR THE TIME STEP               76:        0.68579E+02

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


 INSTANT    0.770000000E+02   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        -0.457564066E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491725E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11764E+01 0.20865E+01
   Friction velocity        uet   :  0.55463E-02 0.18892E+01
   Friction velocity        uk    :  0.55395E-02 0.18454E+01
   Dimensionless distance   yplus :  0.32255E-04 0.73744E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        717
   Nb of faces within the viscous sub-layer     :      32713
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27619E+00     106   0.15433E+00   0.15178E+01 0.94975E+02 
c  Velocity[X]                                      0.45537E+00 
c  Velocity[Y]                                      0.51593E+00 
c  Velocity[Z]                                      0.54652E+00 
c  Pressure     0.93301E-02     624   0.19042E-02   0.14739E+00 0.33518E+03 
c  k            0.10246E-01      66   0.17346E-02   0.51517E-03 0.42447E+03 
c  epsilon      0.94281E+02      59   0.28234E-02   0.37427E+06 0.66805E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6058e-05                            12
a  epsilon         -1.4791                            23


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4225          4.9273         0.30781        0.048454
v  Velocity[Y]            -4.0989          4.9704         0.13943         0.11775
v  Velocity[Z]            -7.2009          6.8761        -0.11892     -0.00040134
v  ǁVelocityǁ           8.051e-06          8.4046         0.88335          1.0064
v  Pressure                -13734           10584          6420.9          5625.1
v  k                   2.8932e-09         0.58136       0.0028835       0.0047565
v  epsilon             4.0524e-05           23786          11.634          2.2411
v  TurbVisc            9.4275e-14         0.11253      0.00039793       0.0043754
v  total_pressure      4.8627e+05      5.1058e+05      5.0642e+05      5.0563e+05


 TIME FOR THE TIME STEP               77:        0.71470E+02

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


 INSTANT    0.780000000E+02   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         0.105207526E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12110E+01 0.20879E+01
   Friction velocity        uet   :  0.33924E-02 0.18982E+01
   Friction velocity        uk    :  0.33882E-02 0.18538E+01
   Dimensionless distance   yplus :  0.32303E-04 0.74095E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        720
   Nb of faces within the viscous sub-layer     :      32709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27647E+00     104   0.15356E+00   0.14118E+01 0.91483E+02 
c  Velocity[X]                                      0.43761E+00 
c  Velocity[Y]                                      0.44264E+00 
c  Velocity[Z]                                      0.53158E+00 
c  Pressure     0.91346E-02     656   0.18488E-02   0.14362E+00 0.11623E+04 
c  k            0.10247E-01      59   0.18747E-02   0.40971E-03 0.36369E+03 
c  epsilon      0.94108E+02      44   0.46176E-02   0.27958E+06 0.57042E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5928e-05                            15
a  epsilon         -1.9733                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4339          4.9472         0.30796        0.048445
v  Velocity[Y]            -4.1882          4.9032         0.13933         0.11775
v  Velocity[Z]            -7.1127          7.6097        -0.11892      -0.0003225
v  ǁVelocityǁ          8.0368e-06          8.4604         0.88387          1.0065
v  Pressure                -13701           10565          6406.3            5615
v  k                   2.9467e-09         0.58604       0.0028785       0.0047588
v  epsilon             4.0144e-05           23869          11.438          2.2426
v  TurbVisc            2.4675e-13         0.11253      0.00039497       0.0043749
v  total_pressure       4.863e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               78:        0.78239E+02

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


 INSTANT    0.790000000E+02   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.115305958E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491698E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11574E+01 0.20850E+01
   Friction velocity        uet   :  0.48982E-02 0.18885E+01
   Friction velocity        uk    :  0.48923E-02 0.18447E+01
   Dimensionless distance   yplus :  0.32271E-04 0.73927E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        716
   Nb of faces within the viscous sub-layer     :      32715
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27649E+00     105   0.15650E+00   0.14185E+01 0.91800E+02 
c  Velocity[X]                                      0.44644E+00 
c  Velocity[Y]                                      0.45185E+00 
c  Velocity[Z]                                      0.52016E+00 
c  Pressure     0.89752E-02     643   0.18019E-02   0.14101E+00 0.10146E+04 
c  k            0.10250E-01      57   0.18356E-02   0.40128E-03 0.22870E+03 
c  epsilon      0.94215E+02      41   0.34354E-02   0.48421E+05 0.12643E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.8582e-05                            12
a  epsilon         -1.5131                            26


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4533          4.9331         0.30809        0.048503
v  Velocity[Y]            -4.1157          4.9858         0.13931          0.1178
v  Velocity[Z]            -7.2058          7.4723        -0.11901     -0.00037474
v  ǁVelocityǁ          8.0558e-06          8.4263         0.88442          1.0066
v  Pressure                -13673           10583          6419.9            5626
v  k                   1.9348e-09         0.58226       0.0028761       0.0047577
v  epsilon             3.6791e-05           23769          11.409          2.2422
v  TurbVisc             2.464e-13         0.11253      0.00039276       0.0043746
v  total_pressure      4.8633e+05      5.1058e+05      5.0642e+05      5.0563e+05


 TIME FOR THE TIME STEP               79:        0.68242E+02

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


 INSTANT    0.800000000E+02   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         0.642188872E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491729E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12082E+01 0.20850E+01
   Friction velocity        uet   :  0.37199E-02 0.18944E+01
   Friction velocity        uk    :  0.37154E-02 0.18503E+01
   Dimensionless distance   yplus :  0.32303E-04 0.73811E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        726
   Nb of faces within the viscous sub-layer     :      32702
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27650E+00     106   0.16034E+00   0.14497E+01 0.91588E+02 
c  Velocity[X]                                      0.45258E+00 
c  Velocity[Y]                                      0.45489E+00 
c  Velocity[Z]                                      0.54222E+00 
c  Pressure     0.89738E-02     658   0.20666E-02   0.14149E+00 0.26729E+03 
c  k            0.10260E-01      58   0.12041E-02   0.22322E-03 0.15692E+03 
c  epsilon      0.94286E+02      43   0.19501E-02   0.24492E+05 0.68437E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6424e-05                            15
a  epsilon         -1.8259                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4263          4.9306         0.30816        0.048461
v  Velocity[Y]            -4.1049          4.9907          0.1393         0.11783
v  Velocity[Z]            -7.2564          7.3984        -0.11904     -0.00033081
v  ǁVelocityǁ          8.0687e-06          8.5115         0.88497          1.0067
v  Pressure                -13665           10587          6421.7            5628
v  k                   5.7105e-09         0.58531       0.0028775       0.0047592
v  epsilon             3.8801e-05           23800          11.422          2.2454
v  TurbVisc            1.8418e-13         0.11253      0.00039066       0.0043741
v  total_pressure      4.8633e+05      5.1059e+05      5.0642e+05      5.0563e+05


 TIME FOR THE TIME STEP               80:        0.70539E+02

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


 INSTANT    0.810000000E+02   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        -0.113801031E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491727E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12383E+01 0.20811E+01
   Friction velocity        uet   :  0.29074E-02 0.18913E+01
   Friction velocity        uk    :  0.29039E-02 0.18472E+01
   Dimensionless distance   yplus :  0.32336E-04 0.73959E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        717
   Nb of faces within the viscous sub-layer     :      32699
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27626E+00     104   0.15542E+00   0.14911E+01 0.94118E+02 
c  Velocity[X]                                      0.44552E+00 
c  Velocity[Y]                                      0.48139E+00 
c  Velocity[Z]                                      0.56415E+00 
c  Pressure     0.90091E-02     774   0.17770E-02   0.14152E+00 0.55670E+03 
c  k            0.10264E-01      60   0.12872E-02   0.14095E-03 0.10935E+03 
c  epsilon      0.94250E+02      49   0.22866E-02   0.87080E+04 0.42088E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.446e-05                            16
a  epsilon         -1.5575                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4388          4.9038         0.30826        0.048461
v  Velocity[Y]            -4.1565          4.9169         0.13925          0.1178
v  Velocity[Z]            -7.0749          7.0165        -0.11911     -0.00040547
v  ǁVelocityǁ          8.0679e-06          8.2906         0.88551          1.0068
v  Pressure                -13685           10577          6413.4          5622.3
v  k                   2.5645e-09         0.58122       0.0028776        0.004759
v  epsilon             4.0814e-05           23661          11.415          2.2461
v  TurbVisc            2.4573e-13         0.11253      0.00038861       0.0043736
v  total_pressure      4.8632e+05      5.1058e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               81:        0.78461E+02

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


 INSTANT    0.820000000E+02   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        -0.294758289E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491687E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11207E+01 0.20839E+01
   Friction velocity        uet   :  0.34703E-02 0.18920E+01
   Friction velocity        uk    :  0.34661E-02 0.18480E+01
   Dimensionless distance   yplus :  0.32330E-04 0.73921E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        722
   Nb of faces within the viscous sub-layer     :      32699
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27636E+00     106   0.15759E+00   0.14814E+01 0.93726E+02 
c  Velocity[X]                                      0.45724E+00 
c  Velocity[Y]                                      0.45643E+00 
c  Velocity[Z]                                      0.56769E+00 
c  Pressure     0.90366E-02     620   0.18066E-02   0.14220E+00 0.55014E+03 
c  k            0.10264E-01      58   0.14035E-02   0.29631E-03 0.35073E+03 
c  epsilon      0.94445E+02      42   0.24309E-02   0.21274E+06 0.50908E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippin===============================================================


 INSTANT    0.840000000E+02   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        -0.138545692E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12217E+01 0.20866E+01
   Friction velocity        uet   :  0.33991E-02 0.18978E+01
   Friction velocity        uk    :  0.33949E-02 0.18534E+01
   Dimensionless distance   yplus :  0.32359E-04 0.73757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        718
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27621E+00     105   0.15724E+00   0.14563E+01 0.92107E+02 
c  Velocity[X]                                      0.44729E+00 
c  Velocity[Y]                                      0.45718E+00 
c  Velocity[Z]                                      0.55182E+00 
c  Pressure     0.89973E-02     609   0.17920E-02   0.14141E+00 0.10366E+04 
c  k            0.10270E-01      58   0.15674E-02   0.27696E-03 0.21144E+03 
c  epsilon      0.94589E+02      41   0.24494E-02   0.34906E+05 0.11959E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3014e-05                            16
a  epsilon         -1.7057                            32


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4357          4.9966         0.30872        0.048474
v  Velocity[Y]            -4.1318          4.9213         0.13908         0.11783
v  Velocity[Z]             -7.127           6.748        -0.11947     -0.00032716
v  ǁVelocityǁ          8.0895e-06          8.4303          0.8871          1.0069
v  Pressure                -13888           10568          6405.1          5617.1
v  k                    8.034e-09         0.58545       0.0028764       0.0047567
v  epsilon             4.0777e-05           23849          11.473          2.2475
v  TurbVisc            2.4495e-13         0.11253      0.00038299       0.0043715
v  total_pressure      4.8611e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               84:        0.75235E+02

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


 INSTANT    0.850000000E+02   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         0.173678813E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------===============================================================


 INSTANT    0.840000000E+02   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        -0.138545692E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491730E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12217E+01 0.20866E+01
   Friction velocity        uet   :  0.33991E-02 0.18978E+01
   Friction velocity        uk    :  0.33949E-02 0.18534E+01
   Dimensionless distance   yplus :  0.32359E-04 0.73757E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        718
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27621E+00     105   0.15724E+00   0.14563E+01 0.92107E+02 
c  Velocity[X]                                      0.44729E+00 
c  Velocity[Y]                                      0.45718E+00 
c  Velocity[Z]                                      0.55182E+00 
c  Pressure     0.89973E-02     609   0.17920E-02   0.14141E+00 0.10366E+04 
c  k            0.10270E-01      58   0.15674E-02   0.27696E-03 0.21144E+03 
c  epsilon      0.94589E+02 v  total_pressure      4.8604e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               85:        0.70291E+02

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


 INSTANT    0.860000000E+02   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         0.921283293E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491725E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12296E+01 0.20876E+01
   Friction velocity        uet   :  0.42870E-02 0.18958E+01
   Friction velocity        uk    :  0.42816E-02 0.18517E+01
   Dimensionless distance   yplus :  0.32335E-04 0.73216E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        718
   Nb of faces within the viscous sub-layer     :      32704
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27616E+00     104   0.15999E+00   0.14334E+01 0.91979E+02 
c  Velocity[X]                                      0.46038E+00 
c  Velocity[Y]                                      0.46433E+00 
c  Velocity[Z]                                      0.50871E+00 
c  Pressure     0.89543E-02     588   0.18888E-02   0.14061E+00 0.38864E+03 
c  k            0.10270E-01      57   0.12899E-02   0.16470E-03 0.27041E+03 
c  epsilon      0.94816E+02      40   0.24076E-02   0.10182E+06 0.35683E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5514e-05                            17
a  epsilon         -1.8948                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4256          4.9409         0.30894        0.048444
v  Velocity[Y]            -4.1703          5.0365         0.13899         0.11783
v  Velocity[Z]            -7.1923          7.6122        -0.11969     -0.00030095
v  ǁVelocityǁ           8.091e-06           8.473         0.88807           1.007
v  Pressure                -14049           10574          6407.3            5620
v  k                   7.4625e-09          0.5864       0.0028769       0.0047562
v  epsilon             4.2251e-05           23881          11.554          2.2475
v  TurbVisc            2.4447e-13         0.11253      0.00037955       0.0043703
v  total_pressure      4.8595e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               86:        0.77128E+02

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


 INSTANT    0.870000000E+02   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         0.790301122E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective 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  total_pressure      4.8604e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               85:        0.67040E+02

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


 INSTANT    0.860000000E+02   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         0.921283293E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491725E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12296E+01 0.20876E+01
   Friction velocity        uet   :  0.42870E-02 0.18958E+01
   Friction velocity        uk    :  0.42816E-02 0.18517E+01
   Dimensionless distance   yplus :  0.32335E-04 0.73216E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        718
   Nb of faces within the viscous sub-layer     :      32704
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27616E+00     104   0.15999E+00   0.14334E+01 0.91979E+02 
c  Velocity[X]                                      0.46038E+00 
c  Velocity[Y]                                      0.46433E+00 
c  Velocity[Z]                                      0.50871E+00 
c  Pressure     0.v  epsilon             4.0858e-05           23719          11.495          2.2492
v  TurbVisc            2.4425e-13         0.11253        0.000378       0.0043697
v  total_pressure       4.859e+05      5.1058e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               87:        0.80590E+02

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


 INSTANT    0.880000000E+02   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        -0.122781927E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491727E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11079E+01 0.20864E+01
   Friction velocity        uet   :  0.63846E-02 0.18967E+01
   Friction velocity        uk    :  0.63766E-02 0.18525E+01
   Dimensionless distance   yplus :  0.32322E-04 0.72917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        713
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27593E+00     104   0.15847E+00   0.14777E+01 0.92894E+02 
c  Velocity[X]                                      0.45611E+00 
c  Velocity[Y]                                      0.46486E+00 
c  Velocity[Z]                                      0.55677E+00 
c  Pressure     0.88765E-02     533   0.18056E-02   0.13999E+00 0.39907E+03 
c  k            0.10266E-01      55   0.14395E-02   0.15702E-03 0.11857E+03 
c  epsilon      0.94518E+02      39   0.23176E-02   0.98030E+04 0.63249E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5145e-05                            17
a  epsilon         -1.7975                            31


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4428          5.0054         0.30901        0.048454
v  Velocity[Y]            -4.1505          5.0034         0.13884         0.11782
v  Velocity[Z]            -7.2054          6.7465        -0.11981     -0.00031353
v  ǁVelocityǁ          8.0403e-06          8.4345         0.88881          1.0071
v  Pressure                -14164           10572          6403.4            5618
v  k                   8.7451e-09         0.58554       0.0028713        0.004755
v  epsilon             2.8569e-05           23866          11.461          2.2466
v  TurbVisc            2.4391e-13         0.11253      0.00037653       0.0043693
v  total_pressure      4.8584e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               88:        0.68479E+02

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


 INSTANT    0.890000000E+02   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        -0.150430058E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491723E+00
Free inlet               13           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  epsilon             4.0858e-05           23719          11.495          2.2492
v  TurbVisc            2.4425e-13         0.11253        0.000378       0.0043697
v  total_pressure       4.859e+05      5.1058e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               87:        0.74643E+02

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


 INSTANT    0.880000000E+02   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        -0.122781927E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491727E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11079E+01 0.20864E+01
   Friction velocity        uet   :  0.63846E-02 0.18967E+01
   Friction velocity        uk    :  0.63766E-02 0.18525E+01
   Dimensionless distance   yplus :  0.32322E-04 0.72917E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        713
   Nb of faces within the viscous sub-layer     :      32711
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27593E+00     104   0.15847E+00   0.14777E+01 0.92894E+02 
c  Velocity[X]                                   v  Pressure                -14248           10583          6411.2          5623.6
v  k                   1.0963e-08         0.58128       0.0028768        0.004755
v  epsilon             3.9863e-05           23726          11.554          2.2498
v  TurbVisc            2.4356e-13         0.11253      0.00037515       0.0043686
v  total_pressure      4.8575e+05      5.1058e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               89:        0.65220E+02

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


 INSTANT    0.900000000E+02   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        -0.222105929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491708E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12030E+01 0.20840E+01
   Friction velocity        uet   :  0.69315E-02 0.18954E+01
   Friction velocity        uk    :  0.69226E-02 0.18512E+01
   Dimensionless distance   yplus :  0.32331E-04 0.72752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27596E+00     103   0.15648E+00   0.14077E+01 0.91553E+02 
c  Velocity[X]                                      0.44989E+00 
c  Velocity[Y]                                      0.42646E+00 
c  Velocity[Z]                                      0.53135E+00 
c  Pressure     0.83599E-02     576   0.16994E-02   0.13186E+00 0.69743E+03 
c  k            0.10279E-01      61   0.14779E-02   0.20341E-03 0.24261E+03 
c  epsilon      0.94648E+02      45   0.26518E-02   0.70445E+05 0.28257E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3206e-05                            17
a  epsilon         -1.8462                            30


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4334          4.9756         0.30905        0.048471
v  Velocity[Y]            -4.1502          4.9111         0.13875         0.11778
v  Velocity[Z]              -7.07           7.844        -0.11996     -0.00029579
v  ǁVelocityǁ          8.0914e-06          8.5032         0.88942          1.0072
v  Pressure                -14271           10575          6402.3          5617.6
v  k                   1.1378e-09         0.58509       0.0028719       0.0047548
v  epsilon             4.0744e-05           23799          11.482          2.2494
v  TurbVisc            2.4327e-13         0.11253      0.00037386       0.0043681
v  total_pressure      4.8573e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               90:        0.69586E+02

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


 INSTANT    0.910000000E+02   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.901275082E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491728E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15 v  Pressure                -14248           10583          6411.2          5623.6
v  k                   1.0963e-08         0.58128       0.0028768        0.004755
v  epsilon             3.9863e-05           23726          11.554          2.2498
v  TurbVisc            2.4356e-13         0.11253      0.00037515       0.0043686
v  total_pressure      4.8575e+05      5.1058e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               89:        0.63388E+02

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


 INSTANT    0.900000000E+02   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        -0.222105929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491708E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12030E+01 0.20840E+01
   Friction velocity        uet   :  0.69315E-02 0.18954E+01
   Friction velocity        uk    :  0.69226E-02 0.18512E+01
   Dimensionless distance   yplus :  0.32331E-04 0.72752E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        709
   Nb of faces within the viscous sub-layer     :      32709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------v  Velocity[Z]            -7.0716          7.8158        -0.12004     -0.00032423
v  ǁVelocityǁ          8.0548e-06          8.3048         0.88968          1.0073
v  Pressure                -14313           10585          6410.4            5623
v  k                   7.5934e-09          0.5822       0.0028694       0.0047545
v  epsilon              4.164e-05           23692          11.457           2.249
v  TurbVisc            3.6368e-14         0.11253      0.00037264       0.0043677
v  total_pressure      4.8569e+05      5.1059e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               91:        0.71399E+02

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


 INSTANT    0.920000000E+02   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        -0.145018539E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491728E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12313E+01 0.20817E+01
   Friction velocity        uet   :  0.46296E-02 0.18913E+01
   Friction velocity        uk    :  0.46238E-02 0.18474E+01
   Dimensionless distance   yplus :  0.32311E-04 0.72651E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        711
   Nb of faces within the viscous sub-layer     :      32709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27607E+00     103   0.15802E+00   0.14448E+01 0.92279E+02 
c  Velocity[X]                                      0.44877E+00 
c  Velocity[Y]                                      0.45770E+00 
c  Velocity[Z]                                      0.53828E+00 
c  Pressure     0.85763E-02     586   0.17402E-02   0.13504E+00 0.81683E+03 
c  k            0.10279E-01      57   0.12693E-02   0.16349E-03 0.25929E+03 
c  epsilon      0.94865E+02      43   0.25967E-02   0.88781E+05 0.32899E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.7225e-05                            15
a  epsilon         -1.8736                            32


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4341          4.9708         0.30905        0.048525
v  Velocity[Y]            -4.1732          5.0263         0.13876         0.11782
v  Velocity[Z]            -7.2936          7.6831        -0.12016      -0.0003229
v  ǁVelocityǁ          8.0597e-06          8.5381         0.89002          1.0073
v  Pressure                -14370           10574          6404.6          5619.5
v  k                   4.1321e-09         0.58555       0.0028711       0.0047541
v  epsilon             1.0508e-05           23745           11.54          2.2482
v  TurbVisc            2.4251e-13         0.11253      0.00037155       0.0043675
v  total_pressure      4.8563e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               92:        0.63096E+02

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


 INSTANT    0.930000000E+02   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        -0.847004757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.0000v  Velocity[Z]            -7.0716          7.8158        -0.12004     -0.00032423
v  ǁVelocityǁ          8.0548e-06          8.3048         0.88968          1.0073
v  Pressure                -14313           10585          6410.4            5623
v  k                   7.5934e-09          0.5822       0.0028694       0.0047545
v  epsilon              4.164e-05           23692          11.457           2.249
v  TurbVisc            3.6368e-14         0.11253      0.00037264       0.0043677
v  total_pressure      4.8569e+05      5.1059e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               91:        0.74677E+02

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


 INSTANT    0.920000000E+02   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        -0.145018539E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491728E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12313E+01 0.20817E+01
   Friction velocity        uet   :  0.46296E-02 0.18913E+01
   Friction velocity        uk    :  0.46238E-02 0.18474E+01
   Dimensionless distance   yplus :  0.32311E-04 0.72651E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        711
   Nb of faces within the viscous sub-layer     :      32709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27607E+00     103   0.15802E+00   0.14448E+01 0.92279E+02 
c  Velocity[X]                                      0.44877E+00 
c  Velocity[Y]                                      0.45770E+00 
c  Velocity[Z]                                      0.53828E+00 
c  Pressure     0.85763E-02     586   0.17402E-02   0.13504E+00 0.81683E+03 
c  k            0.10279E-01      57   0.12693E-02   0.16349E-03 0.25929E+03 
c  epsilon      0.94865E+02      43   0.25967E-02   0.88781E+05 0.32899E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.7225e-05                            15
a  epsilon         -1.8736                            32


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4341          4.9708         0.30905        0.048525
v  Velocity[Y]            -4.1732          5.0263         0.13876         0.11782
v  Velocity[Z]            -7.2936          7.6831        -0.12016      -0.0003229
v  ǁVelocityǁ          8.0597e-06          8.5381         0.89002          1.0073
v  Pressure                -14370           10574          6404.6          5619.5
v  k                   4.1321e-09         0.58555       0.0028711       0.0047541
v  epsilon             1.0508e-05           23745           11.54          2.2482
v  TurbVisc            2.4251e-13         0.11253      0.00037155       0.0043675
v  total_pressure      4.8563e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               92:        0.71346E+02

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


 INSTANT    0.930000000E+02   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        -0.847004757E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491697E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12360E+01 0.20817E+01
   Friction velocity        uet   :  0.45296E-02 0.18899E+01
   Friction velocity        uk    :  0.45240E-02 0.18460E+01
   Dimensionless distance   yplus :  0.32334E-04 0.73115E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        698
   Nb of faces within the viscous sub-layer     :      32702
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27594E+00     102   0.15606E+00   0.14244E+01 0.91337E+02 
c  Velocity[X]                                      0.44119E+00 
c  Velocity[Y]                                      0.43747E+00 
c  Velocity[Z]                                      0.54573E+00 
c  Pressure     0.84822E-02     534   0.16768E-02   0.13357E+00 0.13198E+03 
c  k            0.10289E-01      55   0.13624E-02   0.16290E-03 0.23121E+03 
c  epsilon      0.95012E+02      39   0.24780E-02   0.68479E+05 0.28653E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2726e-05                            15
a  epsilon         -1.5678                            33


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4468          4.9314           0.309        0.048482
v  Velocity[Y]            -4.1126          4.9413         0.13876         0.11787
v  Velocity[Z]            -7.0964          7.0711         -0.1202     -0.00036888
v  ǁVelocityǁ          8.0611e-06            8.27          0.8902          1.0074
v  Pressure                -14417           10574          6405.1          5619.7
v  k                   6.5562e-09         0.58028       0.0028698       0.0047543
v  epsilon              3.345e-05           23688          11.476            2.25
v  TurbVisc            2.4219e-13         0.11253      0.00037048       0.0043672
v  total_pressure      4.8558e+05      5.1057e+05      5.0641e+05      5.0562e+05


 TIME FOR THE TIME STEP               93:        0.66509E+02

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


 INSTANT    0.940000000E+02   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000         0.109017320E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491696E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11371E+01 0.20870E+01
   Friction velocity        uet   :  0.38985E-02 0.18958E+01
   Friction velocity        uk    :  0.38936E-02 0.18517E+01
   Dimensionless distance   yplus :  0.32330E-04 0.72666E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        705
   Nb of faces within the viscous sub-layer     :      32699
   Total number of wall faces                   :      4
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4269          4.9971         0.30897        0.048485
v  Velocity[Y]            -4.1528          5.0383         0.13876         0.11784
v  Velocity[Z]            -7.1527           6.879        -0.12035     -0.00035977
v  ǁVelocityǁ          8.1061e-06          8.2885         0.89068          1.0075
v  Pressure                -14509           10576          6404.6          5619.7
v  k                   3.7692e-09          0.5824       0.0028686       0.0047547
v  epsilon             2.5193e-05           23767          11.467          2.2498
v  TurbVisc            2.8607e-14         0.11253      0.00036873       0.0043669
v  total_pressure      4.8549e+05      5.1058e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               95:        0.54031E+02

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


 INSTANT    0.960000000E+02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.196154665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11835E+01 0.20857E+01
   Friction velocity        uet   :  0.68320E-02 0.18973E+01
   Friction velocity        uk    :  0.68233E-02 0.18530E+01
   Dimensionless distance   yplus :  0.32422E-04 0.72496E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        705
   Nb of faces within the viscous sub-layer     :      32701
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27585E+00     102   0.15903E+00   0.14626E+01 0.92790E+02 
c  Velocity[X]                                      0.46514E+00 
c  Velocity[Y]                                      0.44468E+00 
c  Velocity[Z]                                      0.55273E+00 
c  Pressure     0.84483E-02     665   0.16829E-02   0.13334E+00 0.94647E+03 
c  k            0.10282E-01      53   0.21584E-02   0.40792E-03 0.21600E+03 
c  epsilon      0.94891E+02      36   0.42410E-02   0.51346E+05 0.99917E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.375e-05                            17
a  epsilon         -1.9172                            27


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4355          4.9748          0.3089        0.048491
v  Velocity[Y]            -4.1052           4.924         0.13873         0.11783
v  Velocity[Z]            -7.1659          7.6229        -0.12039     -0.00028856
v  ǁVelocityǁ          8.0823e-06          8.4887         0.89077          1.0075
v  Pressure                -14568           10554          6392.6          5611.1
v  k                   1.5116e-09         0.58577       0.0028713        0.004755
v  epsilon             1.4844e-05           23813          11.504          2.2527
v  TurbVisc            2.4103e-13         0.11253      0.00036794       0.0043668
v  total_pressure      4.8543e+05      5.1055e+05      5.0639e+05      5.0561e+05


 TIME FOR THE TIME STEP               96:        0.69442E+02

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


 INSTANT    0.970000000E+02   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces  
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4269          4.9971         0.30897        0.048485
v  Velocity[Y]            -4.1528          5.0383         0.13876         0.11784
v  Velocity[Z]            -7.1527           6.879        -0.12035     -0.00035977
v  ǁVelocityǁ          8.1061e-06          8.2885         0.89068          1.0075
v  Pressure                -14509           10576          6404.6          5619.7
v  k                   3.7692e-09          0.5824       0.0028686       0.0047547
v  epsilon             2.5193e-05           23767          11.467          2.2498
v  TurbVisc            2.8607e-14         0.11253      0.00036873       0.0043669
v  total_pressure      4.8549e+05      5.1058e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               95:        0.60257E+02

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


 INSTANT    0.960000000E+02   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.442491710E+00
Smooth wall               5       41000        -0.196154665E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491724E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11835E+01 0.20857E+01
   Friction velocity        uet   :  0.68320E-02 0.18973E+01
   Friction velocity        uk    :  0.68233E-02 0.18530E+01
   Dimensionless distance   yplus :  0.32422E-04 0.72496E+01
   ------------------------------------------------------
  a  k           -3.1527e-05                            16
a  epsilon         -1.4458                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4518          4.9883         0.30887         0.04854
v  Velocity[Y]            -4.1725          5.0193          0.1387          0.1178
v  Velocity[Z]            -7.1069           7.488        -0.12048     -0.00032803
v  ǁVelocityǁ          8.0562e-06          8.2784         0.89092          1.0075
v  Pressure                -14621           10567          6404.2          5619.3
v  k                   1.6268e-09         0.58092       0.0028745        0.004754
v  epsilon             1.7268e-05           23786          11.673          2.2512
v  TurbVisc            1.6076e-13         0.11253      0.00036734       0.0043669
v  total_pressure      4.8538e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               97:        0.80244E+02

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


 INSTANT    0.980000000E+02   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        -0.725565608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491691E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11488E+01 0.20877E+01
   Friction velocity        uet   :  0.38367E-02 0.18937E+01
   Friction velocity        uk    :  0.38321E-02 0.18497E+01
   Dimensionless distance   yplus :  0.32321E-04 0.72543E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        711
   Nb of faces within the viscous sub-layer     :      32695
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27600E+00     103   0.15693E+00   0.14445E+01 0.91815E+02 
c  Velocity[X]                                      0.45461E+00 
c  Velocity[Y]                                      0.45499E+00 
c  Velocity[Z]                                      0.53491E+00 
c  Pressure     0.85320E-02     568   0.16945E-02   0.13488E+00 0.20472E+03 
c  k            0.10288E-01      55   0.12848E-02   0.19841E-03 0.30384E+03 
c  epsilon      0.95154E+02      38   0.32629E-02   0.19060E+06 0.48444E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.647e-05                            14
a  epsilon         -1.9525                            30


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4309          5.0199         0.30883        0.048494
v  Velocity[Y]            -4.1731          5.0122         0.13872         0.11774
v  Velocity[Z]            -7.2487          7.2863         -0.1205     -0.00033405
v  ǁVelocityǁ          8.0895e-06          8.4928          0.8911          1.0077
v  Pressure                -14675           10551          6403.3          5619.1
v  k                   7.9533e-09         0.58534       0.0028743       0.0047554
v  epsilon              1.152e-05           23892          11.543           2.253
v  TurbVisc            1.5469e-13         0.11253      0.00036659       0.0043665
v  total_pressure      4.8533e+05      5.1055e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               98:        0.74190E+02

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


 INSTANT    0.990000000E+02   TIME STEP NUMBER              99
 ============================================================= 




   *a  k           -3.1527e-05                            16
a  epsilon         -1.4458                            29


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4518          4.9883         0.30887         0.04854
v  Velocity[Y]            -4.1725          5.0193          0.1387          0.1178
v  Velocity[Z]            -7.1069           7.488        -0.12048     -0.00032803
v  ǁVelocityǁ          8.0562e-06          8.2784         0.89092          1.0075
v  Pressure                -14621           10567          6404.2          5619.3
v  k                   1.6268e-09         0.58092       0.0028745        0.004754
v  epsilon             1.7268e-05           23786          11.673          2.2512
v  TurbVisc            1.6076e-13         0.11253      0.00036734       0.0043669
v  total_pressure      4.8538e+05      5.1057e+05       5.064e+05      5.0562e+05


 TIME FOR THE TIME STEP               97:        0.73855E+02

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


 INSTANT    0.980000000E+02   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        -0.725565608E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491691E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11488E+01 0.20877E+01
   Friction velocity        uet   :  0.38367E-02 0.18937E+01
   Friction velocity        uk    :  0.
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2313e-05                            15
a  epsilon         -1.5302                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4559          5.0002         0.30879        0.048498
v  Velocity[Y]            -4.1175          4.9599         0.13878         0.11779
v  Velocity[Z]            -7.0505          7.2595        -0.12051     -0.00037077
v  ǁVelocityǁ          8.1167e-06           8.216         0.89113          1.0077
v  Pressure                -14763           10551          6398.6          5614.3
v  k                    6.661e-09         0.58258       0.0028732       0.0047552
v  epsilon              1.489e-05           23714          11.506          2.2539
v  TurbVisc            2.3982e-13         0.11253      0.00036609       0.0043663
v  total_pressure      4.8524e+05      5.1055e+05       5.064e+05      5.0561e+05


 TIME FOR THE TIME STEP               99:        0.70741E+02

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


 INSTANT    0.100000000E+03   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        -0.369724866E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491727E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11117E+01 0.20866E+01
   Friction velocity        uet   :  0.64298E-02 0.18966E+01
   Friction velocity        uk    :  0.64216E-02 0.18524E+01
   Dimensionless distance   yplus :  0.32445E-04 0.72443E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        712
   Nb of faces within the viscous sub-layer     :      32706
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27605E+00     100   0.15855E+00   0.14169E+01 0.91249E+02 
c  Velocity[X]                                      0.44744E+00 
c  Velocity[Y]                                      0.44901E+00 
c  Velocity[Z]                                      0.52049E+00 
c  Pressure     0.82422E-02     792   0.18061E-02   0.12991E+00 0.86754E+03 
c  k            0.10289E-01      53   0.15378E-02   0.11717E-03 0.85116E+02 
c  epsilon      0.95398E+02      36   0.21501E-02   0.55211E+04 0.42255E+03 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.4893e-05                            17
a  epsilon         -1.7677                            33


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4333          5.0392         0.30871        0.048538
v  Velocity[Y]            -4.1612          5.0333         0.13874         0.11779
v  Velocity[Z]            -7.0456          7.6471        -0.12048     -0.00027021
v  ǁVelocityǁ          8.1154e-06           8.464         0.89125          1.0077
v  Pressure                -14753           10550          6392.2          5610.3
v  k                   5.0907e-10         0.58602       0.0028719       0.0047549
v  epsilon             8.6843e-06           23869          11.507          2.2519
v  TurbVisc            2.3935e-13         0.11253       0.0003656       0.0043662
v  total_pressure      4.8525e+05      5.1055e+05      5.0639e+05      5.0561e+05


 TIME FOR THE TIME STEP              100:        0.70673E+02

==========================================================
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2313e-05                            15
a  epsilon         -1.5302                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4559          5.0002         0.30879        0.048498
v  Velocity[Y]            -4.1175          4.9599         0.13878         0.11779
v  Velocity[Z]            -7.0505          7.2595        -0.12051     -0.00037077
v  ǁVelocityǁ          8.1167e-06           8.216         0.89113          1.0077
v  Pressure                -14763           10551          6398.6          5614.3
v  k                    6.661e-09         0.58258       0.0028732       0.0047552
v  epsilon              1.489e-05           23714          11.506          2.2539
v  TurbVisc            2.3982e-13         0.11253      0.00036609       0.0043663
v  total_pressure      4.8524e+05      5.1055e+05       5.064e+05      5.0561e+05


 TIME FOR THE TIME STEP               99:        0.67331E+02

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


 INSTANT    0.100000000E+03   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        -0.369724866E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.442491727E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6658e-05                             7
a  epsilon         -1.0436                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4393          13.645         0.36824        0.078226
v  Velocity[Y]            -14.133           8.494         0.22953         0.18921
v  Velocity[Z]            -14.759          13.337        -0.12827     -0.00083285
v  ǁVelocityǁ          8.1213e-06          21.549          1.0472          1.5274
v  Pressure               -2919.5           41374           24527           22155
v  k                   7.8647e-09         0.57597        0.002952       0.0055398
v  epsilon             2.6732e-05           23319          11.745          2.3387
v  TurbVisc            9.0681e-15         0.11253      0.00036509        0.004366
v  total_pressure      4.9708e+05      5.4137e+05      5.2453e+05      5.2215e+05


 TIME FOR THE TIME STEP              101:        0.99186E+02

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


 INSTANT    0.102000000E+03   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         0.151780377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640842E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16312E+02 0.21651E+01
   Friction velocity        uet   :  0.84567E-02 0.19792E+01
   Friction velocity        uk    :  0.84458E-02 0.20127E+01
   Dimensionless distance   yplus :  0.32462E-04 0.10474E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2894
   Nb of faces within the viscous sub-layer     :      29534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63342E+00     149   0.15283E+00   0.13562E+03 0.62404E+03 
c  Velocity[X]                                      0.27738E+02 
c  Velocity[Y]                                      0.43165E+02 
c  Velocity[Z]                                      0.64721E+02 
c  Pressure     0.67044E-01    1140   0.13288E+00   0.72447E+00 0.25305E+06 
c  k            0.21024E-01      94   0.28270E-01   0.53875E+00 0.59435E+04 
c  epsilon      0.51837E+03      68   0.71906E-01   0.59287E+09 0.19793E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon       -0.044557                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7645          7.9414         0.38528        0.077844
v  Velocity[Y]            -7.0495          11.595         0.23216          0.1856
v  Velocity[Z]            -14.437          10.279        -0.13879     -0.00099265
v  ǁVelocityǁ          8.2578e-06          15.623          1.0866          1.5069
v  Pressure                -14506           25406           16701           13972
v  k                   3.6413e-08          2.4678       0.0047645       0.0077409
v  epsilon             2.5515e-05      1.2404e+05           25.76          5.7234
v  TurbVisc            2.3842e-13         0.13762      0.00039744       0.0053459
v  total_pressure      4.8549e+05      5.2541e+05       5.167e+05      5.1397e+05


 TIME FOR T-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6658e-05                             7
a  epsilon         -1.0436                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.4393          13.645         0.36824        0.078226
v  Velocity[Y]            -14.133           8.494         0.22953         0.18921
v  Velocity[Z]            -14.759          13.337        -0.12827     -0.00083285
v  ǁVelocityǁ          8.1213e-06          21.549          1.0472          1.5274
v  Pressure               -2919.5           41374           24527           22155
v  k                   7.8647e-09         0.57597        0.002952       0.0055398
v  epsilon             2.6732e-05           23319          11.745          2.3387
v  TurbVisc            9.0681e-15         0.11253      0.00036509        0.004366
v  total_pressure      4.9708e+05      5.4137e+05      5.2453e+05      5.2215e+05


 TIME FOR THE TIME STEP              101:        0.75475E+02

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


 INSTANT    0.102000000E+03   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         0.151780377E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640842E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------c  k            0.22190E-01      80   0.11320E+00   0.17403E+00 0.29584E+04 
c  epsilon      0.60256E+03      50   0.36956E+00   0.21795E+09 0.28664E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00042187                            39
a  epsilon         -7.5543                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4587          7.6312         0.39816        0.078237
v  Velocity[Y]            -6.9082          12.364         0.23101          0.1863
v  Velocity[Z]            -15.485          12.177        -0.14405     -0.00032068
v  ǁVelocityǁ          8.4127e-06           16.28          1.1208           1.521
v  Pressure                -18573           24249           15917           13468
v  k                   9.0022e-09         0.77978       0.0041357       0.0072804
v  epsilon             2.4349e-05           29996          21.068          3.9719
v  TurbVisc            2.3803e-13         0.14109      0.00040712       0.0056328
v  total_pressure      4.8143e+05      5.2425e+05      5.1592e+05      5.1347e+05


 TIME FOR THE TIME STEP              103:        0.83196E+02

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


 INSTANT    0.104000000E+03   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.133043276E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640800E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92732E+01 0.22843E+01
   Friction velocity        uet   :  0.48650E-02 0.20908E+01
   Friction velocity        uk    :  0.48642E-02 0.20408E+01
   Dimensionless distance   yplus :  0.33029E-04 0.89532E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2744
   Nb of faces within the viscous sub-layer     :      30044
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59098E+00     136   0.14538E+00   0.50572E+02 0.43350E+03 
c  Velocity[X]                                      0.14173E+02 
c  Velocity[Y]                                      0.20399E+02 
c  Velocity[Z]                                      0.16000E+02 
c  Pressure     0.54139E-01     966   0.28257E-01   0.59339E+00 0.12519E+05 
c  k            0.20077E-01      78   0.13428E-01   0.23590E-01 0.15675E+04 
c  epsilon      0.35406E+03      56   0.48094E-01   0.17782E+08 0.16935E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011909                            47
a  epsilon         -2.5087                            31


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.8553          9.1297         0.40944        0.078294
v  Velocity[Y]            -7.7911          10.798         0.22721         0.18639
v  Velocity[Z]            -16.693          12.729        -0.14803     -0.00014395
v  ǁVelocityǁ          8.6513e-06          18.732          1.1511          1.5303
v  Pressure                -21425           24359           15881           13530
v  k                   3.0023e-09         0.82435       0.0043237       0.0074104
v  epsilon             2.5213e-06           44299          c  k            0.22190E-01      80   0.11320E+00   0.17403E+00 0.29584E+04 
c  epsilon      0.60256E+03      50   0.36956E+00   0.21795E+09 0.28664E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00042187                            39
a  epsilon         -7.5543                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.4587          7.6312         0.39816        0.078237
v  Velocity[Y]            -6.9082          12.364         0.23101          0.1863
v  Velocity[Z]            -15.485          12.177        -0.14405     -0.00032068
v  ǁVelocityǁ          8.4127e-06           16.28          1.1208           1.521
v  Pressure                -18573           24249           15917           13468
v  k                   9.0022e-09         0.77978       0.0041357       0.0072804
v  epsilon             2.4349e-05           29996          21.068          3.9719
v  TurbVisc            2.3803e-13         0.14109      0.00040712       0.0056328
v  total_pressure      4.8143e+05      5.2425e+05      5.1592e+05      5.1347e+05


 TIME FOR THE TIME STEP              103:        0.89255E+02

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


 INSTANT    0.104000000E+03   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.133043276E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640800E+00
Free inlet               13           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[Z]                                      0.13178E+02 
c  Pressure     0.54429E-01     718   0.27261E-01   0.57546E+00 0.55064E+04 
c  k            0.19717E-01      75   0.91067E-02   0.19020E-01 0.14196E+04 
c  epsilon      0.29260E+03      50   0.26685E-01   0.14817E+08 0.16789E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7735e-05                            40
a  epsilon       -0.028565                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.6115          10.826         0.41999        0.078236
v  Velocity[Y]             -8.798          9.3556         0.22303         0.18651
v  Velocity[Z]            -19.003          13.669        -0.15199     -4.1115e-05
v  ǁVelocityǁ          9.1089e-06          21.124          1.1798          1.5386
v  Pressure                -23456           24598           15959           13645
v  k                   3.1553e-10         0.91478        0.004548       0.0075289
v  epsilon             4.4874e-07           73822          26.788          4.0461
v  TurbVisc            2.3835e-13         0.14179      0.00039813       0.0060166
v  total_pressure      4.7654e+05       5.246e+05      5.1596e+05      5.1365e+05


 TIME FOR THE TIME STEP              105:        0.74571E+02

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


 INSTANT    0.106000000E+03   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.826910059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12711E+02 0.25622E+01
   Friction velocity        uet   :  0.15076E-01 0.22374E+01
   Friction velocity        uk    :  0.14992E-01 0.21988E+01
   Dimensionless distance   yplus :  0.34422E-04 0.95991E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2774
   Nb of faces within the viscous sub-layer     :      29990
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61756E+00     133   0.15232E+00   0.31332E+02 0.34144E+03 
c  Velocity[X]                                      0.85469E+01 
c  Velocity[Y]                                      0.11785E+02 
c  Velocity[Z]                                      0.11001E+02 
c  Pressure     0.54742E-01    1203   0.25000E-01   0.55758E+00 0.31275E+04 
c  k            0.19831E-01      72   0.73411E-02   0.17582E-01 0.14540E+04 
c  epsilon      0.28129E+03      56   0.20478E-01   0.17117E+08 0.15051E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.4178e-05                            24
a  epsilon      -0.0063395                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.6323          10.725         0.43026        0.078082
v  Velocity[Y]            -9.0669          9.5984         0.21898         0.18663
v  Velocity[Z]            -16.198          14.965        -0.15531     -2.9333e-05
v  ǁVelocityǁ          9.8147e-06          19.204          1.2077          1.5466
v  Pressure                -25215           24868           16044           13749c  Velocity[Z]                                      0.13178E+02 
c  Pressure     0.54429E-01     718   0.27261E-01   0.57546E+00 0.55064E+04 
c  k            0.19717E-01      75   0.91067E-02   0.19020E-01 0.14196E+04 
c  epsilon      0.29260E+03      50   0.26685E-01   0.14817E+08 0.16789E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7735e-05                            40
a  epsilon       -0.028565                            24


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.6115          10.826         0.41999        0.078236
v  Velocity[Y]             -8.798          9.3556         0.22303         0.18651
v  Velocity[Z]            -19.003          13.669        -0.15199     -4.1115e-05
v  ǁVelocityǁ          9.1089e-06          21.124          1.1798          1.5386
v  Pressure                -23456           24598           15959           13645
v  k                   3.1553e-10         0.91478        0.004548       0.0075289
v  epsilon             4.4874e-07           73822          26.788          4.0461
v  TurbVisc            2.3835e-13         0.14179      0.00039813       0.0060166
v  total_pressure      4.7654e+05       5.246e+05      5.1596e+05      5.1365e+05


 TIME FOR THE TIME STEP              105:        0.68212E+02

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


 INSTANT    0.106000000E+03   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.826910059E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15   c  Velocity     0.62786E+00     130   0.15573E+00   0.26749E+02 0.31312E+03 
c  Velocity[X]                                      0.72404E+01 
c  Velocity[Y]                                      0.10128E+02 
c  Velocity[Z]                                      0.93811E+01 
c  Pressure     0.55947E-01     820   0.23472E-01   0.55258E+00 0.30120E+04 
c  k            0.20064E-01      70   0.50513E-02   0.15535E-01 0.18235E+04 
c  epsilon      0.29315E+03      51   0.18327E-01   0.48524E+08 0.35582E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6163e-05                            11
a  epsilon       -0.024874                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7071          12.394         0.44048        0.077959
v  Velocity[Y]            -8.9725          9.3968         0.21582         0.18637
v  Velocity[Z]            -14.433          13.376        -0.15851     -0.00011387
v  ǁVelocityǁ          1.0481e-05           17.97          1.2353          1.5536
v  Pressure                -26941           24955           16014           13757
v  k                   6.7581e-10          1.4126       0.0050638       0.0076965
v  epsilon             1.3486e-06      1.6224e+05          35.451          4.2897
v  TurbVisc              2.41e-13         0.14181      0.00041256       0.0062191
v  total_pressure      4.7306e+05      5.2496e+05      5.1601e+05      5.1376e+05


 TIME FOR THE TIME STEP              107:        0.77774E+02

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


 INSTANT    0.108000000E+03   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        -0.246529543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640805E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78735E+01 0.31088E+01
   Friction velocity        uet   :  0.57856E-02 0.23230E+01
   Friction velocity        uk    :  0.57689E-02 0.23202E+01
   Dimensionless distance   yplus :  0.36857E-04 0.92903E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2809
   Nb of faces within the viscous sub-layer     :      29851
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63630E+00     127   0.16063E+00   0.23464E+02 0.29290E+03 
c  Velocity[X]                                      0.62987E+01 
c  Velocity[Y]                                      0.89935E+01 
c  Velocity[Z]                                      0.81719E+01 
c  Pressure     0.55927E-01     859   0.19418E-01   0.54223E+00 0.22386E+04 
c  k            0.20252E-01      69   0.43667E-02   0.11758E-01 0.11585E+04 
c  epsilon      0.30201E+03      52   0.14590E-01   0.13163E+08 0.16434E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.4382e-05                             9
a  epsilon       -0.037161                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.8229           9.105         0.45016        0.077844
v  Velocity[Y]            -9.0758          9.1328          0.2141         0.18633
v  Velocity[Z]             -13.64       c  Velocity     0.62786E+00     130   0.15573E+00   0.26749E+02 0.31312E+03 
c  Velocity[X]                                      0.72404E+01 
c  Velocity[Y]                                      0.10128E+02 
c  Velocity[Z]                                      0.93811E+01 
c  Pressure     0.55947E-01     820   0.23472E-01   0.55258E+00 0.30120E+04 
c  k            0.20064E-01      70   0.50513E-02   0.15535E-01 0.18235E+04 
c  epsilon      0.29315E+03      51   0.18327E-01   0.48524E+08 0.35582E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6163e-05                            11
a  epsilon       -0.024874                            14


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -2.7071          12.394         0.44048        0.077959
v  Velocity[Y]            -8.9725          9.3968         0.21582         0.18637
v  Velocity[Z]            -14.433          13.376        -0.15851     -0.00011387
v  ǁVelocityǁ          1.0481e-05           17.97          1.2353          1.5536
v  Pressure                -26941           24955           16014           13757
v  k                   6.7581e-10          1.4126       0.0050638       0.0076965
v  epsilon             1.3486e-06      1.6224e+05          35.451          4.2897
v  TurbVisc              2.41e-13         0.14181      0.00041256       0.0062191
v  total_pressure      4.7306e+05      5.2496e+05      5.1601e+05      5.1376e+05


 TIME FOR THE TIME STEP              107:        0.78574E+02

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


 INSTANT    0.108000000E+03   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        -0.246529543E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64265E+00     126   0.16035E+00   0.21029E+02 0.27784E+03 
c  Velocity[X]                                      0.56722E+01 
c  Velocity[Y]                                      0.83336E+01 
c  Velocity[Z]                                      0.70231E+01 
c  Pressure     0.54830E-01     980   0.15249E-01   0.52400E+00 0.21279E+04 
c  k            0.20392E-01      68   0.61899E-02   0.12815E-01 0.14157E+04 
c  epsilon      0.30789E+03      53   0.14425E-01   0.15696E+08 0.19006E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1155e-05                            10
a  epsilon       -0.012844                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.907          8.8889         0.45919        0.077741
v  Velocity[Y]            -8.9167           8.778         0.21406         0.18617
v  Velocity[Z]            -12.847          14.219        -0.16441     -0.00027918
v  ǁVelocityǁ          1.1182e-05          16.371          1.2881          1.5654
v  Pressure                -29646           24938           15875           13677
v  k                   7.2858e-09          1.3983       0.0055229       0.0078051
v  epsilon             2.9443e-06      1.4166e+05          40.794          4.5158
v  TurbVisc            2.4589e-13         0.14181      0.00042517       0.0063158
v  total_pressure      4.7035e+05      5.2494e+05      5.1587e+05      5.1368e+05


 TIME FOR THE TIME STEP              109:        0.79218E+02

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


 INSTANT    0.110000000E+03   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        -0.269761344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63798E+01 0.32594E+01
   Friction velocity        uet   :  0.68543E-02 0.23792E+01
   Friction velocity        uk    :  0.68335E-02 0.24285E+01
   Dimensionless distance   yplus :  0.37912E-04 0.93122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2870
   Nb of faces within the viscous sub-layer     :      29612
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64752E+00     126   0.16919E+00   0.19867E+02 0.26982E+03 
c  Velocity[X]                                      0.55558E+01 
c  Velocity[Y]                                      0.77275E+01 
c  Velocity[Z]                                      0.65837E+01 
c  Pressure     0.54215E-01     895   0.13166E-01   0.50904E+00 0.23747E+04 
c  k            0.20633E-01      69   0.54824E-02   0.13581E-01 0.13632E+04 
c  epsilon      0.32023E+03      53   0.12326E-01   0.15216E+08 0.15976E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.818e-05                             6
a  epsilon        -0.10262                            10


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0019          8.700   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64265E+00     126   0.16035E+00   0.21029E+02 0.27784E+03 
c  Velocity[X]                                      0.56722E+01 
c  Velocity[Y]                                      0.83336E+01 
c  Velocity[Z]                                      0.70231E+01 
c  Pressure     0.54830E-01     980   0.15249E-01   0.52400E+00 0.21279E+04 
c  k            0.20392E-01      68   0.61899E-02   0.12815E-01 0.14157E+04 
c  epsilon      0.30789E+03      53   0.14425E-01   0.15696E+08 0.19006E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1155e-05                            10
a  epsilon       -0.012844                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -2.907          8.8889         0.45919        0.077741
v  Velocity[Y]            -8.9167           8.778         0.21406         0.18617
v  Velocity[Z]            -12.847          14.219        -0.16441     -0.00027918
v  ǁVelocityǁ          1.1182e-05          16.371          1.2881          1.5654
v  Pressure                -29646           24938           15875           13677
v  k                   7.2858e-09          1.3983       0.0055229       0.0078051
v  epsilon             2.9443e-06      1.4166e+05          40.794          4.5158
v  TurbVisc            2.4589e-13         0.14181      0.00042517       0.0063158
v  total_pressure      4.7035e+05      5.2494e+05      5.1587e+05      5.1368e+05


 TIME FOR THE TIME STEP              109:        0.82952E+02

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


 INSTANT    0.110000000E+03   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        -0.269761344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63798E+01 0.32594E+01
   Friction velocity        uet   :  0.68543E-02 0.23792E+01
   Friction velocity        uk    :  0.68335E-02 0.24285E+01
   Dimensionless distance   yplus :  0.37912E-04 0.93122E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2870
   Nb of faces within the viscous sub-layer     :      29612
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64752E+00     126   0.16919E+00   0.19867E+02 0.26982E+03 
c  Velocity[X]                                      0.55558E+01 
c  Velocity[Y]                                      0.77275E+01 
c  Velocity[Z]                                      0.65837E+01 
c  Pressure     0.54215E-01     895   0.13166E-01   0.50904E+00 0.23747E+04 
c  k            0.20633E-01      69   0.54824E-02   0.13581E-01 0.13632E+04 
c  epsilon      0.32023E+03      53   0.12326E-01   0.15216E+08 0.15976E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.818e-05                             6
a  epsilon        -0.10262                            10


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0019          8.7004          0.4672        0.077535
v  Velocity[Y]            -8.7955          8.6244         0.21511         0.18628
v  Velocity[Z]            -12.807          15.497        -0.16763     -0.00035041
v  ǁVelocityǁ          1.1181e-05           15.98          1.3127          1.5701
v  Pressure                -30479           24923           15822           13644
v  k                   3.8659e-08          1.4692       0.0057807       0.0078511
v  epsilon             1.3112e-05      1.5125e+05          44.374          4.6451
v  TurbVisc            2.4924e-13         0.14181      0.00043116       0.0063436
v  total_pressure      4.6952e+05      5.2492e+05      5.1582e+05      5.1364e+05


 TIME FOR THE TIME STEP              110:        0.73549E+02

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


 INSTANT    0.111000000E+03   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.131361228E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74613E+01 0.32776E+01
   Friction velocity        uet   :  0.84197E-02 0.24019E+01
   Friction velocity        uk    :  0.83938E-02 0.24374E+01
   Dimensionless distance   yplus :  0.37817E-04 0.92367E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2904
   Nb of faces within the viscous sub-layer     :      29509
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65031E+00     127   0.16767E+00   0.19568E+02 0.26694E+03 
c  Velocity[X]                                      0.54074E+01 
c  Velocity[Y]                                      0.73261E+01 
c  Velocity[Z]                                      0.68345E+01 
c  Pressure     0.52958E-01     947   0.13225E-01   0.49428E+00 0.16149E+04 
c  k            0.20882E-01      69   0.37929E-02   0.12764E-01 0.12459E+04 
c  epsilon      0.32841E+03      58   0.89075E-02   0.84553E+07 0.10390E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.1733e-05                             6
a  epsilon       -0.052358                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.0671          9.1523         0.47404         0.07734
v  Velocity[Y]            -8.8658          8.4916         0.21695         0.18628
v  Velocity[Z]            -12.667          13.344        -0.17107     -0.00048586
v  ǁVelocityǁ          1.1057e-05          16.042          1.3359          1.5744
v  Pressure                -30864           25020           15752           13597
v  k                   3.9642e-08          1.4764       0.0060183       0.0078892
v  epsilon             1.7487e-05      1.5269e+05          47.541          4.7603
v  TurbVisc            2.5318e-13         0.14181      0.00043704       0.0063633
v  total_pressure      4.6914e+05      5.2502e+05      5.1575e+05       5.136e+05


 TIME FOR THE TIME STEP              111:        0.77272E+02

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


 INSTANT    0.112000000E+03   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Ma   Nb of faces within the viscous sub-layer     :      29286
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65360E+00     124   0.16493E+00   0.16974E+02 0.24553E+03 
c  Velocity[X]                                      0.46111E+01 
c  Velocity[Y]                                      0.64996E+01 
c  Velocity[Z]                                      0.58632E+01 
c  Pressure     0.51459E-01     714   0.13365E-01   0.47117E+00 0.20320E+04 
c  k            0.21267E-01      68   0.34835E-02   0.13037E-01 0.11510E+04 
c  epsilon      0.34507E+03      54   0.68374E-02   0.76097E+07 0.76836E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.2155e-05                             6
a  epsilon        -0.13105                            15


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2314          9.7205          0.4854        0.077092
v  Velocity[Y]            -8.4676          8.3455          0.2216         0.18663
v  Velocity[Z]            -12.488          13.499        -0.17933     -0.00052505
v  ǁVelocityǁ          1.0333e-05          15.867          1.3795          1.5822
v  Pressure                -31532           25476           15696           13572
v  k                   4.2652e-08          1.4949       0.0064766       0.0079539
v  epsilon             1.6331e-05      1.5682e+05          53.323          4.9727
v  TurbVisc             2.634e-13         0.14181      0.00044667       0.0063867
v  total_pressure      4.6847e+05      5.2548e+05       5.157e+05      5.1357e+05


 TIME FOR THE TIME STEP              113:        0.68216E+02

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


 INSTANT    0.114000000E+03   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        -0.143093508E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640801E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59365E+01 0.33284E+01
   Friction velocity        uet   :  0.92566E-02 0.25107E+01
   Friction velocity        uk    :  0.92278E-02 0.24782E+01
   Dimensionless distance   yplus :  0.36104E-04 0.89088E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3045
   Nb of faces within the viscous sub-layer     :      29140
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65588E+00     124   0.16980E+00   0.15327E+02 0.23325E+03 
c  Velocity[X]                                      0.40431E+01 
c  Velocity[Y]                                      0.58554E+01 
c  Velocity[Z]                                      0.54281E+01 
c  Pressure     0.50392E-01     781   0.12383E-01   0.45766E+00 0.10020E+04 
c  k            0.21488E-01      69   0.34638E-02   0.12265E-01 0.14371E+04 
c  epsilon      0.36029E+03      54   0.13935E-01   0.23811E+08 0.16601E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.8213e-05                             4
a    Nb of faces within the viscous sub-layer     :      29286
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65360E+00     124   0.16493E+00   0.16974E+02 0.24553E+03 
c  Velocity[X]                                      0.46111E+01 
c  Velocity[Y]                                      0.64996E+01 
c  Velocity[Z]                                      0.58632E+01 
c  Pressure     0.51459E-01     714   0.13365E-01   0.47117E+00 0.20320E+04 
c  k            0.21267E-01      68   0.34835E-02   0.13037E-01 0.11510E+04 
c  epsilon      0.34507E+03      54   0.68374E-02   0.76097E+07 0.76836E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.2155e-05                             6
a  epsilon        -0.13105                            15


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.2314          9.7205          0.4854        0.077092
v  Velocity[Y]            -8.4676          8.3455          0.2216         0.18663
v  Velocity[Z]            -12.488          13.499        -0.17933     -0.00052505
v  ǁVelocityǁ          1.0333e-05          15.867          1.3795          1.5822
v  Pressure                -31532           25476           15696           13572
v  k                   4.2652e-08          1.4949       0.0064766       0.0079539
v  epsilon             1.6331e-05      1.5682e+05          53.323          4.9727
v  TurbVisc             2.634e-13         0.14181      0.00044667       0.0063867
v  total_pressure      4.6847e+05      5.2548e+05       5.157e+05      5.1357e+05


 TIME FOR THE TIME STEP              113:        0.64141E+02

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


 INSTANT    0.114000000E+03   TIME STEP NUMBER             114
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.35687E-04 0.85429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3078
   Nb of faces within the viscous sub-layer     :      29013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65658E+00     122   0.17016E+00   0.14370E+02 0.22630E+03 
c  Velocity[X]                                      0.39747E+01 
c  Velocity[Y]                                      0.51525E+01 
c  Velocity[Z]                                      0.52429E+01 
c  Pressure     0.50179E-01     682   0.11442E-01   0.44966E+00 0.27494E+04 
c  k            0.21696E-01      68   0.32374E-02   0.10996E-01 0.12139E+04 
c  epsilon      0.37120E+03      54   0.76527E-02   0.85555E+07 0.83351E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.723e-05                             6
a  epsilon       -0.033955                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3433          9.7721         0.49469        0.077035
v  Velocity[Y]            -7.9775          8.2008         0.22617         0.18703
v  Velocity[Z]            -12.752          13.685        -0.18872     -0.00056167
v  ǁVelocityǁ          1.0228e-05          15.524          1.4182          1.5894
v  Pressure                -31756           25866           15706           13590
v  k                   4.8098e-08          1.4976        0.006917       0.0080131
v  epsilon             1.5336e-05      1.5759e+05          59.268          5.1709
v  TurbVisc            2.8113e-13         0.14181      0.00045471        0.006399
v  total_pressure      4.6824e+05      5.2587e+05      5.1571e+05      5.1359e+05


 TIME FOR THE TIME STEP              115:        0.71723E+02

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


 INSTANT    0.116000000E+03   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.231543524E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59377E+01 0.33161E+01
   Friction velocity        uet   :  0.10920E-01 0.25240E+01
   Friction velocity        uk    :  0.10885E-01 0.24673E+01
   Dimensionless distance   yplus :  0.35784E-04 0.84528E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3121
   Nb of faces within the viscous sub-layer     :      28902
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65750E+00     121   0.16931E+00   0.13014E+02 0.21578E+03 
c  Velocity[X]                                      0.35404E+01 
c  Velocity[Y]                                      0.48445E+01 
c  Velocity[Z]                                      0.46286E+01 
c  Pressure     0.50144E-01     700   0.10056E-01   0.44482E+00 0.54346E+03 
c  k            0.21966E-01      67   0.41959E-02   0.10210E-01 0.10903E+04 
c  epsilon      0.38613E+03      55   0.10627E-01   0.78331E+07 0.79734E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initia   Dimensionless distance   yplus :  0.35687E-04 0.85429E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3078
   Nb of faces within the viscous sub-layer     :      29013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65658E+00     122   0.17016E+00   0.14370E+02 0.22630E+03 
c  Velocity[X]                                      0.39747E+01 
c  Velocity[Y]                                      0.51525E+01 
c  Velocity[Z]                                      0.52429E+01 
c  Pressure     0.50179E-01     682   0.11442E-01   0.44966E+00 0.27494E+04 
c  k            0.21696E-01      68   0.32374E-02   0.10996E-01 0.12139E+04 
c  epsilon      0.37120E+03      54   0.76527E-02   0.85555E+07 0.83351E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -2.723e-05                             6
a  epsilon       -0.033955                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.3433          9.7721         0.49469        0.077035
v  Velocity[Y]            -7.9775          8.2008         0.22617         0.18703
v  Velocity[Z]            -12.752          13.685        -0.18872     -0.00056167
v  ǁVelocityǁ          1.0228e-05          15.524          1.4182          1.5894
v  Pressure                -31756           25866           15706           13590
v  k                   4.8098e-08          1.4976        0.006917       0.0080131
v  epsilon             1.5336e-05      1.5759e+05          59.268          5.1709
v  TurbVisc            2.8113e-13         0.14181      0.00045471        0.006399
v  total_pressure      4.6824e+05      5.2587e+05      5.1571e+05      5.1359e+05


 TIME FOR THE TIME STEP              115:        0.75501E+02

=========================   Rel velocity at the wall uiptn : -0.57569E+01 0.33374E+01
   Friction velocity        uet   :  0.96336E-02 0.24985E+01
   Friction velocity        uk    :  0.96034E-02 0.24869E+01
   Dimensionless distance   yplus :  0.35836E-04 0.83843E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3143
   Nb of faces within the viscous sub-layer     :      28774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65930E+00     121   0.16920E+00   0.12364E+02 0.20893E+03 
c  Velocity[X]                                      0.33752E+01 
c  Velocity[Y]                                      0.45222E+01 
c  Velocity[Z]                                      0.44670E+01 
c  Pressure     0.50204E-01     844   0.94892E-02   0.43814E+00 0.87295E+03 
c  k            0.22167E-01      72   0.58993E-02   0.17934E-01 0.17404E+04 
c  epsilon      0.40089E+03      59   0.15107E-01   0.37639E+08 0.20603E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2636e-05                             6
a  epsilon       -0.039015                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.5088          9.2618         0.50301        0.077126
v  Velocity[Y]            -7.7229          8.0083         0.23057         0.18715
v  Velocity[Z]            -13.007          11.701        -0.19847     -0.00063411
v  ǁVelocityǁ          1.0621e-05          15.692          1.4514          1.5961
v  Pressure                -32017           25984           15655           13572
v  k                   5.2891e-08          1.5637       0.0073541        0.008069
v  epsilon             1.4599e-05      1.5872e+05          66.918          5.3644
v  TurbVisc            3.1037e-13         0.14181      0.00046128       0.0064066
v  total_pressure      4.6798e+05      5.2598e+05      5.1565e+05      5.1357e+05


 TIME FOR THE TIME STEP              117:        0.77727E+02

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


 INSTANT    0.118000000E+03   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.703069702E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59318E+01 0.33224E+01
   Friction velocity        uet   :  0.10544E-01 0.25611E+01
   Friction velocity        uk    :  0.10511E-01 0.24859E+01
   Dimensionless distance   yplus :  0.36454E-04 0.83923E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3163
   Nb of faces within the viscous sub-layer     :      28626
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66009E+00     120   0.17111E+00   0.11423E+02 0.20113E+03 
c  Velocity[X]                                      0.31658E+01 
c  Velocity[Y]                                      0.39829E+01 
c  Velocity[Z]                                      0.42743E+01 
c  Pressure     0.49599E-01     845   0.86357E-02   0.42958E+00 0.18866E+04 
c  k            0.22323E-01      67   0.49808E-02   0.12635E-01 0.11258E+04 
c  epsilon      0.40888E+03      54   0.12195E-01   0.98351E+07 0.80215   Rel velocity at the wall uiptn : -0.57569E+01 0.33374E+01
   Friction velocity        uet   :  0.96336E-02 0.24985E+01
   Friction velocity        uk    :  0.96034E-02 0.24869E+01
   Dimensionless distance   yplus :  0.35836E-04 0.83843E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3143
   Nb of faces within the viscous sub-layer     :      28774
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65930E+00     121   0.16920E+00   0.12364E+02 0.20893E+03 
c  Velocity[X]                                      0.33752E+01 
c  Velocity[Y]                                      0.45222E+01 
c  Velocity[Z]                                      0.44670E+01 
c  Pressure     0.50204E-01     844   0.94892E-02   0.43814E+00 0.87295E+03 
c  k            0.22167E-01      72   0.58993E-02   0.17934E-01 0.17404E+04 
c  epsilon      0.40089E+03      59   0.15107E-01   0.37639E+08 0.20603E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2636e-05                             6
a  epsilon       -0.039015                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.5088          9.2618         0.50301        0.077126
v  Velocity[Y]            -7.7229          8.0083         0.23057         0.18715
v  Velocity[Z]            -13.007          11.701        -0.19847     -0.00063411
v  ǁVelocityǁ          1.0621e-05          15.692          1.4514          1.5961
v  Pressure                -32017           25984           15655           13572
v  k                   5.2891e-08          1.5637       0.0073541        0.008069
v  epsilon             1.4599e-05      1.5872e+05          66.918          5.3644
v  TurbVisc            3.1037e-13         0.14181      0.00046128     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61211E+01 0.33407E+01
   Friction velocity        uet   :  0.83930E-02 0.25684E+01
   Friction velocity        uk    :  0.82877E-02 0.24947E+01
   Dimensionless distance   yplus :  0.37423E-04 0.84632E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3195
   Nb of faces within the viscous sub-layer     :      28518
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66116E+00     120   0.16874E+00   0.11047E+02 0.19741E+03 
c  Velocity[X]                                      0.31135E+01 
c  Velocity[Y]                                      0.38886E+01 
c  Velocity[Z]                                      0.40448E+01 
c  Pressure     0.48721E-01     789   0.80783E-02   0.41934E+00 0.19901E+04 
c  k            0.22501E-01      63   0.38312E-02   0.98862E-02 0.11633E+04 
c  epsilon      0.41872E+03      47   0.93583E-02   0.13372E+08 0.11942E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6013e-05                             4
a  epsilon       -0.022916                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6552          8.8127         0.51139        0.077131
v  Velocity[Y]            -7.4768          8.0228         0.23459         0.18703
v  Velocity[Z]            -13.324          11.852        -0.20772     -0.00071495
v  ǁVelocityǁ          1.1902e-05          15.882           1.479          1.6015
v  Pressure                -33203           26002           15590           13544
v  k                    5.117e-08          1.5016       0.0076599       0.0081214
v  epsilon             1.4106e-05      1.5861e+05          69.952          5.5029
v  TurbVisc            3.5554e-13         0.14181      0.00046698       0.0064133
v  total_pressure       4.668e+05        5.26e+05      5.1559e+05      5.1354e+05


 TIME FOR THE TIME STEP              119:        0.77936E+02

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


 INSTANT    0.120000000E+03   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         0.233558343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640793E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62566E+01 0.33428E+01
   Friction velocity        uet   :  0.11186E-01 0.25895E+01
   Friction velocity        uk    :  0.11151E-01 0.25122E+01
   Dimensionless distance   yplus :  0.38641E-04 0.85225E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3200
   Nb of faces within the viscous sub-layer     :      28366
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66269E+00     120   0.16991E+00   0.10409E+02 0.19173E+03 
c  Velocity[X]                                      0.29049E+01 
c  Velocity[Y]                                      0.37080E+01 
c  Velocity[Z]                                      0.37960E+01 
c  Pressure     0.46006E-01     763   0.70------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61211E+01 0.33407E+01
   Friction velocity        uet   :  0.83930E-02 0.25684E+01
   Friction velocity        uk    :  0.82877E-02 0.24947E+01
   Dimensionless distance   yplus :  0.37423E-04 0.84632E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3195
   Nb of faces within the viscous sub-layer     :      28518
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66116E+00     120   0.16874E+00   0.11047E+02 0.19741E+03 
c  Velocity[X]                                      0.31135E+01 
c  Velocity[Y]                                      0.38886E+01 
c  Velocity[Z]                                      0.40448E+01 
c  Pressure     0.48721E-01     789   0.80783E-02   0.41934E+00 0.19901E+04 
c  k            0.22501E-01      63   0.38312E-02   0.98862E-02 0.11633E+04 
c  epsilon      0.41872E+03      47   0.93583E-02   0.13372E+08 0.11942E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6013e-05                             4
a  epsilon       -0.022916                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.6552          8.8127         0.51139        0.077131
v  Velocity[Y]            -7.4768          8.0228         0.23459         0.18703
v  Velocity[Z]            -13.324          11.852        -0.20772     -0.00071495
v  ǁVelocityǁ          1.1902e-05          15.882           1.479          1.6015
v  Pressure                -33203           26002           15590           13544
v  k                    5.117e-08          1.5016       0.0076599       0.0081214
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65579E+01 0.33256E+01
   Friction velocity        uet   :  0.10035E-01 0.25840E+01
   Friction velocity        uk    :  0.10003E-01 0.25068E+01
   Dimensionless distance   yplus :  0.39702E-04 0.84814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3201
   Nb of faces within the viscous sub-layer     :      28228
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66312E+00     119   0.17126E+00   0.10469E+02 0.19092E+03 
c  Velocity[X]                                      0.29947E+01 
c  Velocity[Y]                                      0.37032E+01 
c  Velocity[Z]                                      0.37711E+01 
c  Pressure     0.43896E-01     746   0.70467E-02   0.37947E+00 0.19305E+04 
c  k            0.22727E-01      64   0.35965E-02   0.12197E-01 0.11559E+04 
c  epsilon      0.43168E+03      52   0.73431E-02   0.78210E+07 0.64367E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.4654e-05                             4
a  epsilon        -0.13199                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7491          9.1013         0.52036        0.077033
v  Velocity[Y]            -7.2761          8.0376         0.23801         0.18679
v  Velocity[Z]            -13.779          11.562        -0.21495     -0.00069494
v  ǁVelocityǁ          1.3275e-05          16.421          1.5012          1.6056
v  Pressure                -34181           25950           15504           13501
v  k                   5.0207e-08          1.4826       0.0080115       0.0081647
v  epsilon             1.3832e-05      1.5585e+05          74.393          5.6503
v  TurbVisc            2.0874e-13         0.14181      0.00047237       0.0064192
v  total_pressure      4.6582e+05      5.2595e+05       5.155e+05       5.135e+05


 TIME FOR THE TIME STEP              121:        0.70722E+02

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


 INSTANT    0.122000000E+03   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         0.628172902E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67239E+01 0.33479E+01
   Friction velocity        uet   :  0.52288E-02 0.26132E+01
   Friction velocity        uk    :  0.52280E-02 0.25345E+01
   Dimensionless distance   yplus :  0.40902E-04 0.84668E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3195
   Nb of faces within the viscous sub-layer     :      28095
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66364E+00     119   0.17039E+00   0.10091E+02 0.18756E+03 
c  Velocity[X]                                      0.29897E+01 
c  Velocity[Y]      ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65579E+01 0.33256E+01
   Friction velocity        uet   :  0.10035E-01 0.25840E+01
   Friction velocity        uk    :  0.10003E-01 0.25068E+01
   Dimensionless distance   yplus :  0.39702E-04 0.84814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3201
   Nb of faces within the viscous sub-layer     :      28228
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66312E+00     119   0.17126E+00   0.10469E+02 0.19092E+03 
c  Velocity[X]                                      0.29947E+01 
c  Velocity[Y]                                      0.37032E+01 
c  Velocity[Z]                                      0.37711E+01 
c  Pressure     0.43896E-01     746   0.70467E-02   0.37947E+00 0.19305E+04 
c  k            0.22727E-01      64   0.35965E-02   0.12197E-01 0.11559E+04 
c  epsilon      0.43168E+03      52   0.73431E-02   0.78210E+07 0.64367E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.4654e-05                             4
a  epsilon        -0.13199                            12


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.7491          9.1013         0.52036        0.077033
v  Velocity[Y]            -7.2761          8.0376         0.23801         0.18679
v  Velocity[Z]            -13.779          11.562        -0.21495     -0.00069494
v  ǁVelocityǁ          1.3275e-05          16.421     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67758E+01 0.33514E+01
   Friction velocity        uet   :  0.54938E-02 0.26077E+01
   Friction velocity        uk    :  0.54931E-02 0.25288E+01
   Dimensionless distance   yplus :  0.42165E-04 0.84659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3198
   Nb of faces within the viscous sub-layer     :      27998
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66505E+00     118   0.17210E+00   0.99218E+01 0.18614E+03 
c  Velocity[X]                                      0.29177E+01 
c  Velocity[Y]                                      0.34631E+01 
c  Velocity[Z]                                      0.35410E+01 
c  Pressure     0.40984E-01     748   0.60389E-02   0.35560E+00 0.30924E+04 
c  k            0.22993E-01      62   0.38616E-02   0.99628E-02 0.11028E+04 
c  epsilon      0.44608E+03      45   0.89301E-02   0.92314E+07 0.73094E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011106                             2
a  epsilon       -0.012803                             7


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8539          9.0282          0.5295        0.076927
v  Velocity[Y]            -7.0472          8.1018         0.23998         0.18661
v  Velocity[Z]            -13.533          11.482        -0.21969     -0.00067166
v  ǁVelocityǁ          1.4764e-05            16.2           1.519          1.6089
v  Pressure                -34942           25859           15375           13432
v  k                   4.9877e-08          1.5021        0.008281        0.008191
v  epsilon             1.3742e-05      1.5914e+05          78.042          5.7655
v  TurbVisc            4.9751e-13         0.14181      0.00047671       0.0064214
v  total_pressure      4.6506e+05      5.2586e+05      5.1537e+05      5.1343e+05


 TIME FOR THE TIME STEP              123:        0.78169E+02

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


 INSTANT    0.124000000E+03   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         0.108803039E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64604E+01 0.33407E+01
   Friction velocity        uet   :  0.60541E-02 0.26298E+01
   Friction velocity        uk    :  0.60529E-02 0.25502E+01
   Dimensionless distance   yplus :  0.43229E-04 0.84232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3199
   Nb of faces within the viscous sub-layer     :      27881
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67758E+01 0.33514E+01
   Friction velocity        uet   :  0.54938E-02 0.26077E+01
   Friction velocity        uk    :  0.54931E-02 0.25288E+01
   Dimensionless distance   yplus :  0.42165E-04 0.84659E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3198
   Nb of faces within the viscous sub-layer     :      27998
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66505E+00     118   0.17210E+00   0.99218E+01 0.18614E+03 
c  Velocity[X]                                      0.29177E+01 
c  Velocity[Y]                                      0.34631E+01 
c  Velocity[Z]                                      0.35410E+01 
c  Pressure     0.40984E-01     748   0.60389E-02   0.35560E+00 0.30924E+04 
c  k            0.22993E-01      62   0.38616E-02   0.99628E-02 0.11028E+04 
c  epsilon      0.44608E+03      45   0.89301E-02   0.92314E+07 0.73094E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011106                             2
a  epsilon       -0.012803                             7


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8539          9.0282          0.5295        0.076927
v  Velocity[Y]            -7Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69891E+01 0.33536E+01
   Friction velocity        uet   :  0.64505E-02 0.26215E+01
   Friction velocity        uk    :  0.64503E-02 0.25417E+01
   Dimensionless distance   yplus :  0.44035E-04 0.83798E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3206
   Nb of faces within the viscous sub-layer     :      27794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66544E+00     117   0.16609E+00   0.96114E+01 0.18383E+03 
c  Velocity[X]                                      0.27215E+01 
c  Velocity[Y]                                      0.34485E+01 
c  Velocity[Z]                                      0.34414E+01 
c  Pressure     0.36999E-01     752   0.60392E-02   0.32472E+00 0.18170E+04 
c  k            0.23114E-01      60   0.25440E-02   0.63875E-02 0.78128E+03 
c  epsilon      0.44984E+03      43   0.48031E-02   0.38739E+07 0.38844E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012947                             3
a  epsilon      -0.0024547                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.8937          9.0966         0.53777        0.076989
v  Velocity[Y]            -7.1804          8.0437         0.24067         0.18633
v  Velocity[Z]            -13.723          11.412        -0.22279     -0.00059162
v  ǁVelocityǁ          1.5894e-05          16.386          1.5326          1.6112
v  Pressure                -35553           25808           15263           13367
v  k                   5.0066e-08          1.5054       0.0084773       0.0082153
v  epsilon             1.3794e-05      1.5971e+05          80.532          5.8546
v  TurbVisc            5.8069e-13         0.14181      0.00048001       0.0064224
v  total_pressure      4.6445e+05      5.2581e+05      5.1526e+05      5.1337e+05


 TIME FOR THE TIME STEP              125:        0.72039E+02

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


 INSTANT    0.126000000E+03   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.200470634E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640795E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66534E+01 0.33580E+01
   Friction velocity        uet   :  0.56133E-02 0.26382E+01
   Friction velocity        uk    :  0.56129E-02 0.25580E+01
   Dimensionless distance   yplus :  0.44950E-04 0.83820E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3213
   Nb of faces within the viscous sub-layer     :      27717
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69891E+01 0.33536E+01
   Friction velocity        uet   :  0.64505E-02 0.26215E+01
   Friction velocity        uk    :  0.64503E-02 0.25417E+01
   Dimensionless distance   yplus :  0.44035E-04 0.83798E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3206
   Nb of faces within the viscous sub-layer     :      27794
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66544E+00     117   0.16609E+00   0.96114E+01 0.18383E+03 
c  Velocity[X]                                      0.27215E+01 
c  Velocity[Y]                                      0.34485E+01 
c  Velocity[Z]                                      0.34414E+01 
c  Pressure     0.36999E-01     752   0.60392E-02   0.32472E+00 0.18170E+04 
c  k            0.23114E-01      60   0.25440E-02   0.63875E-02 0.78128E+03 
c  epsilon      0.44984E+03      43   0.48031E-02   0.38739E+07 0.38844E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012947                             3
a  epsilon      -0.0024547                             2


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

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.232748815E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68192E+01 0.33650E+01
   Friction velocity        uet   :  0.65424E-02 0.25820E+01
   Friction velocity        uk    :  0.65422E-02 0.25527E+01
   Dimensionless distance   yplus :  0.45583E-04 0.83800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3215
   Nb of faces within the viscous sub-layer     :      27684
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66668E+00     116   0.16689E+00   0.94388E+01 0.18152E+03 
c  Velocity[X]                                      0.26342E+01 
c  Velocity[Y]                                      0.32161E+01 
c  Velocity[Z]                                      0.35885E+01 
c  Pressure     0.35067E-01     674   0.58221E-02   0.31095E+00 0.23965E+04 
c  k            0.23272E-01      60   0.29581E-02   0.56837E-02 0.84606E+03 
c  epsilon      0.45914E+03      44   0.77428E-02   0.64482E+07 0.62111E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2322e-05                             1
a  epsilon       -0.015331                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9533          9.0426         0.54446         0.07715
v  Velocity[Y]            -7.2241            8.09          0.2408         0.18616
v  Velocity[Z]             -13.78          11.187        -0.22476     -0.00057262
v  ǁVelocityǁ          1.7023e-05          16.406          1.5432           1.613
v  Pressure                -36317           25723           15154           13308
v  k                   5.0685e-08          1.5306       0.0086288       0.0082356
v  epsilon             1.3954e-05      1.6082e+05          83.112           5.922
v  TurbVisc            6.5716e-13         0.14181        0.000483       0.0064238
v  total_pressure      4.6368e+05      5.2572e+05      5.1515e+05      5.1331e+05


 TIME FOR THE TIME STEP              127:        0.62263E+02

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


 INSTANT    0.128000000E+03   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.221334036E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640847E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67243E+01 0.33556E+01
   Friction velocity        uet   :  0.35938E-02 0.26478E+01
   Friction velocity        uk    :  0.35937E-02 0.25671E+01
   Dimensionless distance   yplus :  0.46625E-04 0.83829E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3223
   Nb of faces within the viscous sub-layer     :      27624
   Total nuInlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.232748815E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640794E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68192E+01 0.33650E+01
   Friction velocity        uet   :  0.65424E-02 0.25820E+01
   Friction velocity        uk    :  0.65422E-02 0.25527E+01
   Dimensionless distance   yplus :  0.45583E-04 0.83800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3215
   Nb of faces within the viscous sub-layer     :      27684
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66668E+00     116   0.16689E+00   0.94388E+01 0.18152E+03 
c  Velocity[X]                                      0.26342E+01 
c  Velocity[Y]                                      0.32161E+01 
c  Velocity[Z]                                      0.35885E+01 
c  Pressure     0.35067E-01     674   0.58221E-02   0.31095E+00 0.23965E+04 
c  k            0.23272E-01      60   0.29581E-02   0.56837E-02 0.84606E+03 
c  epsilon      0.45914E+03      44   0.77428E-02   0.64482E+07 0.62111E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2322e-05                             1
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.938468893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640846E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67869E+01 0.33725E+01
   Friction velocity        uet   :  0.84181E-02 0.26396E+01
   Friction velocity        uk    :  0.84176E-02 0.25655E+01
   Dimensionless distance   yplus :  0.47495E-04 0.83814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3233
   Nb of faces within the viscous sub-layer     :      27571
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66751E+00     115   0.16800E+00   0.88068E+01 0.17171E+03 
c  Velocity[X]                                      0.25925E+01 
c  Velocity[Y]                                      0.30806E+01 
c  Velocity[Z]                                      0.31338E+01 
c  Pressure     0.34046E-01     659   0.64414E-02   0.30388E+00 0.25060E+04 
c  k            0.23395E-01      59   0.27429E-02   0.51578E-02 0.84178E+03 
c  epsilon      0.46592E+03      41   0.59663E-02   0.58105E+07 0.64508E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.6749e-05                             2
a  epsilon       -0.037168                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -3.9519          8.9781         0.54888         0.07717
v  Velocity[Y]            -7.4954          8.0912         0.24124         0.18602
v  Velocity[Z]            -13.506          11.637        -0.22521     -0.00044183
v  ǁVelocityǁ          1.8173e-05          16.092          1.5512          1.6142
v  Pressure                -36982           25699           15097           13286
v  k                   5.1677e-08          1.5577       0.0087506       0.0082503
v  epsilon             2.0143e-06       1.618e+05          84.928          5.9785
v  TurbVisc            7.1576e-13         0.14181      0.00048493       0.0064244
v  total_pressure      4.6302e+05       5.257e+05       5.151e+05      5.1329e+05


 TIME FOR THE TIME STEP              129:        0.65503E+02

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


 INSTANT    0.130000000E+03   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         0.696015884E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640847E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64386E+01 0.33701E+01
   Friction velocity        uet   :  0.73702E-02 0.26576E+01
   Friction velocity        uk    :  0.73697E-02 0.25765E+01
   Dimensionless distance   yplus :  0.48256E-04 0.83825E+01
   ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.938468893E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640846E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67869E+01 0.33725E+01
   Friction velocity        uet   :  0.84181E-02 0.26396E+01
   Friction velocity        uk    :  0.84176E-02 0.25655E+01
   Dimensionless distance   yplus :  0.47495E-04 0.83814E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3233
   Nb of faces within the viscous sub-layer     :      27571
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66751E+00     115   0.16800E+00   0.88068E+01 0.17171E+03 
c  Velocity[X]                                      0.25925E+01 
c  Velocity[Y]                                      0.30806E+01 
c  Velocity[Z]                                      0.31338E+01 
c  Pressure     0.34046E-01     659   0.64414E-02   0.30388E+00 0.25060E+04 
c  k            0.23395E-01      59   0.27429E-02   0.51578E-02 0.84178E+03 
c  epsilon      0.46592E+03      41   0.59663E-02   0.58105E+07 0.64508E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.194567631E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67099E+01 0.33681E+01
   Friction velocity        uet   :  0.85696E-02 0.26452E+01
   Friction velocity        uk    :  0.85683E-02 0.25684E+01
   Dimensionless distance   yplus :  0.48947E-04 0.83800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3240
   Nb of faces within the viscous sub-layer     :      27490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66734E+00     117   0.16719E+00   0.89648E+01 0.17078E+03 
c  Velocity[X]                                      0.27268E+01 
c  Velocity[Y]                                      0.30905E+01 
c  Velocity[Z]                                      0.31476E+01 
c  Pressure     0.33362E-01     822   0.64423E-02   0.30044E+00 0.56926E+03 
c  k            0.23510E-01      60   0.25698E-02   0.59187E-02 0.11194E+04 
c  epsilon      0.47256E+03      49   0.74276E-02   0.17941E+08 0.15211E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon       -0.022279                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.0427          9.4378         0.55159         0.07714
v  Velocity[Y]             -7.518          8.1091         0.24182         0.18594
v  Velocity[Z]            -13.882          11.529        -0.22466     -0.00049301
v  ǁVelocityǁ          1.9389e-05          16.591          1.5576          1.6146
v  Pressure                -37479           25767           15095           13302
v  k                   5.3029e-08          1.5639       0.0088447       0.0082613
v  epsilon             1.4503e-05       1.607e+05          86.983          6.0259
v  TurbVisc            7.4731e-13         0.14181      0.00048698       0.0064249
v  total_pressure      4.6252e+05      5.2577e+05       5.151e+05       5.133e+05


 TIME FOR THE TIME STEP              131:        0.73920E+02

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


 INSTANT    0.132000000E+03   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         0.113062258E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640855E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68462E+01 0.33627E+01
   Friction velocity        uet   :  0.80325E-02 0.26620E+01
   Friction velocity         ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.194567631E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67099E+01 0.33681E+01
   Friction velocity        uet   :  0.85696E-02 0.26452E+01
   Friction velocity        uk    :  0.85683E-02 0.25684E+01
   Dimensionless distance   yplus :  0.48947E-04 0.83800E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3240
   Nb of faces within the viscous sub-layer     :      27490
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66734E+00     117   0.16719E+00   0.89648E+01 0.17078E+03 
c  Velocity[X]                                      0.27268E+01 
c  Velocity[Y]                                      0.30905E+01 
c  Velocity[Z]                                      0.31476E+01 
c  Pressure     0.33362E-01     822   0.64423E-02   0.30044E+00 0.56926E+03 
c  k            0.23510E-01      60   0.25698E-02   0.59187E-02 0.11194E+04 
c  epsilon      0.47256E+03      49   0.74276E-02   0.17941E+08 0.15211E+05 
----------------------------------------------------------------------- INSTANT    0.133000000E+03   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.255366657E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68478E+01 0.33757E+01
   Friction velocity        uet   :  0.88801E-02 0.26495E+01
   Friction velocity        uk    :  0.88788E-02 0.25787E+01
   Dimensionless distance   yplus :  0.50585E-04 0.83803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3236
   Nb of faces within the viscous sub-layer     :      27443
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66810E+00     116   0.16939E+00   0.88961E+01 0.16838E+03 
c  Velocity[X]                                      0.26908E+01 
c  Velocity[Y]                                      0.29850E+01 
c  Velocity[Z]                                      0.32204E+01 
c  Pressure     0.32654E-01     822   0.55714E-02   0.29463E+00 0.48452E+03 
c  k            0.23590E-01      57   0.19447E-02   0.19626E-02 0.40822E+03 
c  epsilon      0.47932E+03      39   0.25138E-02   0.73958E+06 0.21449E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.12799                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3076          9.3743         0.55328         0.07721
v  Velocity[Y]            -7.5598          8.1143         0.24232         0.18585
v  Velocity[Z]            -13.793          11.618        -0.22336     -0.00045634
v  ǁVelocityǁ          2.0022e-05           16.44          1.5622           1.615
v  Pressure                -38069           25781           15072           13299
v  k                   5.4711e-08          1.5665         0.00891       0.0082672
v  epsilon             1.4884e-05      1.6146e+05          88.402          6.0513
v  TurbVisc            7.5987e-13         0.14181      0.00048836       0.0064253
v  total_pressure      4.6193e+05      5.2578e+05      5.1507e+05       5.133e+05


 TIME FOR THE TIME STEP              133:        0.74669E+02

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


 INSTANT    0.134000000E+03   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         0.679732090E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67372E+01 0.33853E+01
   Friction velocity       INSTANT    0.133000000E+03   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.255366657E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68478E+01 0.33757E+01
   Friction velocity        uet   :  0.88801E-02 0.26495E+01
   Friction velocity        uk    :  0.88788E-02 0.25787E+01
   Dimensionless distance   yplus :  0.50585E-04 0.83803E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3236
   Nb of faces within the viscous sub-layer     :      27443
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66810E+00     116   0.16939E+00   0.88961E+01 0.16838E+03 
c  Velocity[X]                                      0.26908E+01 
c  Velocity[Y]                                      0.29850E+01 
c  Velocity[Z]                                      0.32204E+01 
c  Pressure     0.32654E-01     822   0.55714E-02   0.29463E+00 0.48452E+03 
c  k            0.23590E-01      57   0.19447E-02   0.19626E-02 0.40822E+03 
c  epsilon      0.47932E+03      39   0.25138E-02   0.73958E+06 0.21449E+04 
-----===============================================================


 INSTANT    0.135000000E+03   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        -0.136669924E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640853E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72640E+01 0.33855E+01
   Friction velocity        uet   :  0.11503E-01 0.26622E+01
   Friction velocity        uk    :  0.11501E-01 0.26043E+01
   Dimensionless distance   yplus :  0.51185E-04 0.84129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3256
   Nb of faces within the viscous sub-layer     :      27401
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66884E+00     115   0.16802E+00   0.87994E+01 0.16687E+03 
c  Velocity[X]                                      0.27421E+01 
c  Velocity[Y]                                      0.29531E+01 
c  Velocity[Z]                                      0.31042E+01 
c  Pressure     0.33350E-01     898   0.55779E-02   0.30213E+00 0.27679E+03 
c  k            0.23674E-01      59   0.24498E-02   0.40572E-02 0.76984E+03 
c  epsilon      0.48474E+03      45   0.40179E-02   0.43225E+07 0.55667E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.0987e-08                             1
a  epsilon        -0.16352                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1792          9.5483         0.55476        0.077125
v  Velocity[Y]            -7.6673          8.0814         0.24296         0.18579
v  Velocity[Z]            -13.749          11.808        -0.22185     -0.00045662
v  ǁVelocityǁ          2.0107e-05          16.565          1.5662           1.615
v  Pressure                -38415           25880           15089           13327
v  k                    5.667e-08          1.5723       0.0089879       0.0082716
v  epsilon             1.5341e-05      1.6307e+05          89.793          6.0811
v  TurbVisc            7.6748e-13         0.14181      0.00048998       0.0064262
v  total_pressure      4.6158e+05      5.2588e+05      5.1509e+05      5.1333e+05


 TIME FOR THE TIME STEP              135:        0.68193E+02

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


 INSTANT    0.136000000E+03   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.550846775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640866E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------===============================================================


 INSTANT    0.135000000E+03   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        -0.136669924E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640853E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72640E+01 0.33855E+01
   Friction velocity        uet   :  0.11503E-01 0.26622E+01
   Friction velocity        uk    :  0.11501E-01 0.26043E+01
   Dimensionless distance   yplus :  0.51185E-04 0.84129E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3256
   Nb of faces within the viscous sub-layer     :      27401
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66884E+00     115   0.16802E+00   0.87994E+01 0.16687E+03 
c  Velocity[X]                                      0.27421E+01 
c  Velocity[Y]                                      0.29531E+01 
c  Velocity[Z]                                      0.31042E+01 
c  Pressure     0.33350E-01     898   0.55779E-02   0.30213E+00 0.27679E+03 
c  k            0.23674E-01      59   0.24498E-02   0.40572E-02 0.76984E+03 
c  epsilon      0.48474E+03      45   0.40179E-02   0.43225E+07 0.55667E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.0987e-08                             1
a  epsilon        -0.16352                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1792          9.5483         0.55476        0.077125
v  Velocity[Y]            -7.6673          8.0814         0.24296         0.18579
v  Velocity[Z]            -13.749          11.808        -0.22185     -0.00045662
v  ǁVelocityǁ          2.0107e-05          16.565          1.5662           1.615
v  Pressure                -38415           25880           15089           13327
v  k                    5.667e-08          1.5723       0.0089879       0.0082716
v  epsilon             1.5341e-05      1.6307e+05          89.793          6.0811
v  TurbVisc            7.6748e-13         0.14181      0.00048998       0.0064262
v  total_pressure      4.6158e+05      5.2588e+05      5.1509e+05      5.1333e+05


 TIME FOR THE TIME STEP              135:        0.83795E+02

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


 INSTANT    0.136000000E+03   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.550846775E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640866E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66591E+01 0.33685E+01
   Friction velocity        uet   :  0.10927E-01 0.26798E+01
   Friction velocity        uk    :  0.10925E-01 0.25977E+01
   Dimensionless distance   yplus :  0.51063E-04 0.83825E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3268
   Nb of faces within the viscous sub-layer     :      27400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66893E+00     113   0.16685E+00   0.87960E+01 0.16785E+03 
c  Velocity[X]                                      0.27500E+01 
c  Velocity[Y]                                      0.28439E+01 
c  Velocity[Z]                                      0.32022E+01 
c  Pressure     0.34282E-01     809   0.53316E-02   0.31226E+00 0.79190E+03 
c  k            0.23666E-01      58   0.24015E-02   0.30930E-02 0.60875E+03 
c  epsilon      0.48493E+03      42   0.33814E-02   0.24169E+07 0.38043E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6791e-05                             2
a  epsilon       -0.068405                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.1874          9.4914         0.55555        0.077065
v  Velocity[Y]            -7.6034          8.1118         0.24355         0.18578
v  Velocity[Z]            -13.954          12.067        -0.22121     -0.00048822
v  ǁVelocityǁ           2.016e-05          16.738          1.5681           1.615
v  Pressure                -38664           25932           15103           13339
v  k                   5.7724e-08          1.5695       0.0090121       0.0082734
v  epsilon             1.5597e-05      1.6018e+05          90.173          6.0881
v  TurbVisc             7.711e-13         0.14181      0.00049045       0.0064264
v  total_pressure      4.6134e+05      5.2593e+05       5.151e+05      5.1334e+05


 TIME FOR THE TIME STEP              136:        0.75352E+02

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


 INSTANT    0.137000000E+03   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        -0.146974590E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640866E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68900E+01 0.33852E+01
   Friction velocity        uet   :  0.11370E-01 0.26323E+01
   Friction velocity        uk    :  0.11368E-01 0.26167E+01
   Dimensionless distance   yplus :  0.51168E-04 0.83807E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3265
   Nb of faces within the viscous sub-layer     :      27407
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66976E+00     113   0.16857E+00   0.84749E+01 0.16510E+03 
c  Velocity[X]                                      0.25908E+01 
c  Velocity[Y]                                      0.27252E+01 
c  Velocity[Z]                                      0.31588E+01 
c  Pressure     0.v  epsilon             1.6158e-05      1.6319e+05          91.933           6.105
v  TurbVisc            7.7874e-13         0.14181      0.00049145       0.0064273
v  total_pressure      4.6094e+05      5.2601e+05      5.1513e+05      5.1337e+05


 TIME FOR THE TIME STEP              138:        0.58322E+02

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


 INSTANT    0.139000000E+03   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        -0.149247645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640855E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67370E+01 0.33961E+01
   Friction velocity        uet   :  0.57467E-02 0.26783E+01
   Friction velocity        uk    :  0.57463E-02 0.26310E+01
   Dimensionless distance   yplus :  0.51193E-04 0.83864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3259
   Nb of faces within the viscous sub-layer     :      27411
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67056E+00     114   0.16934E+00   0.81637E+01 0.16306E+03 
c  Velocity[X]                                      0.25526E+01 
c  Velocity[Y]                                      0.26800E+01 
c  Velocity[Z]                                      0.29311E+01 
c  Pressure     0.33939E-01     857   0.48581E-02   0.31117E+00 0.62035E+03 
c  k            0.23746E-01      59   0.25025E-02   0.38987E-02 0.73911E+03 
c  epsilon      0.48990E+03      41   0.48594E-02   0.45225E+07 0.52556E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.8533e-06                             2
a  epsilon        -0.24227                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2563          9.2547         0.55825        0.077122
v  Velocity[Y]            -7.5926          8.0723         0.24504         0.18552
v  Velocity[Z]            -13.958          11.903           -0.22     -0.00060072
v  ǁVelocityǁ          2.0214e-05           16.53          1.5739          1.6149
v  Pressure                -39204           26097           15159           13390
v  k                   6.0817e-08          1.5797       0.0091096       0.0082743
v  epsilon             1.6441e-05      1.6404e+05          92.136          6.1153
v  TurbVisc            7.8257e-13         0.14181      0.00049209       0.0064274
v  total_pressure       4.608e+05       5.261e+05      5.1516e+05      5.1339e+05


 TIME FOR THE TIME STEP              139:        0.80022E+02

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


 INSTANT    0.140000000E+03   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        -0.429940211E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640857E+00
Free inlet               13           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  epsilon             1.6158e-05      1.6319e+05          91.933           6.105
v  TurbVisc            7.7874e-13         0.14181      0.00049145       0.0064273
v  total_pressure      4.6094e+05      5.2601e+05      5.1513e+05      5.1337e+05


 TIME FOR THE TIME STEP              138:        0.72941E+02

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


 INSTANT    0.139000000E+03   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        -0.149247645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640855E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67370E+01 0.33961E+01
   Friction velocity        uet   :  0.57467E-02 0.26783E+01
   Friction velocity        uk    :  0.57463E-02 0.26310E+01
   Dimensionless distance   yplus :  0.51193E-04 0.83864E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3259
   Nb of faces within the viscous sub-layer     :      27411
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67056E+00     114   0.16934E+00   0.81637E+01 0.16306E+03 
c  Velocity[X]                                      0.25526E+01 
c  Velocity[Y]                                      0.26800E+01 
c  Velocity[Z]                                      0.29311E+01 
c  Pressure     0.33939E-01     857   0.48581E-02   0.31117E+00 0.62035E+03 
c  k            0.23746E-01      59   0.25025E-02   0.38987E-02 0.73911E+03 
c  epsilon      0.48990E+03      41   0.48594E-02   0.45225E+07 0.52556E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.8533e-06                             2
a  epsilon        -0.24227                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2563          9.2547         0.55825        0.077122
v  Velocity[Y]            -7.5926          8.0723         0.24504         0.18552
v  Velocity[Z]            -13.958          11.903           -0.22     -0.00060072
v  ǁVelocityǁ          2.0214e-05           16.53          1.5739          1.6149
v  Pressure                -39204           26097           15159           13390
v  k                   6.0817e-08          1.5797       0.0091096       0.0082743
v  epsilon             1.6441e-05      1.6404e+05          92.136          6.1153
v  TurbVisc            7.8257e-13         0.14181      0.00049209       0.0064274
v  total_pressure       4.608e+05       5.261e+05      5.1516e+05      5.1339e+05


 TIME FOR THE TIME STEP              139:        0.75629E+02

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


 INSTANT    0.140000000E+03   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        -0.429940211E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640857E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68965E+01 0.33807E+01
   Friction velocity        uet   :  0.10896E-01 0.26920E+01
   Friction velocity        uk    :  0.10895E-01 0.26092E+01
   Dimensionless distance   yplus :  0.51313E-04 0.83943E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3272
   Nb of faces within the viscous sub-layer     :      27400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67081E+00     112   0.16363E+00   0.79988E+01 0.16285E+03 
c  Velocity[X]                                      0.23951E+01 
c  Velocity[Y]                                      0.27107E+01 
c  Velocity[Z]                                      0.28930E+01 
c  Pressure     0.33558E-01     625   0.51896E-02   0.30834E+00 0.28023E+03 
c  k            0.23750E-01      57   0.21635E-02   0.29602E-02 0.66119E+03 
c  epsilon      0.48915E+03      46   0.34432E-02   0.30603E+07 0.41348E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.3604e-06                             1
a  epsilon        -0.13804                             8


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2679          9.4667         0.55916        0.077153
v  Velocity[Y]            -7.4693          8.2193         0.24547         0.18554
v  Velocity[Z]            -13.868          12.086        -0.21989     -0.00053814
v  ǁVelocityǁ          2.0447e-05          16.612           1.576           1.615
v  Pressure                -39449           26126           15170           13400
v  k                   6.1685e-08          1.5868       0.0091486       0.0082759
v  epsilon             1.6713e-05      1.6156e+05          92.963          6.1269
v  TurbVisc            7.8598e-13         0.14181      0.00049269       0.0064277
v  total_pressure      4.6055e+05      5.2613e+05      5.1517e+05       5.134e+05


 TIME FOR THE TIME STEP              140:        0.69062E+02

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


 INSTANT    0.141000000E+03   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        -0.317031993E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67940E+01 0.33897E+01
   Friction velocity        uet   :  0.10784E-01 0.26786E+01
   Friction velocity        uk    :  0.10781E-01 0.26378E+01
   Dimensionless distance   yplus :  0.51682E-04 0.83942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3264
   Nb of faces within the viscous sub-layer     :      27381
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67231E+00     111   0.16720E+00   0.78016E+01 0.16013E+03 
c  Velocity[X]                                      0.24011E+01 
c  Velocity[Y]                                      0.25023E+01 
c  Velocity[Z]                                      0.28982E+01 
c  Pressure     0.32755E-01     676   0.49792E-02   0.29977E+00 0.59308E+03 
c  k            0.23775E-01      56   0.21100E-02   0.26459E-02 0.54614E+03 
c  epsilon      0.48960E+03      39   0.28679E-02   0.19409E+07 0.30988E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.2334e-05                             2
a  epsilon       -0.059929                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3125          9.6053         0.56007        0.077178
v  Velocity[Y]            -7.6642          8.1214         0.24577         0.18558
v  Velocity[Z]            -13.954          11.797        -0.21993     -0.00061664
v  ǁVelocityǁ           2.034e-05          16.838           1.578          1.6152
v  Pressure                -39705           26191           15201           13426
v  k                   6.2274e-08          1.5698         0.00918       0.0082782
v  epsilon             1.6943e-05      1.6319e+05          93.348          6.1361
v  TurbVisc            7.9014e-13         0.14181      0.00049321       0.0064282
v  total_pressure       4.603e+05      5.2619e+05       5.152e+05      5.1343e+05


 TIME FOR THE TIME STEP              141:        0.67814E+02

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


 INSTANT    0.142000000E+03   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        -0.116719975E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640845E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69196E+01 0.33928E+01
   Friction velocity        uet   :  0.31985E-02 0.26990E+01
   Friction velocity        uk    :  0.31981E-02 0.26158E+01
   Dimensionless distance   yplus :  0.51535E-04 0.83998E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3265
   Nb of faces within the viscous sub-layer     :      27375
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67275E+00     110   0.16778E+00   0.79560E+01 0.16407E+03 
c  Velocity[X]                                      0.24484E+01 
c  Velocity[Y]                                      0.24647E+01 
c  Velocity[Z]                                      0.30428E+01 
c  Pressure     0.31967E-01     557   0.51840E-02   0.29228E+00 0.38199E+03 
c  k            0.23805E-01      57   0.25484E-02   0.54418E-02 0.10544E+04 
c  epsilon      0.49558E+03      50   0.79883E-02   0.14866E+08 0.10616E+05 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.5499e-06                             2
a  epsilon       -0.040231                             7


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2828          9.4082         0.56109        0.077161
v  Velocity[Y]            -7.6975           8.264         0.24605         0.18557
v  Velocity[Z]             -14.09           12.11        -0.22012     -0.00056475
v  ǁVelocityǁ          2.0435e-05           16.68          1.5801          1.6151
v  Pressure                -39856           26221           15224           13447
v  k                   6.1423e-08          1.6024       0.0092336       0.0082785
v  epsilon             1.7018e-05      1.6364e+05          94.952          6.1514
v  TurbVisc            7.9373e-13         0.14181      0.00049398       0.0064285
v  total_pressure      4.6014e+05      5.2622e+05      5.1522e+05      5.1345e+05


 TIME FOR THE TIME STEP              142:        0.72369E+02

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


 INSTANT    0.143000000E+03   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.106491948E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70379E+01 0.33944E+01
   Friction velocity        uet   :  0.54712E-02 0.26837E+01
   Friction velocity        uk    :  0.54705E-02 0.26447E+01
   Dimensionless distance   yplus :  0.51657E-04 0.83987E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3276
   Nb of faces within the viscous sub-layer     :      27363
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67264E+00     110   0.16758E+00   0.78014E+01 0.16182E+03 
c  Velocity[X]                                      0.24300E+01 
c  Velocity[Y]                                      0.24711E+01 
c  Velocity[Z]                                      0.29002E+01 
c  Pressure     0.31193E-01     750   0.52502E-02   0.28576E+00 0.76356E+03 
c  k            0.23837E-01      60   0.24600E-02   0.24556E-02 0.61132E+03 
c  epsilon      0.49705E+03      46   0.36172E-02   0.29849E+07 0.47536E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.1073e-06                             1
a  epsilon       -0.034587                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.315          9.2548         0.56191        0.077161
v  Velocity[Y]            -7.6894          8.1433          0.2462         0.18562
v  Velocity[Z]            -14.084           11.79        -0.22045     -0.00061882
v  ǁVelocityǁ          2.0701e-05          16.517          1.5822          1.6151
v  Pressure                -39981           26222           15237           13454
v  k                   4.4677e-08          1.6423       0.0092494       0.0082813
v  epsilon             1.7051e-05      1.6305e+05          94.783          6.1625
v  TurbVisc             7.976e-13         0.14181      0.00049475       0.0064289
v  total_pressure      4.6002e+05      5.2622e+05      5.1524e+05      5.1345e+05


 TIME FOR THE TIME STEP              143:        0.71026E+02

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


 INSTANT    0.144000000E+03   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        -0.163234736E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70356E+01 0.34062E+01
   Friction velocity        uet   :  0.59794E-02 0.26997E+01
   Friction velocity        uk    :  0.59788E-02 0.26162E+01
   Dimensionless distance   yplus :  0.52020E-04 0.84041E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3271
   Nb of faces within the viscous sub-layer     :      27354
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67299E+00     111   0.16896E+00   0.78604E+01 0.16347E+03 
c  Velocity[X]                                      0.24426E+01 
c  Velocity[Y]                                      0.25607E+01 
c  Velocity[Z]                                      0.28571E+01 
c  Pressure     0.30183E-01     639   0.46525E-02   0.27648E+00 0.15489E+04 
c  k            0.23819E-01      57   0.22534E-02   0.23629E-02 0.55326E+03 
c  epsilon      0.49692E+03      38   0.25027E-02   0.18872E+07 0.34081E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.8331e-06                             2
a  epsilon       -0.051264                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4666          9.1584         0.56265        0.077057
v  Velocity[Y]            -7.6102          8.3065         0.24626         0.18563
v  Velocity[Z]            -13.479          12.152        -0.22062     -0.00054158
v  ǁVelocityǁ          2.0673e-05          16.137          1.5839           1.615
v  Pressure                -40010           26259           15233           13456
v  k                   5.2079e-08          1.6432       0.0092709       0.0082812
v  epsilon             1.7046e-05      1.6558e+05           95.26          6.1644
v  TurbVisc             8.018e-13         0.14181      0.00049517       0.0064292
v  total_pressure      4.5999e+05      5.2626e+05      5.1523e+05      5.1346e+05


 TIME FOR THE TIME STEP              144:        0.67348E+02

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


 INSTANT    0.145000000E+03   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.273897069E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640796E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63852E+01 0.33900E+01
   Friction velocity        uet   :  0.77144E-02 0.26857E+01
   Friction velocity        uk    :  0.77137E-02 0.26467E+01
   Dimensionless distance   yplus :  0.51988E-04 0.84030E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3273
   Nb of faces within the viscous sub-layer     :      27342
   Total number of wall faces                   :      4
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3771          9.5952         0.56371        0.076955
v  Velocity[Y]            -7.6551          8.3227         0.24634         0.18567
v  Velocity[Z]            -14.069          12.305        -0.22126     -0.00059789
v  ǁVelocityǁ          2.0771e-05          16.806          1.5876          1.6149
v  Pressure                -40189           26330           15253           13472
v  k                    5.606e-08          1.6468       0.0093168       0.0082828
v  epsilon             1.6954e-05        1.65e+05          95.916          6.1786
v  TurbVisc            8.0936e-13         0.14181      0.00049637       0.0064295
v  total_pressure      4.5981e+05      5.2633e+05      5.1525e+05      5.1347e+05


 TIME FOR THE TIME STEP              146:        0.61712E+02

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


 INSTANT    0.147000000E+03   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        -0.340342592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640826E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70079E+01 0.33735E+01
   Friction velocity        uet   :  0.17083E-01 0.26836E+01
   Friction velocity        uk    :  0.17077E-01 0.26381E+01
   Dimensionless distance   yplus :  0.52125E-04 0.84020E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3280
   Nb of faces within the viscous sub-layer     :      27333
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67425E+00     110   0.16698E+00   0.79098E+01 0.16322E+03 
c  Velocity[X]                                      0.24420E+01 
c  Velocity[Y]                                      0.25372E+01 
c  Velocity[Z]                                      0.29306E+01 
c  Pressure     0.27903E-01     688   0.38242E-02   0.25513E+00 0.30880E+03 
c  k            0.23927E-01      58   0.23619E-02   0.42875E-02 0.68350E+03 
c  epsilon      0.50025E+03      45   0.32581E-02   0.34385E+07 0.37892E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -6.737e-06                             2
a  epsilon        -0.12117                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3388           9.455         0.56417        0.077008
v  Velocity[Y]            -7.5113          8.2041         0.24624         0.18571
v  Velocity[Z]            -14.068          12.132        -0.22152     -0.00053255
v  ǁVelocityǁ          2.0611e-05           16.75           1.589          1.6149
v  Pressure                -40330           26401           15256           13476
v  k                   5.3984e-08          1.6497       0.0093463       0.0082846
v  epsilon             1.6877e-05      1.6054e+05          96.298          6.1969
v  TurbVisc            8.1333e-13         0.14181      0.00049702       0.0064296
v  total_pressure      4.5967e+05       5.264e+05      5.1526e+05      5.1348e+05


 TIME FOR THE TIME STEP              147:        0.73490E+02

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


 INSTANT    0.148000000E+03   TIME STEP NUMBER             148
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces  
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3771          9.5952         0.56371        0.076955
v  Velocity[Y]            -7.6551          8.3227         0.24634         0.18567
v  Velocity[Z]            -14.069          12.305        -0.22126     -0.00059789
v  ǁVelocityǁ          2.0771e-05          16.806          1.5876          1.6149
v  Pressure                -40189           26330           15253           13472
v  k                    5.606e-08          1.6468       0.0093168       0.0082828
v  epsilon             1.6954e-05        1.65e+05          95.916          6.1786
v  TurbVisc            8.0936e-13         0.14181      0.00049637       0.0064295
v  total_pressure      4.5981e+05      5.2633e+05      5.1525e+05      5.1347e+05


 TIME FOR THE TIME STEP              146:        0.62758E+02

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


 INSTANT    0.147000000E+03   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        -0.340342592E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640826E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70079E+01 0.33735E+01
   Friction velocity        uet   :  0.17083E-01 0.26836E+01
   Friction velocity        uk    :  0.17077E-01 0.26381E+01
   Dimensionless distance   yplus :  0.52125E-04 0.84020E+01
   ------------------------------------------------------
  a  k           -8.6994e-06                             3
a  epsilon        -0.22309                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3577          9.3057         0.56457        0.076998
v  Velocity[Y]            -7.7082           8.308         0.24604         0.18575
v  Velocity[Z]            -13.914          12.091        -0.22181     -0.00059387
v  ǁVelocityǁ          2.0569e-05          16.558          1.5905          1.6148
v  Pressure                -40419           26449           15261           13483
v  k                   5.1932e-08          1.6476       0.0093491       0.0082842
v  epsilon             1.6614e-05      1.6346e+05          96.356          6.1919
v  TurbVisc            8.1638e-13         0.14181      0.00049763       0.0064297
v  total_pressure      4.5958e+05      5.2645e+05      5.1526e+05      5.1348e+05


 TIME FOR THE TIME STEP              148:        0.73737E+02

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


 INSTANT    0.149000000E+03   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        -0.354089451E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68428E+01 0.33932E+01
   Friction velocity        uet   :  0.85353E-02 0.26824E+01
   Friction velocity        uk    :  0.85319E-02 0.26422E+01
   Dimensionless distance   yplus :  0.51843E-04 0.84040E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3288
   Nb of faces within the viscous sub-layer     :      27322
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67394E+00     111   0.16641E+00   0.75407E+01 0.16047E+03 
c  Velocity[X]                                      0.22788E+01 
c  Velocity[Y]                                      0.24930E+01 
c  Velocity[Z]                                      0.27688E+01 
c  Pressure     0.26231E-01     914   0.35341E-02   0.23999E+00 0.57002E+03 
c  k            0.23963E-01      59   0.22659E-02   0.39764E-02 0.75306E+03 
c  epsilon      0.50049E+03      48   0.35782E-02   0.34284E+07 0.46584E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.5962e-06                             3
a  epsilon        -0.14741                             8


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3801          9.0892         0.56486        0.076961
v  Velocity[Y]            -7.7389          8.2552         0.24602         0.18578
v  Velocity[Z]            -13.996          11.849        -0.22203     -0.00055712
v  ǁVelocityǁ          2.0754e-05          16.509          1.5919          1.6148
v  Pressure                -40392           26465           15277           13494
v  k                   4.9969e-08          1.6576        0.009381       0.0082865
v  epsilon             1.6382e-05      1.6357e+05          96.775          6.2099
v  TurbVisc             8.188e-13         0.14181      0.00049823       0.0064299
v  total_pressure      4.5961e+05      5.2646e+05      5.1528e+05      5.1349e+05


 TIME FOR THE TIME STEP              149:        0.80444E+02

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


 INSTANT    0.150000000E+03   TIME STEP NUMBER             150
 ============================================================= 




   *a  k           -8.6994e-06                             3
a  epsilon        -0.22309                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3577          9.3057         0.56457        0.076998
v  Velocity[Y]            -7.7082           8.308         0.24604         0.18575
v  Velocity[Z]            -13.914          12.091        -0.22181     -0.00059387
v  ǁVelocityǁ          2.0569e-05          16.558          1.5905          1.6148
v  Pressure                -40419           26449           15261           13483
v  k                   5.1932e-08          1.6476       0.0093491       0.0082842
v  epsilon             1.6614e-05      1.6346e+05          96.356          6.1919
v  TurbVisc            8.1638e-13         0.14181      0.00049763       0.0064297
v  total_pressure      4.5958e+05      5.2645e+05      5.1526e+05      5.1348e+05


 TIME FOR THE TIME STEP              148:        0.63517E+02

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


 INSTANT    0.149000000E+03   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        -0.354089451E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68428E+01 0.33932E+01
   Friction velocity        uet   :  0.85353E-02 0.26824E+01
   Friction velocity        uk    :  0.
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.0665e-06                             3
a  epsilon        -0.48842                             8


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.363           9.227         0.56525        0.077023
v  Velocity[Y]            -7.4238          8.3129         0.24587         0.18571
v  Velocity[Z]            -13.594          12.669        -0.22217     -0.00046852
v  ǁVelocityǁ          2.0583e-05           16.24          1.5933          1.6149
v  Pressure                -40561           26421           15283           13503
v  k                   4.8153e-08          1.6546       0.0093864       0.0082872
v  epsilon             1.6189e-05      1.6185e+05          96.727          6.2093
v  TurbVisc            8.2078e-13         0.14181        0.000499         0.00643
v  total_pressure      4.5944e+05      5.2642e+05      5.1528e+05       5.135e+05


 TIME FOR THE TIME STEP              150:        0.67087E+02

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


 INSTANT    0.151000000E+03   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        -0.978542610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65078E+01 0.33886E+01
   Friction velocity        uet   :  0.12219E-01 0.26832E+01
   Friction velocity        uk    :  0.12117E-01 0.26398E+01
   Dimensionless distance   yplus :  0.51866E-04 0.84716E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3289
   Nb of faces within the viscous sub-layer     :      27319
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67507E+00     111   0.17131E+00   0.76140E+01 0.16100E+03 
c  Velocity[X]                                      0.24183E+01 
c  Velocity[Y]                                      0.24125E+01 
c  Velocity[Z]                                      0.27831E+01 
c  Pressure     0.26196E-01     612   0.36400E-02   0.23989E+00 0.91321E+03 
c  k            0.24040E-01      56   0.24351E-02   0.34032E-02 0.51381E+03 
c  epsilon      0.50311E+03      41   0.34629E-02   0.18646E+07 0.22418E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.4279e-06                             4
a  epsilon        -0.34129                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4237          9.4415         0.56551        0.077051
v  Velocity[Y]            -7.4827          8.2686          0.2458         0.18587
v  Velocity[Z]             -14.35          12.022        -0.22223     -0.00052883
v  ǁVelocityǁ          2.0567e-05          17.022          1.5946          1.6148
v  Pressure                -40566           26523           15320           13527
v  k                   4.6523e-08          1.6612       0.0094099         0.00829
v  epsilon             1.6038e-05      1.6289e+05          97.011          6.2266
v  TurbVisc            8.2201e-13         0.14181      0.00049964       0.0064301
v  total_pressure      4.5943e+05      5.2652e+05      5.1532e+05      5.1353e+05


 TIME FOR THE TIME STEP              151:        0.73074E+02

==========================================================
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.0665e-06                             3
a  epsilon        -0.48842                             8


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.363           9.227         0.56525        0.077023
v  Velocity[Y]            -7.4238          8.3129         0.24587         0.18571
v  Velocity[Z]            -13.594          12.669        -0.22217     -0.00046852
v  ǁVelocityǁ          2.0583e-05           16.24          1.5933          1.6149
v  Pressure                -40561           26421           15283           13503
v  k                   4.8153e-08          1.6546       0.0093864       0.0082872
v  epsilon             1.6189e-05      1.6185e+05          96.727          6.2093
v  TurbVisc            8.2078e-13         0.14181        0.000499         0.00643
v  total_pressure      4.5944e+05      5.2642e+05      5.1528e+05       5.135e+05


 TIME FOR THE TIME STEP              150:        0.62107E+02

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


 INSTANT    0.151000000E+03   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        -0.978542610E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.6167e-06                             4
a  epsilon         -0.3158                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3391           9.196         0.56567        0.076951
v  Velocity[Y]            -7.4255          8.3246         0.24558         0.18571
v  Velocity[Z]            -13.681          12.472        -0.22236     -0.00051069
v  ǁVelocityǁ          2.0722e-05          16.275          1.5959          1.6149
v  Pressure                -40941           26510           15318           13527
v  k                   4.5104e-08          1.6432       0.0094234       0.0082911
v  epsilon             1.5932e-05       1.637e+05          97.069           6.224
v  TurbVisc            8.2286e-13         0.14181      0.00050018       0.0064302
v  total_pressure      4.5906e+05      5.2651e+05      5.1532e+05      5.1353e+05


 TIME FOR THE TIME STEP              152:        0.76103E+02

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


 INSTANT    0.153000000E+03   TIME STEP NUMBER             153
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.248555716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65978E+01 0.33900E+01
   Friction velocity        uet   :  0.13801E-01 0.26809E+01
   Friction velocity        uk    :  0.13795E-01 0.26438E+01
   Dimensionless distance   yplus :  0.52059E-04 0.84797E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3298
   Nb of faces within the viscous sub-layer     :      27312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67506E+00     109   0.17037E+00   0.77285E+01 0.16322E+03 
c  Velocity[X]                                      0.23995E+01 
c  Velocity[Y]                                      0.23669E+01 
c  Velocity[Z]                                      0.29621E+01 
c  Pressure     0.25433E-01     587   0.35950E-02   0.23301E+00 0.42197E+03 
c  k            0.24073E-01      60   0.25750E-02   0.20682E-02 0.43003E+03 
c  epsilon      0.50192E+03      48   0.34061E-02   0.10849E+07 0.21271E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6841e-05                             8
a  epsilon         -0.2667                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3765          9.3369          0.5657         0.07697
v  Velocity[Y]            -7.4995          8.3118         0.24533         0.18584
v  Velocity[Z]            -14.125            11.7        -0.22259     -0.00050901
v  ǁVelocityǁ          2.0537e-05          16.751           1.597          1.6148
v  Pressure                -41062           26598           15312           13520
v  k                   2.6972e-08            1.64       0.0094415       0.0082948
v  epsilon              1.587e-05      1.6283e+05          97.107          6.2329
v  TurbVisc            8.2407e-13         0.14181      0.00050086       0.0064305
v  total_pressure      4.5894e+05       5.266e+05-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.6167e-06                             4
a  epsilon         -0.3158                             6


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3391           9.196         0.56567        0.076951
v  Velocity[Y]            -7.4255          8.3246         0.24558         0.18571
v  Velocity[Z]            -13.681          12.472        -0.22236     -0.00051069
v  ǁVelocityǁ          2.0722e-05          16.275          1.5959          1.6149
v  Pressure                -40941           26510           15318           13527
v  k                   4.5104e-08          1.6432       0.0094234       0.0082911
v  epsilon             1.5932e-05       1.637e+05          97.069           6.224
v  TurbVisc            8.2286e-13         0.14181      0.00050018       0.0064302
v  total_pressure      4.5906e+05      5.2651e+05      5.1532e+05      5.1353e+05


 TIME FOR THE TIME STEP              152:        0.69288E+02

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


 INSTANT    0.153000000E+03   TIME STEP NUMBER             153
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.248555716E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------c  k            0.24053E-01      55   0.22659E-02   0.16384E-02 0.35059E+03 
c  epsilon      0.50121E+03      39   0.23610E-02   0.49015E+06 0.14722E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.2745e-06                             3
a  epsilon        -0.24299                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.386          9.3541         0.56592        0.076916
v  Velocity[Y]            -7.5898          8.3545         0.24501         0.18581
v  Velocity[Z]            -13.688          13.016        -0.22271     -0.00052859
v  ǁVelocityǁ           2.036e-05          16.428          1.5982          1.6149
v  Pressure                -41351           26679           15328           13535
v  k                   4.2942e-08          1.6514        0.009445       0.0082954
v  epsilon             1.5847e-05      1.6426e+05          97.137          6.2301
v  TurbVisc            8.2392e-13         0.14181      0.00050136       0.0064308
v  total_pressure      4.5865e+05      5.2668e+05      5.1533e+05      5.1354e+05


 TIME FOR THE TIME STEP              154:        0.70339E+02

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


 INSTANT    0.155000000E+03   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.321181680E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640787E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66112E+01 0.33842E+01
   Friction velocity        uet   :  0.14381E-01 0.26760E+01
   Friction velocity        uk    :  0.14375E-01 0.26379E+01
   Dimensionless distance   yplus :  0.51559E-04 0.85345E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3297
   Nb of faces within the viscous sub-layer     :      27301
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67560E+00     109   0.16895E+00   0.77199E+01 0.16322E+03 
c  Velocity[X]                                      0.23989E+01 
c  Velocity[Y]                                      0.24991E+01 
c  Velocity[Z]                                      0.28218E+01 
c  Pressure     0.25699E-01     621   0.33188E-02   0.23557E+00 0.78836E+03 
c  k            0.24159E-01      56   0.30891E-02   0.38593E-02 0.57305E+03 
c  epsilon      0.50317E+03      38   0.35728E-02   0.20644E+07 0.30426E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.5995e-06                             6
a  epsilon        -0.23705                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3834          9.3719         0.56593        0.076859
v  Velocity[Y]            -7.7066           8.267         0.24475         0.18593
v  Velocity[Z]             -14.36          13.755        -0.22291     -0.00050356
v  ǁVelocityǁ          2.0541e-05          17.005          1.5993          1.6149
v  Pressure                -41427           26722           15339           13540
v  k                   4.2188e-08          1.6407       0.0094662       0.0083014
v  epsilon              1.586e-05      1.6187e+05          c  k            0.24053E-01      55   0.22659E-02   0.16384E-02 0.35059E+03 
c  epsilon      0.50121E+03      39   0.23610E-02   0.49015E+06 0.14722E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.2745e-06                             3
a  epsilon        -0.24299                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.386          9.3541         0.56592        0.076916
v  Velocity[Y]            -7.5898          8.3545         0.24501         0.18581
v  Velocity[Z]            -13.688          13.016        -0.22271     -0.00052859
v  ǁVelocityǁ           2.036e-05          16.428          1.5982          1.6149
v  Pressure                -41351           26679           15328           13535
v  k                   4.2942e-08          1.6514        0.009445       0.0082954
v  epsilon             1.5847e-05      1.6426e+05          97.137          6.2301
v  TurbVisc            8.2392e-13         0.14181      0.00050136       0.0064308
v  total_pressure      4.5865e+05      5.2668e+05      5.1533e+05      5.1354e+05


 TIME FOR THE TIME STEP              154:        0.67192E+02

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


 INSTANT    0.155000000E+03   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.321181680E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640787E+00
Free inlet               13           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[Z]                                      0.28772E+01 
c  Pressure     0.24193E-01     682   0.32201E-02   0.22114E+00 0.48163E+03 
c  k            0.24175E-01      59   0.48936E-02   0.32403E-02 0.55620E+03 
c  epsilon      0.50171E+03      42   0.87523E-02   0.20043E+07 0.30586E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.9904e-06                             3
a  epsilon        -0.23864                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3854          9.2183         0.56611        0.076881
v  Velocity[Y]            -7.5228          8.3589         0.24436         0.18593
v  Velocity[Z]            -13.563           12.58        -0.22329      -0.0004836
v  ǁVelocityǁ          2.0337e-05          16.157          1.6003          1.6148
v  Pressure                -41598           26719           15340           13541
v  k                   4.1631e-08          1.6507       0.0094886       0.0083012
v  epsilon             1.5905e-05      1.6382e+05          97.605           6.252
v  TurbVisc            8.2389e-13         0.14181      0.00050221       0.0064312
v  total_pressure       4.584e+05      5.2672e+05      5.1534e+05      5.1354e+05


 TIME FOR THE TIME STEP              156:        0.67615E+02

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


 INSTANT    0.157000000E+03   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        -0.357241625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64634E+01 0.33724E+01
   Friction velocity        uet   :  0.11851E-01 0.26787E+01
   Friction velocity        uk    :  0.11847E-01 0.26332E+01
   Dimensionless distance   yplus :  0.51528E-04 0.85808E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3296
   Nb of faces within the viscous sub-layer     :      27271
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67594E+00     108   0.16775E+00   0.75769E+01 0.16107E+03 
c  Velocity[X]                                      0.23851E+01 
c  Velocity[Y]                                      0.24434E+01 
c  Velocity[Z]                                      0.27483E+01 
c  Pressure     0.24132E-01     533   0.31252E-02   0.22138E+00 0.61513E+03 
c  k            0.24200E-01      53   0.27108E-02   0.30202E-02 0.59536E+03 
c  epsilon      0.50208E+03      39   0.34531E-02   0.25803E+07 0.43317E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.3764e-07                             1
a  epsilon        -0.24616                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3675          8.9875          0.5662        0.076902
v  Velocity[Y]            -7.5505          8.3181         0.24398         0.18603
v  Velocity[Z]            -14.138          12.514        -0.22351     -0.00045301
v  ǁVelocityǁ          2.0178e-05          16.388          1.6014          1.6148
v  Pressure                -41709           26796           15343           13542c  Velocity[Z]                                      0.28772E+01 
c  Pressure     0.24193E-01     682   0.32201E-02   0.22114E+00 0.48163E+03 
c  k            0.24175E-01      59   0.48936E-02   0.32403E-02 0.55620E+03 
c  epsilon      0.50171E+03      42   0.87523E-02   0.20043E+07 0.30586E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.9904e-06                             3
a  epsilon        -0.23864                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3854          9.2183         0.56611        0.076881
v  Velocity[Y]            -7.5228          8.3589         0.24436         0.18593
v  Velocity[Z]            -13.563           12.58        -0.22329      -0.0004836
v  ǁVelocityǁ          2.0337e-05          16.157          1.6003          1.6148
v  Pressure                -41598           26719           15340           13541
v  k                   4.1631e-08          1.6507       0.0094886       0.0083012
v  epsilon             1.5905e-05      1.6382e+05          97.605           6.252
v  TurbVisc            8.2389e-13         0.14181      0.00050221       0.0064312
v  total_pressure       4.584e+05      5.2672e+05      5.1534e+05      5.1354e+05


 TIME FOR THE TIME STEP              156:        0.69136E+02

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


 INSTANT    0.157000000E+03   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        -0.357241625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640788E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15   c  Velocity     0.67595E+00     106   0.16933E+00   0.74653E+01 0.16099E+03 
c  Velocity[X]                                      0.22992E+01 
c  Velocity[Y]                                      0.23194E+01 
c  Velocity[Z]                                      0.28466E+01 
c  Pressure     0.23643E-01     627   0.31529E-02   0.21651E+00 0.93802E+03 
c  k            0.24225E-01      59   0.28273E-02   0.28864E-02 0.53056E+03 
c  epsilon      0.50337E+03      44   0.37754E-02   0.20397E+07 0.37305E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1412e-06                             2
a  epsilon        -0.24054                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3717          9.1026         0.56634        0.076774
v  Velocity[Y]            -7.5415          8.3981         0.24373         0.18598
v  Velocity[Z]            -13.586          12.993        -0.22398      -0.0004609
v  ǁVelocityǁ          2.0423e-05          16.173          1.6024          1.6148
v  Pressure                -41868           26779           15372           13563
v  k                   4.0766e-08          1.6428       0.0095401       0.0083098
v  epsilon             1.6069e-05      1.6246e+05          98.101          6.2809
v  TurbVisc            8.2266e-13         0.14181      0.00050316       0.0064316
v  total_pressure      4.5813e+05      5.2678e+05      5.1537e+05      5.1356e+05


 TIME FOR THE TIME STEP              158:        0.65401E+02

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


 INSTANT    0.159000000E+03   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        -0.407817231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640854E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65102E+01 0.33895E+01
   Friction velocity        uet   :  0.12875E-01 0.26756E+01
   Friction velocity        uk    :  0.12870E-01 0.26302E+01
   Dimensionless distance   yplus :  0.51652E-04 0.86124E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3306
   Nb of faces within the viscous sub-layer     :      27236
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67601E+00     107   0.17050E+00   0.76725E+01 0.16107E+03 
c  Velocity[X]                                      0.23761E+01 
c  Velocity[Y]                                      0.24153E+01 
c  Velocity[Z]                                      0.28810E+01 
c  Pressure     0.23398E-01     808   0.30416E-02   0.21553E+00 0.11685E+04 
c  k            0.24282E-01      55   0.33000E-02   0.36717E-02 0.50433E+03 
c  epsilon      0.50378E+03      42   0.44227E-02   0.16083E+07 0.21044E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3787e-06                             2
a  epsilon        -0.24895                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3722          9.3442         0.56636        0.076692
v  Velocity[Y]            -7.4642          8.3351         0.24331         0.18615
v  Velocity[Z]             -14.01       c  Velocity     0.67595E+00     106   0.16933E+00   0.74653E+01 0.16099E+03 
c  Velocity[X]                                      0.22992E+01 
c  Velocity[Y]                                      0.23194E+01 
c  Velocity[Z]                                      0.28466E+01 
c  Pressure     0.23643E-01     627   0.31529E-02   0.21651E+00 0.93802E+03 
c  k            0.24225E-01      59   0.28273E-02   0.28864E-02 0.53056E+03 
c  epsilon      0.50337E+03      44   0.37754E-02   0.20397E+07 0.37305E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1412e-06                             2
a  epsilon        -0.24054                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3717          9.1026         0.56634        0.076774
v  Velocity[Y]            -7.5415          8.3981         0.24373         0.18598
v  Velocity[Z]            -13.586          12.993        -0.22398      -0.0004609
v  ǁVelocityǁ          2.0423e-05          16.173          1.6024          1.6148
v  Pressure                -41868           26779           15372           13563
v  k                   4.0766e-08          1.6428       0.0095401       0.0083098
v  epsilon             1.6069e-05      1.6246e+05          98.101          6.2809
v  TurbVisc            8.2266e-13         0.14181      0.00050316       0.0064316
v  total_pressure      4.5813e+05      5.2678e+05      5.1537e+05      5.1356e+05


 TIME FOR THE TIME STEP              158:        0.63394E+02

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


 INSTANT    0.159000000E+03   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        -0.407817231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67580E+00     106   0.16647E+00   0.77939E+01 0.16520E+03 
c  Velocity[X]                                      0.23871E+01 
c  Velocity[Y]                                      0.24165E+01 
c  Velocity[Z]                                      0.29903E+01 
c  Pressure     0.22952E-01     563   0.29182E-02   0.21060E+00 0.53247E+03 
c  k            0.24255E-01      53   0.47706E-02   0.25464E-02 0.41365E+03 
c  epsilon      0.50237E+03      36   0.91443E-02   0.11154E+07 0.18142E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7075e-06                             2
a  epsilon        -0.23299                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4059          9.1414         0.56629        0.076638
v  Velocity[Y]            -7.4378          8.3285         0.24297         0.18611
v  Velocity[Z]              -13.6          12.313        -0.22472     -0.00045457
v  ǁVelocityǁ          2.0133e-05          16.181          1.6036          1.6147
v  Pressure                -42095           26746           15347           13545
v  k                   4.0343e-08          1.6463       0.0095526       0.0083156
v  epsilon             1.6302e-05      1.6142e+05          98.109          6.2848
v  TurbVisc            8.2137e-13         0.14181      0.00050393       0.0064321
v  total_pressure      4.5791e+05      5.2675e+05      5.1535e+05      5.1354e+05


 TIME FOR THE TIME STEP              160:        0.61672E+02

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


 INSTANT    0.161000000E+03   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         0.624131579E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640802E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65240E+01 0.33885E+01
   Friction velocity        uet   :  0.12230E-01 0.26768E+01
   Friction velocity        uk    :  0.12203E-01 0.26307E+01
   Dimensionless distance   yplus :  0.51248E-04 0.86174E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3297
   Nb of faces within the viscous sub-layer     :      27190
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67592E+00     107   0.16800E+00   0.75846E+01 0.16250E+03 
c  Velocity[X]                                      0.23960E+01 
c  Velocity[Y]                                      0.22880E+01 
c  Velocity[Z]                                      0.29006E+01 
c  Pressure     0.22415E-01     537   0.26014E-02   0.20630E+00 0.54708E+03 
c  k            0.24293E-01      54   0.24329E-02   0.27787E-02 0.45534E+03 
c  epsilon      0.50342E+03      38   0.27360E-02   0.10007E+07 0.18680E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5689e-06                             2
a  epsilon        -0.24973                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3763          9.272   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67580E+00     106   0.16647E+00   0.77939E+01 0.16520E+03 
c  Velocity[X]                                      0.23871E+01 
c  Velocity[Y]                                      0.24165E+01 
c  Velocity[Z]                                      0.29903E+01 
c  Pressure     0.22952E-01     563   0.29182E-02   0.21060E+00 0.53247E+03 
c  k            0.24255E-01      53   0.47706E-02   0.25464E-02 0.41365E+03 
c  epsilon      0.50237E+03      36   0.91443E-02   0.11154E+07 0.18142E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7075e-06                             2
a  epsilon        -0.23299                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4059          9.1414         0.56629        0.076638
v  Velocity[Y]            -7.4378          8.3285         0.24297         0.18611
v  Velocity[Z]              -13.6          12.313        -0.22472     -0.00045457
v  ǁVelocityǁ          2.0133e-05          16.181          1.6036          1.6147
v  Pressure                -42095           26746           15347           13545
v  k                   4.0343e-08          1.6463       0.0095526       0.0083156
v  epsilon             1.6302e-05      1.6142e+05          98.109          6.2848
v  TurbVisc            8.2137e-13         0.14181      0.00050393       0.0064321
v  total_pressure      4.5791e+05      5.2675e+05      5.1535e+05      5.1354e+05


 TIME FOR THE TIME STEP              160:        0.61697E+02

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


 INSTANT    0.161000000E+03   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.   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67620E+00     106   0.17019E+00   0.74595E+01 0.16103E+03 
c  Velocity[X]                                      0.24322E+01 
c  Velocity[Y]                                      0.22420E+01 
c  Velocity[Z]                                      0.27853E+01 
c  Pressure     0.22069E-01     592   0.25785E-02   0.20178E+00 0.46266E+03 
c  k            0.24329E-01      55   0.25571E-02   0.23232E-02 0.52511E+03 
c  epsilon      0.50549E+03      37   0.32296E-02   0.22621E+07 0.41836E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3478e-06                             2
a  epsilon        -0.23589                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3506          9.0865         0.56621        0.076624
v  Velocity[Y]            -7.7202          8.3756         0.24219         0.18601
v  Velocity[Z]              -13.5          12.917        -0.22529     -0.00043028
v  ǁVelocityǁ            2.01e-05          16.021          1.6048          1.6149
v  Pressure                -42186           26752           15377           13569
v  k                   4.0384e-08          1.6449       0.0095992       0.0083245
v  epsilon             1.6579e-05      1.6321e+05          98.694          6.3099
v  TurbVisc            8.1904e-13         0.14181       0.0005049       0.0064329
v  total_pressure      4.5781e+05      5.2675e+05      5.1538e+05      5.1357e+05


 TIME FOR THE TIME STEP              162:        0.62806E+02

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


 INSTANT    0.163000000E+03   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        -0.331190815E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640855E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64252E+01 0.33762E+01
   Friction velocity        uet   :  0.20406E-01 0.26767E+01
   Friction velocity        uk    :  0.20330E-01 0.26278E+01
   Dimensionless distance   yplus :  0.51219E-04 0.86138E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3306
   Nb of faces within the viscous sub-layer     :      27166
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67594E+00     108   0.16913E+00   0.74113E+01 0.15951E+03 
c  Velocity[X]                                      0.23542E+01 
c  Velocity[Y]                                      0.23745E+01 
c  Velocity[Z]                                      0.26826E+01 
c  Pressure     0.22249E-01     755   0.29986E-02   0.20403E+00 0.29516E+03 
c  k            0.24377E-01      60   0.27567E-02   0.33857E-02 0.55501E+03 
c  epsilon      0.50599E+03      45   0.34954E-02   0.20675E+07 0.30778E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -1.108e-05                             2
a  epsilon        -0.24841                             2


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

   field                  minimum         maximum        set mean      ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67620E+00     106   0.17019E+00   0.74595E+01 0.16103E+03 
c  Velocity[X]                                      0.24322E+01 
c  Velocity[Y]                                      0.22420E+01 
c  Velocity[Z]                                      0.27853E+01 
c  Pressure     0.22069E-01     592   0.25785E-02   0.20178E+00 0.46266E+03 
c  k            0.24329E-01      55   0.25571E-02   0.23232E-02 0.52511E+03 
c  epsilon      0.50549E+03      37   0.32296E-02   0.22621E+07 0.41836E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3478e-06                             2
a  epsilon        -0.23589                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3506          9.0865         0.56621        0.076624
v  Velocity[Y]            -7.7202          8.3756         0.24219         0.18601
v  Velocity[Z]              -13.5          12.917        -0.22529     -0.00043028
v  ǁVelocityǁ            2.01e-05          16.021          1.6048          1.6149
v  Pressure                -42186           26752           15377           13569
v  k                   4.0384e-08          1.6449       0.0095992       0.0083245
v  epsilon             1.6579e-05      1.6321e+05          98.694          6.3099
v  TurbVisc            8.1904e-13         0.14181       0.0005049       0.0064329
v  total_pressure      4.5781e+05      5.2675e+05      5.1538e+05      5.1357e+05


 TIME FOR THE TIME STEP              162:        0.58324E+02

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


 INSTANT    0.163000000E+03   TIME STEP NUMBER             163
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Ma   Nb of faces within the viscous sub-layer     :      27151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67608E+00     108   0.16433E+00   0.76971E+01 0.16480E+03 
c  Velocity[X]                                      0.25345E+01 
c  Velocity[Y]                                      0.23311E+01 
c  Velocity[Z]                                      0.28314E+01 
c  Pressure     0.21693E-01     640   0.26210E-02   0.19823E+00 0.32633E+03 
c  k            0.24403E-01      58   0.46357E-02   0.48302E-02 0.74132E+03 
c  epsilon      0.50559E+03      45   0.90659E-02   0.49118E+07 0.50816E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6594e-05                             3
a  epsilon        -0.23217                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4824          9.2537         0.56625        0.076715
v  Velocity[Y]            -7.6421          8.3406         0.24155         0.18611
v  Velocity[Z]             -13.42          12.501        -0.22598     -0.00037115
v  ǁVelocityǁ          1.9993e-05          15.934          1.6057           1.615
v  Pressure                -42199           26716           15364           13555
v  k                    4.066e-08            1.64       0.0096323        0.008332
v  epsilon             1.6879e-05      1.6285e+05          98.877          6.3308
v  TurbVisc            8.1563e-13         0.14181      0.00050548       0.0064339
v  total_pressure       4.578e+05      5.2672e+05      5.1536e+05      5.1355e+05


 TIME FOR THE TIME STEP              164:        0.68757E+02

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


 INSTANT    0.165000000E+03   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        -0.867801343E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63302E+01 0.33889E+01
   Friction velocity        uet   :  0.15557E-01 0.26774E+01
   Friction velocity        uk    :  0.15155E-01 0.26348E+01
   Dimensionless distance   yplus :  0.51109E-04 0.85937E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3315
   Nb of faces within the viscous sub-layer     :      27131
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67690E+00     107   0.16535E+00   0.73862E+01 0.15962E+03 
c  Velocity[X]                                      0.23525E+01 
c  Velocity[Y]                                      0.21663E+01 
c  Velocity[Z]                                      0.28673E+01 
c  Pressure     0.22150E-01     639   0.28498E-02   0.20277E+00 0.37724E+03 
c  k            0.24409E-01      57   0.25668E-02   0.21604E-02 0.39584E+03 
c  epsilon      0.50426E+03      43   0.33553E-02   0.86739E+06 0.18127E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7791e-05                             2
a    Nb of faces within the viscous sub-layer     :      27151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67608E+00     108   0.16433E+00   0.76971E+01 0.16480E+03 
c  Velocity[X]                                      0.25345E+01 
c  Velocity[Y]                                      0.23311E+01 
c  Velocity[Z]                                      0.28314E+01 
c  Pressure     0.21693E-01     640   0.26210E-02   0.19823E+00 0.32633E+03 
c  k            0.24403E-01      58   0.46357E-02   0.48302E-02 0.74132E+03 
c  epsilon      0.50559E+03      45   0.90659E-02   0.49118E+07 0.50816E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6594e-05                             3
a  epsilon        -0.23217                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4824          9.2537         0.56625        0.076715
v  Velocity[Y]            -7.6421          8.3406         0.24155         0.18611
v  Velocity[Z]             -13.42          12.501        -0.22598     -0.00037115
v  ǁVelocityǁ          1.9993e-05          15.934          1.6057           1.615
v  Pressure                -42199           26716           15364           13555
v  k                    4.066e-08            1.64       0.0096323        0.008332
v  epsilon             1.6879e-05      1.6285e+05          98.877          6.3308
v  TurbVisc            8.1563e-13         0.14181      0.00050548       0.0064339
v  total_pressure       4.578e+05      5.2672e+05      5.1536e+05      5.1355e+05


 TIME FOR THE TIME STEP              164:        0.73078E+02

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


 INSTANT    0.165000000E+03   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.50744E-04 0.84957E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3319
   Nb of faces within the viscous sub-layer     :      27127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67709E+00     108   0.16625E+00   0.76207E+01 0.16024E+03 
c  Velocity[X]                                      0.23860E+01 
c  Velocity[Y]                                      0.23085E+01 
c  Velocity[Z]                                      0.29262E+01 
c  Pressure     0.21697E-01     717   0.25853E-02   0.19851E+00 0.89470E+03 
c  k            0.24398E-01      54   0.25630E-02   0.25544E-02 0.41597E+03 
c  epsilon      0.50424E+03      41   0.28173E-02   0.10103E+07 0.17086E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2844e-05                             2
a  epsilon        -0.21466                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3596          9.1872         0.56644        0.076654
v  Velocity[Y]            -7.5879          8.3864         0.24122         0.18606
v  Velocity[Z]            -13.114          12.564        -0.22657     -0.00036918
v  ǁVelocityǁ          1.9652e-05          15.797          1.6066          1.6154
v  Pressure                -41911           26755           15392           13573
v  k                   4.0998e-08          1.6401       0.0096477       0.0083391
v  epsilon             1.7176e-05      1.6175e+05          98.901          6.3365
v  TurbVisc            8.1212e-13         0.14181      0.00050601       0.0064346
v  total_pressure      4.5809e+05      5.2676e+05      5.1539e+05      5.1357e+05


 TIME FOR THE TIME STEP              166:        0.70546E+02

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


 INSTANT    0.167000000E+03   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        -0.354946107E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59973E+01 0.33829E+01
   Friction velocity        uet   :  0.19790E-01 0.26754E+01
   Friction velocity        uk    :  0.19789E-01 0.26283E+01
   Dimensionless distance   yplus :  0.50629E-04 0.85810E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3322
   Nb of faces within the viscous sub-layer     :      27121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67744E+00     108   0.16949E+00   0.73257E+01 0.15868E+03 
c  Velocity[X]                                      0.22781E+01 
c  Velocity[Y]                                      0.23030E+01 
c  Velocity[Z]                                      0.27446E+01 
c  Pressure     0.22322E-01     539   0.26240E-02   0.20368E+00 0.41647E+03 
c  k            0.24469E-01      56   0.28674E-02   0.33362E-02 0.58118E+03 
c  epsilon      0.50646E+03      38   0.38756E-02   0.30487E+07 0.43589E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initia   Dimensionless distance   yplus :  0.50744E-04 0.84957E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3319
   Nb of faces within the viscous sub-layer     :      27127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67709E+00     108   0.16625E+00   0.76207E+01 0.16024E+03 
c  Velocity[X]                                      0.23860E+01 
c  Velocity[Y]                                      0.23085E+01 
c  Velocity[Z]                                      0.29262E+01 
c  Pressure     0.21697E-01     717   0.25853E-02   0.19851E+00 0.89470E+03 
c  k            0.24398E-01      54   0.25630E-02   0.25544E-02 0.41597E+03 
c  epsilon      0.50424E+03      41   0.28173E-02   0.10103E+07 0.17086E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2844e-05                             2
a  epsilon        -0.21466                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3596          9.1872         0.56644        0.076654
v  Velocity[Y]            -7.5879          8.3864         0.24122         0.18606
v  Velocity[Z]            -13.114          12.564        -0.22657     -0.00036918
v  ǁVelocityǁ          1.9652e-05          15.797          1.6066          1.6154
v  Pressure                -41911           26755           15392           13573
v  k                   4.0998e-08          1.6401       0.0096477       0.0083391
v  epsilon             1.7176e-05      1.6175e+05          98.901          6.3365
v  TurbVisc            8.1212e-13         0.14181      0.00050601       0.0064346
v  total_pressure      4.5809e+05      5.2676e+05      5.1539e+05      5.1357e+05


 TIME FOR THE TIME STEP              166:        0.61877E+02

=========================   Rel velocity at the wall uiptn : -0.70564E+01 0.33923E+01
   Friction velocity        uet   :  0.19925E-01 0.26911E+01
   Friction velocity        uk    :  0.19234E-01 0.26087E+01
   Dimensionless distance   yplus :  0.51004E-04 0.85017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3322
   Nb of faces within the viscous sub-layer     :      27095
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67785E+00     108   0.17277E+00   0.76328E+01 0.16243E+03 
c  Velocity[X]                                      0.23675E+01 
c  Velocity[Y]                                      0.23431E+01 
c  Velocity[Z]                                      0.29222E+01 
c  Pressure     0.20840E-01     526   0.26162E-02   0.18987E+00 0.15039E+03 
c  k            0.24483E-01      59   0.46926E-02   0.36826E-02 0.53046E+03 
c  epsilon      0.50715E+03      45   0.88356E-02   0.17498E+07 0.22498E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8953e-05                             4
a  epsilon        -0.21833                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3499          9.2601         0.56704        0.076625
v  Velocity[Y]            -7.6181          8.3541         0.24124           0.186
v  Velocity[Z]            -13.233          12.411        -0.22728     -0.00043375
v  ǁVelocityǁ          1.9582e-05          15.926          1.6075          1.6158
v  Pressure                -41662           26659           15391           13575
v  k                   4.1293e-08          1.6517       0.0096919       0.0083457
v  epsilon             1.7451e-05      1.6403e+05          99.725          6.3593
v  TurbVisc            8.0803e-13         0.14181      0.00050665       0.0064357
v  total_pressure      4.5834e+05      5.2666e+05      5.1539e+05      5.1357e+05


 TIME FOR THE TIME STEP              168:        0.63755E+02

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


 INSTANT    0.169000000E+03   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        -0.136131507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640848E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61179E+01 0.33733E+01
   Friction velocity        uet   :  0.19582E-01 0.26745E+01
   Friction velocity        uk    :  0.19581E-01 0.26310E+01
   Dimensionless distance   yplus :  0.50543E-04 0.85827E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3322
   Nb of faces within the viscous sub-layer     :      27100
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67709E+00     110   0.16676E+00   0.78138E+01 0.16255E+03 
c  Velocity[X]                                      0.24064E+01 
c  Velocity[Y]                                      0.25816E+01 
c  Velocity[Z]                                      0.28258E+01 
c  Pressure     0.22188E-01     662   0.28582E-02   0.20241E+00 0.41609E+03 
c  k            0.24478E-01      55   0.28945E-02   0.20594E-02 0.48349E+03 
c  epsilon      0.50594E+03      38   0.37998E-02   0.18096E+07 0.36515   Rel velocity at the wall uiptn : -0.70564E+01 0.33923E+01
   Friction velocity        uet   :  0.19925E-01 0.26911E+01
   Friction velocity        uk    :  0.19234E-01 0.26087E+01
   Dimensionless distance   yplus :  0.51004E-04 0.85017E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3322
   Nb of faces within the viscous sub-layer     :      27095
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67785E+00     108   0.17277E+00   0.76328E+01 0.16243E+03 
c  Velocity[X]                                      0.23675E+01 
c  Velocity[Y]                                      0.23431E+01 
c  Velocity[Z]                                      0.29222E+01 
c  Pressure     0.20840E-01     526   0.26162E-02   0.18987E+00 0.15039E+03 
c  k            0.24483E-01      59   0.46926E-02   0.36826E-02 0.53046E+03 
c  epsilon      0.50715E+03      45   0.88356E-02   0.17498E+07 0.22498E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8953e-05                             4
a  epsilon        -0.21833                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3499          9.2601         0.56704        0.076625
v  Velocity[Y]            -7.6181          8.3541         0.24124           0.186
v  Velocity[Z]            -13.233          12.411        -0.22728     -0.00043375
v  ǁVelocityǁ          1.9582e-05          15.926          1.6075          1.6158
v  Pressure                -41662           26659           15391           13575
v  k                   4.1293e-08          1.6517       0.0096919       0.0083457
v  epsilon             1.7451e-05      1.6403e+05          99.725          6.3593
v  TurbVisc            8.0803e-13         0.14181      0.00050665     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71758E+01 0.33909E+01
   Friction velocity        uet   :  0.19515E-01 0.26892E+01
   Friction velocity        uk    :  0.19514E-01 0.26068E+01
   Dimensionless distance   yplus :  0.50314E-04 0.84953E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3336
   Nb of faces within the viscous sub-layer     :      27090
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67731E+00     109   0.16372E+00   0.73800E+01 0.16069E+03 
c  Velocity[X]                                      0.22810E+01 
c  Velocity[Y]                                      0.23277E+01 
c  Velocity[Z]                                      0.27713E+01 
c  Pressure     0.21792E-01     642   0.27875E-02   0.19789E+00 0.44831E+03 
c  k            0.24471E-01      58   0.25858E-02   0.18358E-02 0.37961E+03 
c  epsilon      0.50707E+03      45   0.29345E-02   0.74138E+06 0.17731E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3355e-05                             4
a  epsilon        -0.19217                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3408          9.0817         0.56762        0.076701
v  Velocity[Y]            -7.6792          8.3629         0.24136         0.18601
v  Velocity[Z]            -13.302          13.046        -0.22758     -0.00038352
v  ǁVelocityǁ          1.9627e-05          15.755          1.6081          1.6164
v  Pressure                -41587           26548           15403           13588
v  k                   4.1483e-08          1.6474       0.0096938       0.0083501
v  epsilon             1.7683e-05      1.6392e+05          99.415          6.3594
v  TurbVisc            8.0341e-13         0.14181      0.00050717       0.0064365
v  total_pressure      4.5841e+05      5.2655e+05       5.154e+05      5.1359e+05


 TIME FOR THE TIME STEP              170:        0.70682E+02

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


 INSTANT    0.171000000E+03   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        -0.232907963E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62103E+01 0.33892E+01
   Friction velocity        uet   :  0.19327E-01 0.26760E+01
   Friction velocity        uk    :  0.19326E-01 0.26215E+01
   Dimensionless distance   yplus :  0.50623E-04 0.85872E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3334
   Nb of faces within the viscous sub-layer     :      27075
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67819E+00     108   0.17071E+00   0.72868E+01 0.15883E+03 
c  Velocity[X]                                      0.22789E+01 
c  Velocity[Y]                                      0.22740E+01 
c  Velocity[Z]                                      0.27339E+01 
c  Pressure     0.23099E-01     555   0.28------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71758E+01 0.33909E+01
   Friction velocity        uet   :  0.19515E-01 0.26892E+01
   Friction velocity        uk    :  0.19514E-01 0.26068E+01
   Dimensionless distance   yplus :  0.50314E-04 0.84953E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3336
   Nb of faces within the viscous sub-layer     :      27090
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67731E+00     109   0.16372E+00   0.73800E+01 0.16069E+03 
c  Velocity[X]                                      0.22810E+01 
c  Velocity[Y]                                      0.23277E+01 
c  Velocity[Z]                                      0.27713E+01 
c  Pressure     0.21792E-01     642   0.27875E-02   0.19789E+00 0.44831E+03 
c  k            0.24471E-01      58   0.25858E-02   0.18358E-02 0.37961E+03 
c  epsilon      0.50707E+03      45   0.29345E-02   0.74138E+06 0.17731E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3355e-05                             4
a  epsilon        -0.19217                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3408          9.0817         0.56762        0.076701
v  Velocity[Y]            -7.6792          8.3629         0.24136         0.18601
v  Velocity[Z]            -13.302          13.046        -0.22758     -0.00038352
v  ǁVelocityǁ          1.9627e-05          15.755          1.6081          1.6164
v  Pressure                -41587           26548           15403           13588
v  k                   4.1483e-08          1.6474       0.0096938       0.0083501
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83103E+01 0.33740E+01
   Friction velocity        uet   :  0.12162E-01 0.26864E+01
   Friction velocity        uk    :  0.12261E-01 0.26046E+01
   Dimensionless distance   yplus :  0.50363E-04 0.87942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3341
   Nb of faces within the viscous sub-layer     :      27072
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67799E+00     108   0.16804E+00   0.76114E+01 0.16444E+03 
c  Velocity[X]                                      0.23948E+01 
c  Velocity[Y]                                      0.22964E+01 
c  Velocity[Z]                                      0.29202E+01 
c  Pressure     0.21380E-01     553   0.26727E-02   0.19482E+00 0.30842E+03 
c  k            0.24552E-01      55   0.23545E-02   0.29019E-02 0.64050E+03 
c  epsilon      0.50766E+03      44   0.37198E-02   0.33527E+07 0.48400E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1052e-05                             4
a  epsilon        -0.20484                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3343          8.9489         0.56841         0.07662
v  Velocity[Y]             -7.708          8.3374         0.24163         0.18601
v  Velocity[Z]            -13.458          13.724         -0.2278     -0.00040312
v  ǁVelocityǁ          1.9288e-05          15.966          1.6085          1.6168
v  Pressure                -41380           26591           15403           13588
v  k                   4.1552e-08          1.6569       0.0097116       0.0083567
v  epsilon             1.7856e-05      1.6113e+05          99.824          6.3721
v  TurbVisc            7.9986e-13         0.14181      0.00050789       0.0064376
v  total_pressure      4.5862e+05      5.2659e+05       5.154e+05      5.1359e+05


 TIME FOR THE TIME STEP              172:        0.60598E+02

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


 INSTANT    0.173000000E+03   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        -0.226863834E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640850E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63946E+01 0.33822E+01
   Friction velocity        uet   :  0.18790E-01 0.26734E+01
   Friction velocity        uk    :  0.18789E-01 0.26205E+01
   Dimensionless distance   yplus :  0.50171E-04 0.85879E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3335
   Nb of faces within the viscous sub-layer     :      27058
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67799E+00     108   0.16777E+00   0.75192E+01 0.16093E+03 
c  Velocity[X]                                      0.23455E+01 
c  Velocity[Y]      ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83103E+01 0.33740E+01
   Friction velocity        uet   :  0.12162E-01 0.26864E+01
   Friction velocity        uk    :  0.12261E-01 0.26046E+01
   Dimensionless distance   yplus :  0.50363E-04 0.87942E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3341
   Nb of faces within the viscous sub-layer     :      27072
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67799E+00     108   0.16804E+00   0.76114E+01 0.16444E+03 
c  Velocity[X]                                      0.23948E+01 
c  Velocity[Y]                                      0.22964E+01 
c  Velocity[Z]                                      0.29202E+01 
c  Pressure     0.21380E-01     553   0.26727E-02   0.19482E+00 0.30842E+03 
c  k            0.24552E-01      55   0.23545E-02   0.29019E-02 0.64050E+03 
c  epsilon      0.50766E+03      44   0.37198E-02   0.33527E+07 0.48400E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1052e-05                             4
a  epsilon        -0.20484                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3343          8.9489         0.56841         0.07662
v  Velocity[Y]             -7.708          8.3374         0.24163         0.18601
v  Velocity[Z]            -13.458          13.724         -0.2278     -0.00040312
v  ǁVelocityǁ          1.9288e-05          15.966     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71673E+01 0.33895E+01
   Friction velocity        uet   :  0.18252E-01 0.26906E+01
   Friction velocity        uk    :  0.18251E-01 0.26085E+01
   Dimensionless distance   yplus :  0.50388E-04 0.85127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3341
   Nb of faces within the viscous sub-layer     :      27055
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67878E+00     108   0.17196E+00   0.75915E+01 0.16176E+03 
c  Velocity[X]                                      0.23622E+01 
c  Velocity[Y]                                      0.23137E+01 
c  Velocity[Z]                                      0.29157E+01 
c  Pressure     0.22538E-01     619   0.34789E-02   0.20436E+00 0.38596E+03 
c  k            0.24560E-01      53   0.49274E-02   0.38476E-02 0.70584E+03 
c  epsilon      0.50646E+03      39   0.10635E-01   0.59235E+07 0.54273E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0276e-05                             3
a  epsilon        -0.21388                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2553          9.1773         0.56934        0.076642
v  Velocity[Y]            -7.6205          8.3962         0.24187         0.18601
v  Velocity[Z]            -13.486          13.067        -0.22739     -0.00040498
v  ǁVelocityǁ          1.9377e-05          16.009          1.6088          1.6174
v  Pressure                -41233           26728           15420           13602
v  k                   4.1503e-08          1.6514       0.0097232       0.0083641
v  epsilon             1.7962e-05      1.6362e+05          100.07          6.3809
v  TurbVisc            7.9712e-13         0.14181      0.00050835       0.0064387
v  total_pressure      4.5877e+05      5.2673e+05      5.1542e+05       5.136e+05


 TIME FOR THE TIME STEP              174:        0.67295E+02

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


 INSTANT    0.175000000E+03   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        -0.261578522E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64124E+01 0.33726E+01
   Friction velocity        uet   :  0.18084E-01 0.26754E+01
   Friction velocity        uk    :  0.18083E-01 0.26419E+01
   Dimensionless distance   yplus :  0.50272E-04 0.85935E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3337
   Nb of faces within the viscous sub-layer     :      27047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71673E+01 0.33895E+01
   Friction velocity        uet   :  0.18252E-01 0.26906E+01
   Friction velocity        uk    :  0.18251E-01 0.26085E+01
   Dimensionless distance   yplus :  0.50388E-04 0.85127E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3341
   Nb of faces within the viscous sub-layer     :      27055
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67878E+00     108   0.17196E+00   0.75915E+01 0.16176E+03 
c  Velocity[X]                                      0.23622E+01 
c  Velocity[Y]                                      0.23137E+01 
c  Velocity[Z]                                      0.29157E+01 
c  Pressure     0.22538E-01     619   0.34789E-02   0.20436E+00 0.38596E+03 
c  k            0.24560E-01      53   0.49274E-02   0.38476E-02 0.70584E+03 
c  epsilon      0.50646E+03      39   0.10635E-01   0.59235E+07 0.54273E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0276e-05                             3
a  epsilon        -0.21388                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2553          9.1773         0.56934        0.076642
v  Velocity[Y]            -7Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640850E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70678E+01 0.33911E+01
   Friction velocity        uet   :  0.17843E-01 0.26930E+01
   Friction velocity        uk    :  0.17842E-01 0.26105E+01
   Dimensionless distance   yplus :  0.50023E-04 0.85112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3348
   Nb of faces within the viscous sub-layer     :      27042
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67836E+00     107   0.16793E+00   0.73558E+01 0.15983E+03 
c  Velocity[X]                                      0.22322E+01 
c  Velocity[Y]                                      0.23461E+01 
c  Velocity[Z]                                      0.27776E+01 
c  Pressure     0.22873E-01     571   0.29585E-02   0.20609E+00 0.17333E+03 
c  k            0.24632E-01      54   0.28326E-02   0.25820E-02 0.48766E+03 
c  epsilon      0.50798E+03      40   0.42335E-02   0.16463E+07 0.29290E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.4314e-05                             4
a  epsilon        -0.22012                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4874           9.313         0.56998        0.076543
v  Velocity[Y]            -7.6687           8.389         0.24232         0.18602
v  Velocity[Z]            -13.779          12.908        -0.22698     -0.00040961
v  ǁVelocityǁ          1.9369e-05          16.393          1.6088          1.6177
v  Pressure                -41151           26794           15411           13594
v  k                   2.6607e-09          1.6527       0.0097259       0.0083723
v  epsilon             1.8006e-05      1.6422e+05          99.668          6.3925
v  TurbVisc            7.9429e-13         0.14181      0.00050879         0.00644
v  total_pressure      4.5885e+05      5.2679e+05      5.1541e+05      5.1359e+05


 TIME FOR THE TIME STEP              176:        0.68505E+02

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


 INSTANT    0.177000000E+03   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        -0.201554102E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640853E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.67191E+01 0.33868E+01
   Friction velocity        uet   :  0.16874E-01 0.26754E+01
   Friction velocity        uk    :  0.16687E-01 0.26320E+01
   Dimensionless distance   yplus :  0.50289E-04 0.86211E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3346
   Nb of faces within the viscous sub-layer     :      27030
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640850E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70678E+01 0.33911E+01
   Friction velocity        uet   :  0.17843E-01 0.26930E+01
   Friction velocity        uk    :  0.17842E-01 0.26105E+01
   Dimensionless distance   yplus :  0.50023E-04 0.85112E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3348
   Nb of faces within the viscous sub-layer     :      27042
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67836E+00     107   0.16793E+00   0.73558E+01 0.15983E+03 
c  Velocity[X]                                      0.22322E+01 
c  Velocity[Y]                                      0.23461E+01 
c  Velocity[Z]                                      0.27776E+01 
c  Pressure     0.22873E-01     571   0.29585E-02   0.20609E+00 0.17333E+03 
c  k            0.24632E-01      54   0.28326E-02   0.25820E-02 0.48766E+03 
c  epsilon      0.50798E+03      40   0.42335E-02   0.16463E+07 0.29290E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.4314e-05                             4
a  epsilon        -0.22012                             3


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

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.608978309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640847E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76253E+01 0.33832E+01
   Friction velocity        uet   :  0.15985E-01 0.26934E+01
   Friction velocity        uk    :  0.15961E-01 0.26108E+01
   Dimensionless distance   yplus :  0.50118E-04 0.85329E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3352
   Nb of faces within the viscous sub-layer     :      27039
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67909E+00     107   0.16649E+00   0.76668E+01 0.16347E+03 
c  Velocity[X]                                      0.24084E+01 
c  Velocity[Y]                                      0.23487E+01 
c  Velocity[Z]                                      0.29097E+01 
c  Pressure     0.23099E-01     509   0.34111E-02   0.20807E+00 0.39452E+03 
c  k            0.24669E-01      52   0.45650E-02   0.30982E-02 0.49891E+03 
c  epsilon      0.50852E+03      36   0.85493E-02   0.20592E+07 0.24520E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3317e-05                             4
a  epsilon        -0.13993                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2962          9.0438         0.57068        0.076645
v  Velocity[Y]            -7.6492          8.4503         0.24282         0.18602
v  Velocity[Z]            -13.503          12.683        -0.22678     -0.00041996
v  ǁVelocityǁ          1.9079e-05          16.007          1.6088          1.6182
v  Pressure                -41014           26815           15436           13613
v  k                   4.1101e-08          1.6482       0.0097356       0.0083778
v  epsilon             1.8007e-05      1.6268e+05          99.975           6.401
v  TurbVisc             7.922e-13         0.14181      0.00050943       0.0064415
v  total_pressure      4.5899e+05      5.2682e+05      5.1544e+05      5.1361e+05


 TIME FOR THE TIME STEP              178:        0.62575E+02

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


 INSTANT    0.179000000E+03   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        -0.174917272E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640852E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.64128E+01 0.33847E+01
   Friction velocity        uet   :  0.15451E-01 0.26788E+01
   Friction velocity        uk    :  0.15450E-01 0.26394E+01
   Dimensionless distance   yplus :  0.49891E-04 0.86268E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3352
   Nb of faces within the viscous sub-layer     :      27020
   Total nuInlet                     2          46        -0.699640825E+00
Smooth wall               5       41000         0.608978309E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640847E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76253E+01 0.33832E+01
   Friction velocity        uet   :  0.15985E-01 0.26934E+01
   Friction velocity        uk    :  0.15961E-01 0.26108E+01
   Dimensionless distance   yplus :  0.50118E-04 0.85329E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3352
   Nb of faces within the viscous sub-layer     :      27039
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67909E+00     107   0.16649E+00   0.76668E+01 0.16347E+03 
c  Velocity[X]                                      0.24084E+01 
c  Velocity[Y]                                      0.23487E+01 
c  Velocity[Z]                                      0.29097E+01 
c  Pressure     0.23099E-01     509   0.34111E-02   0.20807E+00 0.39452E+03 
c  k            0.24669E-01      52   0.45650E-02   0.30982E-02 0.49891E+03 
c  epsilon      0.50852E+03      36   0.85493E-02   0.20592E+07 0.24520E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.3317e-05                             4
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.286775341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74860E+01 0.33971E+01
   Friction velocity        uet   :  0.14883E-01 0.26924E+01
   Friction velocity        uk    :  0.14881E-01 0.26098E+01
   Dimensionless distance   yplus :  0.50257E-04 0.85212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3356
   Nb of faces within the viscous sub-layer     :      27001
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67960E+00     105   0.17271E+00   0.79316E+01 0.16632E+03 
c  Velocity[X]                                      0.24974E+01 
c  Velocity[Y]                                      0.23958E+01 
c  Velocity[Z]                                      0.30384E+01 
c  Pressure     0.23705E-01     643   0.31398E-02   0.21336E+00 0.62265E+03 
c  k            0.24681E-01      57   0.24706E-02   0.24119E-02 0.54004E+03 
c  epsilon      0.51117E+03      45   0.40244E-02   0.21962E+07 0.33694E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.2179e-05                             2
a  epsilon        -0.13668                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -4.57          9.3134         0.57136        0.076554
v  Velocity[Y]            -7.8031          8.4295         0.24342         0.18597
v  Velocity[Z]            -13.332           12.88        -0.22671     -0.00042773
v  ǁVelocityǁ          1.9361e-05          16.043          1.6091          1.6185
v  Pressure                -40914           26618           15452           13626
v  k                   1.5465e-08          1.6527       0.0097755       0.0083827
v  epsilon             1.7984e-05      1.6488e+05          100.79          6.4187
v  TurbVisc            7.9053e-13         0.14181      0.00050995       0.0064427
v  total_pressure      4.5909e+05      5.2662e+05      5.1545e+05      5.1363e+05


 TIME FOR THE TIME STEP              180:        0.65808E+02

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


 INSTANT    0.181000000E+03   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        -0.508548965E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640849E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.62361E+01 0.33711E+01
   Friction velocity        uet   :  0.11943E-01 0.26762E+01
   Friction velocity        uk    :  0.11867E-01 0.26315E+01
   Dimensionless distance   yplus :  0.50240E-04 0.86047E+01
   ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.286775341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74860E+01 0.33971E+01
   Friction velocity        uet   :  0.14883E-01 0.26924E+01
   Friction velocity        uk    :  0.14881E-01 0.26098E+01
   Dimensionless distance   yplus :  0.50257E-04 0.85212E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3356
   Nb of faces within the viscous sub-layer     :      27001
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67960E+00     105   0.17271E+00   0.79316E+01 0.16632E+03 
c  Velocity[X]                                      0.24974E+01 
c  Velocity[Y]                                      0.23958E+01 
c  Velocity[Z]                                      0.30384E+01 
c  Pressure     0.23705E-01     643   0.31398E-02   0.21336E+00 0.62265E+03 
c  k            0.24681E-01      57   0.24706E-02   0.24119E-02 0.54004E+03 
c  epsilon      0.51117E+03      45   0.40244E-02   0.21962E+07 0.33694E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.142773277E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74120E+01 0.33935E+01
   Friction velocity        uet   :  0.14349E-01 0.26927E+01
   Friction velocity        uk    :  0.14347E-01 0.26103E+01
   Dimensionless distance   yplus :  0.50076E-04 0.85156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3356
   Nb of faces within the viscous sub-layer     :      26986
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67899E+00     106   0.16706E+00   0.76476E+01 0.16168E+03 
c  Velocity[X]                                      0.24064E+01 
c  Velocity[Y]                                      0.23305E+01 
c  Velocity[Z]                                      0.29106E+01 
c  Pressure     0.22372E-01     731   0.27106E-02   0.20220E+00 0.24557E+03 
c  k            0.24637E-01      53   0.45896E-02   0.22560E-02 0.40550E+03 
c  epsilon      0.50911E+03      36   0.87283E-02   0.12184E+07 0.20346E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.7561e-06                             3
a  epsilon         -0.1025                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.2739          9.1942         0.57194        0.076536
v  Velocity[Y]            -7.9024          8.3754          0.2438         0.18599
v  Velocity[Z]            -13.625          13.213        -0.22682      -0.0004671
v  ǁVelocityǁ          1.9507e-05          16.182          1.6096          1.6187
v  Pressure                -40822           26750           15456           13629
v  k                   4.0375e-08          1.6463       0.0097736       0.0083862
v  epsilon             1.7962e-05      1.6436e+05          100.65          6.4227
v  TurbVisc            7.8912e-13         0.14181       0.0005103       0.0064432
v  total_pressure      4.5918e+05      5.2675e+05      5.1546e+05      5.1363e+05


 TIME FOR THE TIME STEP              182:        0.63673E+02

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


 INSTANT    0.183000000E+03   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         0.350650672E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640857E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65382E+01 0.33923E+01
   Friction velocity        uet   :  0.1475 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.699640825E+00
Smooth wall               5       41000        -0.142773277E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640797E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74120E+01 0.33935E+01
   Friction velocity        uet   :  0.14349E-01 0.26927E+01
   Friction velocity        uk    :  0.14347E-01 0.26103E+01
   Dimensionless distance   yplus :  0.50076E-04 0.85156E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3356
   Nb of faces within the viscous sub-layer     :      26986
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67899E+00     106   0.16706E+00   0.76476E+01 0.16168E+03 
c  Velocity[X]                                      0.24064E+01 
c  Velocity[Y]                                      0.23305E+01 
c  Velocity[Z]                                      0.29106E+01 
c  Pressure     0.22372E-01     731   0.27106E-02   0.20220E+00 0.24557E+03 
c  k            0.24637E-01      53   0.45896E-02   0.22560E-02 0.40550E+03 
c  epsilon      0.50911E+03      36   0.87283E-02   0.12184E+07 0.20346E+04 
----------------------------------- TIME FOR THE TIME STEP              183:        0.62855E+02

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


 INSTANT    0.184000000E+03   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         0.143801397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74390E+01 0.33782E+01
   Friction velocity        uet   :  0.94726E-02 0.26972E+01
   Friction velocity        uk    :  0.94459E-02 0.26149E+01
   Dimensionless distance   yplus :  0.50286E-04 0.84963E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3359
   Nb of faces within the viscous sub-layer     :      26989
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67880E+00     105   0.16531E+00   0.74640E+01 0.16136E+03 
c  Velocity[X]                                      0.24007E+01 
c  Velocity[Y]                                      0.22973E+01 
c  Velocity[Z]                                      0.27660E+01 
c  Pressure     0.22571E-01     623   0.25154E-02   0.20364E+00 0.63479E+03 
c  k            0.24694E-01      55   0.29046E-02   0.23756E-02 0.46577E+03 
c  epsilon      0.51165E+03      41   0.38990E-02   0.14271E+07 0.27887E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.8402e-06                             4
a  epsilon        -0.14841                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8607          9.2127         0.57259          0.0765
v  Velocity[Y]            -7.6949          8.3747         0.24442         0.18594
v  Velocity[Z]            -13.686          12.657        -0.22688     -0.00047457
v  ǁVelocityǁ          1.9346e-05          16.266          1.6104           1.619
v  Pressure                -40852           26772           15475           13645
v  k                   3.9919e-08          1.6488       0.0097764       0.0083876
v  epsilon             1.7956e-05      1.6135e+05          100.63          6.4296
v  TurbVisc            7.8897e-13         0.14181      0.00051061       0.0064435
v  total_pressure      4.5915e+05      5.2677e+05      5.1548e+05      5.1365e+05


 TIME FOR THE TIME STEP              184:        0.64630E+02

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


 INSTANT    0.185000000E+03   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         0.837051736E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640856E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                    TIME FOR THE TIME STEP              183:        0.63839E+02

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


 INSTANT    0.184000000E+03   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         0.143801397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640798E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74390E+01 0.33782E+01
   Friction velocity        uet   :  0.94726E-02 0.26972E+01
   Friction velocity        uk    :  0.94459E-02 0.26149E+01
   Dimensionless distance   yplus :  0.50286E-04 0.84963E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3359
   Nb of faces within the viscous sub-layer     :      26989
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67880E+00     105   0.16531E+00   0.74640E+01 0.16136E+03 
c  Velocity[X]                                      0.24007E+01 
c  Velocity[Y]                                      0.22973E+01 
c  Velocity[Z]                                      0.27660E+01 
c  Pressure     0.22571E-01     623   0.25154E-02   0.20364E+00 0.63479E+03 
c  k            0.24694v  TurbVisc            7.8886e-13         0.14181      0.00051067       0.0064434
v  total_pressure      4.5909e+05       5.267e+05       5.155e+05      5.1366e+05


 TIME FOR THE TIME STEP              185:        0.64454E+02

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


 INSTANT    0.186000000E+03   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        -0.130994494E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640848E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72963E+01 0.33886E+01
   Friction velocity        uet   :  0.14974E-01 0.26935E+01
   Friction velocity        uk    :  0.14973E-01 0.26111E+01
   Dimensionless distance   yplus :  0.50408E-04 0.85101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3365
   Nb of faces within the viscous sub-layer     :      26962
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67899E+00     105   0.16787E+00   0.74289E+01 0.16157E+03 
c  Velocity[X]                                      0.23497E+01 
c  Velocity[Y]                                      0.22935E+01 
c  Velocity[Z]                                      0.27857E+01 
c  Pressure     0.21522E-01     717   0.25260E-02   0.19518E+00 0.52061E+03 
c  k            0.24797E-01      53   0.47154E-02   0.38042E-02 0.55753E+03 
c  epsilon      0.51314E+03      38   0.88828E-02   0.21811E+07 0.24150E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5343e-06                             4
a  epsilon       -0.087434                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5802          9.1754         0.57319        0.076598
v  Velocity[Y]            -7.4815          8.4102         0.24499           0.186
v  Velocity[Z]            -13.455          13.231        -0.22694     -0.00042133
v  ǁVelocityǁ          1.9302e-05          15.943          1.6115          1.6192
v  Pressure                -40994           26702           15482           13652
v  k                   3.9418e-08          1.6615       0.0098102       0.0083925
v  epsilon             1.7973e-05      1.6314e+05          101.29          6.4478
v  TurbVisc            7.8901e-13         0.14181      0.00051081       0.0064434
v  total_pressure      4.5901e+05       5.267e+05      5.1548e+05      5.1365e+05


 TIME FOR THE TIME STEP              186:        0.67553E+02

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


 INSTANT    0.187000000E+03   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         0.604876399E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640858E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY Cv  TurbVisc            7.8886e-13         0.14181      0.00051067       0.0064434
v  total_pressure      4.5909e+05       5.267e+05       5.155e+05      5.1366e+05


 TIME FOR THE TIME STEP              185:        0.66638E+02

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


 INSTANT    0.186000000E+03   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        -0.130994494E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640848E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72963E+01 0.33886E+01
   Friction velocity        uet   :  0.14974E-01 0.26935E+01
   Friction velocity        uk    :  0.14973E-01 0.26111E+01
   Dimensionless distance   yplus :  0.50408E-04 0.85101E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3365
   Nb of faces within the viscous sub-layer     :      26962
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67899E+00     105   0.16787E+00   0.74289E+01 0.16157E+03 
c  Velocity[X]                                      0.23497E+01 
c  Velocity[Y]                                      0.22935E+01 
cv  k                   3.9158e-08          1.6426       0.0098169       0.0083935
v  epsilon             1.7992e-05      1.6098e+05          101.38          6.4489
v  TurbVisc            7.8864e-13         0.14181      0.00051115       0.0064434
v  total_pressure      4.5892e+05      5.2679e+05      5.1551e+05      5.1367e+05


 TIME FOR THE TIME STEP              187:        0.75407E+02

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


 INSTANT    0.188000000E+03   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        -0.122546601E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76799E+01 0.33902E+01
   Friction velocity        uet   :  0.15895E-01 0.26940E+01
   Friction velocity        uk    :  0.15894E-01 0.26116E+01
   Dimensionless distance   yplus :  0.50146E-04 0.85909E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3367
   Nb of faces within the viscous sub-layer     :      26965
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67893E+00     105   0.16776E+00   0.75380E+01 0.16192E+03 
c  Velocity[X]                                      0.23469E+01 
c  Velocity[Y]                                      0.22908E+01 
c  Velocity[Z]                                      0.29002E+01 
c  Pressure     0.21364E-01     557   0.25471E-02   0.19313E+00 0.95061E+03 
c  k            0.24795E-01      52   0.25555E-02   0.24834E-02 0.55586E+03 
c  epsilon      0.51607E+03      37   0.32043E-02   0.25945E+07 0.43409E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6324e-06                             4
a  epsilon        -0.11344                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8196           9.224         0.57363        0.076532
v  Velocity[Y]            -7.8123          8.3394         0.24525         0.18599
v  Velocity[Z]            -13.709          12.481        -0.22719     -0.00047622
v  ǁVelocityǁ          1.9366e-05          16.261          1.6125          1.6195
v  Pressure                -41157           26780           15496           13661
v  k                   3.8896e-08          1.6496       0.0098121       0.0083919
v  epsilon             1.8016e-05      1.6424e+05          101.18          6.4496
v  TurbVisc              7.88e-13         0.14181       0.0005112       0.0064433
v  total_pressure      4.5884e+05      5.2678e+05       5.155e+05      5.1366e+05


 TIME FOR THE TIME STEP              188:        0.61516E+02

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


 INSTANT    0.189000000E+03   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        -0.940736553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640853E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0       v  k                   3.9158e-08          1.6426       0.0098169       0.0083935
v  epsilon             1.7992e-05      1.6098e+05          101.38          6.4489
v  TurbVisc            7.8864e-13         0.14181      0.00051115       0.0064434
v  total_pressure      4.5892e+05      5.2679e+05      5.1551e+05      5.1367e+05


 TIME FOR THE TIME STEP              187:        0.70608E+02

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


 INSTANT    0.188000000E+03   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        -0.122546601E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640860E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76799E+01 0.33902E+01
   Friction velocity        uet   :  0.15895E-01 0.26940E+01
   Friction velocity        uk    :  0.15894E-01 0.26116E+01
   Dimensionless distance   yplus :  0.50146E-04 0.85909E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3367
   Nb of faces within the viscous sub-layer     :      26965
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67893E+00     105   0.16v  ǁVelocityǁ          1.9188e-05          17.587          1.6131          1.6196
v  Pressure                -41173           26770           15534           13694
v  k                   3.8633e-08          1.6448       0.0098038       0.0083918
v  epsilon             1.8038e-05      1.6161e+05          101.05          6.4466
v  TurbVisc            7.8815e-13         0.14181      0.00051121        0.006443
v  total_pressure      4.5883e+05      5.2677e+05      5.1553e+05      5.1369e+05


 TIME FOR THE TIME STEP              189:        0.66927E+02

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


 INSTANT    0.190000000E+03   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         0.327055629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640805E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76827E+01 0.33773E+01
   Friction velocity        uet   :  0.16295E-01 0.26956E+01
   Friction velocity        uk    :  0.16294E-01 0.26130E+01
   Dimensionless distance   yplus :  0.50019E-04 0.86238E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3375
   Nb of faces within the viscous sub-layer     :      26950
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67858E+00     103   0.16423E+00   0.75752E+01 0.16034E+03 
c  Velocity[X]                                      0.23629E+01 
c  Velocity[Y]                                      0.23305E+01 
c  Velocity[Z]                                      0.28818E+01 
c  Pressure     0.20887E-01     621   0.22559E-02   0.18951E+00 0.58819E+03 
c  k            0.24779E-01      54   0.22447E-02   0.13123E-02 0.31120E+03 
c  epsilon      0.51836E+03      40   0.29270E-02   0.48469E+06 0.13771E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.7981e-06                             5
a  epsilon       -0.052106                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.4313          9.1969         0.57382        0.076613
v  Velocity[Y]             -7.715          8.3782          0.2458           0.186
v  Velocity[Z]            -13.763          13.573        -0.22749     -0.00047884
v  ǁVelocityǁ          1.9071e-05          16.313          1.6135          1.6195
v  Pressure                -41416           26788           15527           13690
v  k                   3.8373e-08          1.6585        0.009821       0.0083915
v  epsilon              1.805e-05      1.6201e+05          101.42          6.4549
v  TurbVisc            7.8749e-13         0.14181       0.0005113       0.0064428
v  total_pressure      4.5858e+05      5.2679e+05      5.1553e+05      5.1369e+05


 TIME FOR THE TIME STEP              190:        0.65813E+02

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


 INSTANT    0.191000000E+03   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         0.117859888E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640851E+00
Free inlv  ǁVelocityǁ          1.9188e-05          17.587          1.6131          1.6196
v  Pressure                -41173           26770           15534           13694
v  k                   3.8633e-08          1.6448       0.0098038       0.0083918
v  epsilon             1.8038e-05      1.6161e+05          101.05          6.4466
v  TurbVisc            7.8815e-13         0.14181      0.00051121        0.006443
v  total_pressure      4.5883e+05      5.2677e+05      5.1553e+05      5.1369e+05


 TIME FOR THE TIME STEP              189:        0.71199E+02

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


 INSTANT    0.190000000E+03   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         0.327055629E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640805E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76827E+01 0.33773E+01
   Friction velocity        uet   :  0.16295E-01 0.26956E+01
   Friction velocity        uk    :  0.16294E-01 0.26130E+01
   Dimensionless distance   yplus :  0.50019E-04 0.86238E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3375
   Nb of faces within the viscous sub-layer     :      26950
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_itev  Velocity[Y]            -7.7591          8.3554         0.24601         0.18604
v  Velocity[Z]            -14.563          13.165        -0.22767     -0.00046039
v  ǁVelocityǁ          1.9222e-05           17.17           1.614          1.6197
v  Pressure                -41460           26837           15541           13702
v  k                   3.8119e-08          1.6408       0.0098137       0.0083907
v  epsilon             1.8066e-05      1.6189e+05          101.19          6.4544
v  TurbVisc            7.8696e-13         0.14181      0.00051144       0.0064427
v  total_pressure      4.5854e+05      5.2684e+05      5.1554e+05       5.137e+05


 TIME FOR THE TIME STEP              191:        0.64539E+02

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


 INSTANT    0.192000000E+03   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        -0.618975252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640841E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76252E+01 0.33949E+01
   Friction velocity        uet   :  0.16101E-01 0.26923E+01
   Friction velocity        uk    :  0.16100E-01 0.26098E+01
   Dimensionless distance   yplus :  0.50084E-04 0.86494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3366
   Nb of faces within the viscous sub-layer     :      26957
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67892E+00     106   0.16613E+00   0.76567E+01 0.16299E+03 
c  Velocity[X]                                      0.23266E+01 
c  Velocity[Y]                                      0.24247E+01 
c  Velocity[Z]                                      0.29054E+01 
c  Pressure     0.20267E-01     495   0.22141E-02   0.18411E+00 0.21015E+03 
c  k            0.24794E-01      54   0.28025E-02   0.29732E-02 0.59560E+03 
c  epsilon      0.51780E+03      37   0.43614E-02   0.31503E+07 0.43528E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -4.737e-06                             4
a  epsilon       -0.066912                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5414          9.1058         0.57395        0.076648
v  Velocity[Y]            -7.6303           8.374         0.24627         0.18598
v  Velocity[Z]            -13.608          12.199        -0.22784     -0.00044967
v  ǁVelocityǁ          1.9125e-05          16.154          1.6144          1.6197
v  Pressure                -41634           26838           15539           13699
v  k                   3.7873e-08          1.6558       0.0098274       0.0083907
v  epsilon             1.8085e-05      1.6465e+05          101.83          6.4591
v  TurbVisc            7.8681e-13         0.14181      0.00051135       0.0064425
v  total_pressure      4.5837e+05      5.2684e+05      5.1554e+05       5.137e+05


 TIME FOR THE TIME STEP              192:        0.63545E+02

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


 INSTANT    0.193000000E+03   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        -0.119201376E-17
Rough wall                6         v  Velocity[Y]            -7.7591          8.3554         0.24601         0.18604
v  Velocity[Z]            -14.563          13.165        -0.22767     -0.00046039
v  ǁVelocityǁ          1.9222e-05           17.17           1.614          1.6197
v  Pressure                -41460           26837           15541           13702
v  k                   3.8119e-08          1.6408       0.0098137       0.0083907
v  epsilon             1.8066e-05      1.6189e+05          101.19          6.4544
v  TurbVisc            7.8696e-13         0.14181      0.00051144       0.0064427
v  total_pressure      4.5854e+05      5.2684e+05      5.1554e+05       5.137e+05


 TIME FOR THE TIME STEP              191:        0.68967E+02

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


 INSTANT    0.192000000E+03   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        -0.618975252E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640841E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76252E+01 0.33949E+01
   Friction velocity        uet   :  0.16101E-01 0.26923E+01
   Friction velocity        uk    :  0.16100E-01 0.26098E+01
   Dimensionless distance   yplus :  0.50084E-04 0.86494E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3366
   Nb of faces within the viscous sub-layer     :      26957
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMAT-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9942          9.3824         0.57414        0.076669
v  Velocity[Y]            -7.5614          8.3574         0.24657         0.18602
v  Velocity[Z]            -14.512          12.361        -0.22802     -0.00051313
v  ǁVelocityǁ          1.9126e-05          17.206          1.6151          1.6199
v  Pressure                -41575           26863           15568           13720
v  k                   3.7637e-08          1.6487       0.0098253       0.0083915
v  epsilon             1.8108e-05      1.6027e+05          101.43          6.4587
v  TurbVisc            7.8614e-13         0.14181      0.00051147       0.0064424
v  total_pressure      4.5842e+05      5.2686e+05      5.1557e+05      5.1372e+05


 TIME FOR THE TIME STEP              193:        0.75714E+02

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


 INSTANT    0.194000000E+03   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        -0.164302604E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75741E+01 0.33834E+01
   Friction velocity        uet   :  0.16711E-01 0.26923E+01
   Friction velocity        uk    :  0.16710E-01 0.26100E+01
   Dimensionless distance   yplus :  0.49919E-04 0.87070E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3372
   Nb of faces within the viscous sub-layer     :      26955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67923E+00     103   0.16922E+00   0.74675E+01 0.16018E+03 
c  Velocity[X]                                      0.23496E+01 
c  Velocity[Y]                                      0.22883E+01 
c  Velocity[Z]                                      0.28296E+01 
c  Pressure     0.19856E-01     755   0.23267E-02   0.18115E+00 0.93067E+03 
c  k            0.24781E-01      53   0.29886E-02   0.21247E-02 0.43895E+03 
c  epsilon      0.51750E+03      37   0.44473E-02   0.14023E+07 0.27932E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.9293e-06                             5
a  epsilon         -0.1021                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.6363          9.1544          0.5744        0.076682
v  Velocity[Y]             -7.882           8.423         0.24682         0.18595
v  Velocity[Z]            -13.615          13.372        -0.22803     -0.00051106
v  ǁVelocityǁ          1.9389e-05          16.121          1.6157            1.62
v  Pressure                -41772           26843           15555           13712
v  k                   3.7414e-08          1.6547       0.0098315       0.0083909
v  epsilon             1.8132e-05      1.6295e+05          101.63          6.4605
v  TurbVisc            7.8573e-13         0.14181      0.00051167       0.0064423
v  total_pressure      4.5823e+05      5.2684e+05      5.1556e+05      5.1371e+05


 TIME FOR THE TIME STEP              194:        0.67151E+02

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


 INSTANT    0.195000000E+03   TIME STEP NUMBER             195
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9942          9.3824         0.57414        0.076669
v  Velocity[Y]            -7.5614          8.3574         0.24657         0.18602
v  Velocity[Z]            -14.512          12.361        -0.22802     -0.00051313
v  ǁVelocityǁ          1.9126e-05          17.206          1.6151          1.6199
v  Pressure                -41575           26863           15568           13720
v  k                   3.7637e-08          1.6487       0.0098253       0.0083915
v  epsilon             1.8108e-05      1.6027e+05          101.43          6.4587
v  TurbVisc            7.8614e-13         0.14181      0.00051147       0.0064424
v  total_pressure      4.5842e+05      5.2686e+05      5.1557e+05      5.1372e+05


 TIME FOR THE TIME STEP              193:        0.65421E+02

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


 INSTANT    0.194000000E+03   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        -0.164302604E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640799E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75741E+01 0.33834E+01
   Friction velocity        uet   :  0.16711E-01 0.26923E+01
   Friction velocity        uk    :  0.16710E-01 0.26100E+01
   Dimensionless distance   yplus :  0.49919E-04 0.87070E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3372
   Nb of faces within the viscous sub-layer     :      2
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.337          9.2681         0.57465        0.076685
v  Velocity[Y]              -7.75          8.4912         0.24713         0.18598
v  Velocity[Z]            -14.351          15.463        -0.22815     -0.00045381
v  ǁVelocityǁ           1.935e-05          17.011          1.6163          1.6201
v  Pressure                -41746           26820           15576           13728
v  k                   3.7204e-08          1.6415       0.0098256         0.00839
v  epsilon             1.8157e-05      1.6259e+05          101.46          6.4552
v  TurbVisc            7.8596e-13         0.14181      0.00051175       0.0064421
v  total_pressure      4.5825e+05      5.2682e+05      5.1558e+05      5.1373e+05


 TIME FOR THE TIME STEP              195:        0.72574E+02

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


 INSTANT    0.196000000E+03   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        -0.220782834E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74498E+01 0.33711E+01
   Friction velocity        uet   :  0.14524E-01 0.26884E+01
   Friction velocity        uk    :  0.14508E-01 0.26114E+01
   Dimensionless distance   yplus :  0.50214E-04 0.86785E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3377
   Nb of faces within the viscous sub-layer     :      26944
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67932E+00     104   0.16824E+00   0.78420E+01 0.16594E+03 
c  Velocity[X]                                      0.24207E+01 
c  Velocity[Y]                                      0.23245E+01 
c  Velocity[Z]                                      0.30967E+01 
c  Pressure     0.19354E-01     620   0.25064E-02   0.17627E+00 0.74612E+03 
c  k            0.24784E-01      53   0.23402E-02   0.22813E-02 0.55269E+03 
c  epsilon      0.51903E+03      36   0.33479E-02   0.27363E+07 0.42824E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -1.551e-06                             3
a  epsilon        -0.10575                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5923          9.0636         0.57483        0.076635
v  Velocity[Y]            -7.6508            8.37          0.2474           0.186
v  Velocity[Z]            -13.495          12.333        -0.22835     -0.00043667
v  ǁVelocityǁ          1.9189e-05          15.967          1.6169            1.62
v  Pressure                -41968           26864           15551           13709
v  k                    3.701e-08           1.651       0.0098485       0.0083907
v  epsilon             1.8184e-05      1.6078e+05          102.14          6.4684
v  TurbVisc            7.8581e-13         0.14181      0.00051174       0.0064418
v  total_pressure      4.5803e+05      5.2686e+05      5.1555e+05      5.1371e+05


 TIME FOR THE TIME STEP              196:        0.69114E+02

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


 INSTANT    0.197000000E+03   TIME STEP NUMBER             197
 ============================================================= 




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

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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.337          9.2681         0.57465        0.076685
v  Velocity[Y]              -7.75          8.4912         0.24713         0.18598
v  Velocity[Z]            -14.351          15.463        -0.22815     -0.00045381
v  ǁVelocityǁ           1.935e-05          17.011          1.6163          1.6201
v  Pressure                -41746           26820           15576           13728
v  k                   3.7204e-08          1.6415       0.0098256         0.00839
v  epsilon             1.8157e-05      1.6259e+05          101.46          6.4552
v  TurbVisc            7.8596e-13         0.14181      0.00051175       0.0064421
v  total_pressure      4.5825e+05      5.2682e+05      5.1558e+05      5.1373e+05


 TIME FOR THE TIME STEP              195:        0.67496E+02

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


 INSTANT    0.196000000E+03   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        -0.220782834E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640863E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74498E+01 0.33711E+01
   Friction velocity        uet   :  0.14524E-01 0.26884E+01
   Friction velocity        uk    :  0.14508E-01 0.26114E+01
   Dimensionless distance   yplus :  0.50214E-04 0-  -------  --------------  --------------  ------------  ------------
a  k           -1.6116e-06                             3
a  epsilon        -0.17181                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3573           9.482         0.57503        0.076615
v  Velocity[Y]            -7.7414          8.4958         0.24766           0.186
v  Velocity[Z]            -14.294          12.113        -0.22863     -0.00047757
v  ǁVelocityǁ          1.9359e-05          17.235          1.6174          1.6201
v  Pressure                -42033           26837           15564           13717
v  k                   3.6829e-08          1.6383       0.0098472       0.0083904
v  epsilon             1.8211e-05      1.6226e+05          101.81          6.4661
v  TurbVisc            7.8578e-13         0.14181      0.00051187       0.0064417
v  total_pressure      4.5797e+05      5.2684e+05      5.1556e+05      5.1372e+05


 TIME FOR THE TIME STEP              197:        0.59626E+02

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


 INSTANT    0.198000000E+03   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        -0.155719777E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640848E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71828E+01 0.33848E+01
   Friction velocity        uet   :  0.13061E-01 0.26912E+01
   Friction velocity        uk    :  0.15917E-01 0.26089E+01
   Dimensionless distance   yplus :  0.50238E-04 0.87136E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3370
   Nb of faces within the viscous sub-layer     :      26930
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67948E+00     106   0.16521E+00   0.74782E+01 0.15981E+03 
c  Velocity[X]                                      0.23102E+01 
c  Velocity[Y]                                      0.23431E+01 
c  Velocity[Z]                                      0.28249E+01 
c  Pressure     0.19386E-01     569   0.27304E-02   0.17614E+00 0.49696E+03 
c  k            0.24720E-01      58   0.29293E-02   0.20100E-02 0.38745E+03 
c  epsilon      0.51631E+03      46   0.40358E-02   0.80954E+06 0.17136E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6715e-06                             2
a  epsilon        -0.13261                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4.768          9.2183         0.57523        0.076666
v  Velocity[Y]            -7.6688          8.3985         0.24782         0.18599
v  Velocity[Z]            -13.675          13.206        -0.22889     -0.00046648
v  ǁVelocityǁ          1.9169e-05           16.23          1.6181          1.6202
v  Pressure                -42093           26855           15572           13722
v  k                   3.6664e-08          1.6585       0.0098549       0.0083895
v  epsilon             1.8238e-05      1.6333e+05          101.95          6.4628
v  TurbVisc            7.8599e-13         0.14181      0.00051194       0.0064417
v  total_pressure      4.5791e+05      5.2685e+05      5.1557e+05      5.1372e+05


 TIME FOR THE TIME STEP              198:        0.60947E+02

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


 INSTANT    0.199000000E+03   TIME STEP NUMBER             199
 -  -------  --------------  --------------  ------------  ------------
a  k           -1.6116e-06                             3
a  epsilon        -0.17181                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.3573           9.482         0.57503        0.076615
v  Velocity[Y]            -7.7414          8.4958         0.24766           0.186
v  Velocity[Z]            -14.294          12.113        -0.22863     -0.00047757
v  ǁVelocityǁ          1.9359e-05          17.235          1.6174          1.6201
v  Pressure                -42033           26837           15564           13717
v  k                   3.6829e-08          1.6383       0.0098472       0.0083904
v  epsilon             1.8211e-05      1.6226e+05          101.81          6.4661
v  TurbVisc            7.8578e-13         0.14181      0.00051187       0.0064417
v  total_pressure      4.5797e+05      5.2684e+05      5.1556e+05      5.1372e+05


 TIME FOR THE TIME STEP              197:        0.66510E+02

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


 INSTANT    0.198000000E+03   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        -0.155719777E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640848E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71828E+01 0.33848E+01
   Friction velocity        u
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9546e-06                             1
a  epsilon        -0.15649                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3375           9.325         0.57533        0.076582
v  Velocity[Y]            -7.5449          8.4838         0.24797         0.18603
v  Velocity[Z]            -14.602           15.56        -0.22922     -0.00052199
v  ǁVelocityǁ          1.9125e-05          17.059          1.6186          1.6203
v  Pressure                -42033           26934           15585           13731
v  k                   2.5695e-08           1.648       0.0098581       0.0083901
v  epsilon             1.8265e-05      1.5955e+05          101.86          6.4706
v  TurbVisc            7.8615e-13         0.14181      0.00051173       0.0064415
v  total_pressure      4.5797e+05      5.2693e+05      5.1559e+05      5.1373e+05


 TIME FOR THE TIME STEP              199:        0.72950E+02

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


 INSTANT    0.200000000E+03   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        -0.461214664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640870E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76599E+01 0.33884E+01
   Friction velocity        uet   :  0.17034E-01 0.26931E+01
   Friction velocity        uk    :  0.17033E-01 0.26106E+01
   Dimensionless distance   yplus :  0.49909E-04 0.87160E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3377
   Nb of faces within the viscous sub-layer     :      26931
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        200, Physical time    0.20000E+03


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

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

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

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.66166E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67980E+00     105   0.16968E+00   0.74286E+01 0.16076E+03 
c  Velocity[X]                                      0.22948E+01 
c  Velocity[Y]                                      0.23353E+01 
c  Velocity[Z]                                      0.27985E+01 
c  Pressure     0.19637E-01     748   0.22668E-02   0.17823E+00 0.88911E+03 
c  k            0.24731E-01      54   0.51858E-02   0.31677E-02 0.46556E+03 
c  epsilon      0.51686E+03      38   0.10707E-01   0.16861E+07 0.20528E+04 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0942e-06                             2
a  epsilon        -0.10759                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Veloci
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9546e-06                             1
a  epsilon        -0.15649                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3375           9.325         0.57533        0.076582
v  Velocity[Y]            -7.5449          8.4838         0.24797         0.18603
v  Velocity[Z]            -14.602           15.56        -0.22922     -0.00052199
v  ǁVelocityǁ          1.9125e-05          17.059          1.6186          1.6203
v  Pressure                -42033           26934           15585           13731
v  k                   2.5695e-08           1.648       0.0098581       0.0083901
v  epsilon             1.8265e-05      1.5955e+05          101.86          6.4706
v  TurbVisc            7.8615e-13         0.14181      0.00051173       0.0064415
v  total_pressure      4.5797e+05      5.2693e+05      5.1559e+05      5.1373e+05


 TIME FOR THE TIME STEP              199:        0.73265E+02

===============================================================


 INSTANT    0.200000000E+03   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        -0.461214664E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.699640870E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Mi------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70879E+00     131   0.15979E+00   0.87668E+03 0.86386E+03 
c  Velocity[X]                                      0.10374E+03 
c  Velocity[Y]                                      0.19491E+03 
c  Velocity[Z]                                      0.57803E+03 
c  Pressure     0.24796E-01    1450   0.20589E+00   0.22494E+00 0.28446E+06 
c  k            0.30520E-01      97   0.62310E-02   0.26661E-01 0.71676E+03 
c  epsilon      0.52101E+03      58   0.86977E-02   0.38205E+07 0.48856E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.35263                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9979          19.733         0.64409         0.10998
v  Velocity[Y]            -15.978          16.039         0.35053         0.26681
v  Velocity[Z]            -36.711          17.784        -0.23626      -0.0010717
v  ǁVelocityǁ           1.918e-05          42.744          1.7852          2.1984
v  Pressure                -21632           78332           46697           42087
v  k                    3.629e-08          1.6398       0.0099752        0.009368
v  epsilon             1.8409e-05      1.5958e+05          102.51          6.6292
v  TurbVisc            7.8681e-13         0.14181      0.00051172       0.0064411
v  total_pressure      4.7837e+05      5.7833e+05       5.467e+05      5.4209e+05


 TIME FOR THE TIME STEP              201:        0.98374E+02

===============================================================


 INSTANT    0.202000000E+03   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         0.627320576E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441577E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48940E+02 0.34454E+01
   Friction velocity        uet   :  0.21827E-01 0.32086E+01
   Friction velocity        uk    :  0.21594E-01 0.27157E+01
   Dimensionless distance   yplus :  0.50002E-04 0.13960E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4356
   Nb of faces within the viscous sub-layer     :      24296
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12577E+01     148   0.15735E+00   0.32007E+03 0.77774E+03 
c  Velocity[X]                                      0.66960E+02 
c  Velocity[Y]                                      0.10022E+03 
c  Velocity[Z]                                      0.15288E+03 
c  Pressure     0.90265E-01    1365   0.11297E+00   0.63996E+00 0.23215E+06 
c  k            0.39076E-01      93   0.23600E-01   0.32571E+00 0.34039E+04 
c  epsilon      0.12282E+04      57   0.62567E-01   0.24350E+09 0.16809E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3389e-06                             1
a  epsilon        -0.15067                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.70879E+00     131   0.15979E+00   0.87668E+03 0.86386E+03 
c  Velocity[X]                                      0.10374E+03 
c  Velocity[Y]                                      0.19491E+03 
c  Velocity[Z]                                      0.57803E+03 
c  Pressure     0.24796E-01    1450   0.20589E+00   0.22494E+00 0.28446E+06 
c  k            0.30520E-01      97   0.62310E-02   0.26661E-01 0.71676E+03 
c  epsilon      0.52101E+03      58   0.86977E-02   0.38205E+07 0.48856E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.35263                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9979          19.733         0.64409         0.10998
v  Velocity[Y]            -15.978          16.039         0.35053         0.26681
v  Velocity[Z]            -36.711          17.784        -0.23626      -0.0010717
v  ǁVelocityǁ           1.918e-05          42.744          1.7852          2.1984
v  Pressure                -21632           78332           46697           42087
v  k                    3.629e-08          1.6398       0.0099752        0.009368
v  epsilon             1.8409e-05      1.5958e+05          102.51          6.6292
v  TurbVisc            7.8681e-13         0.14181      0.00051172       0.0064411
v  total_pressure      4.7837e+05      5.7833e+05       5.467e+05      5.4209e+05


 TIME FOR THE TIME STEP              201:        0.94693E+02

===============================================================


 INSTANT    0.202000000E+03   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Ma   Nb of faces within the viscous sub-layer     :      24746
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11725E+01     140   0.15634E+00   0.16387E+03 0.60518E+03 
c  Velocity[X]                                      0.39760E+02 
c  Velocity[Y]                                      0.64703E+02 
c  Velocity[Z]                                      0.59405E+02 
c  Pressure     0.77315E-01    1311   0.32286E-01   0.55705E+00 0.43019E+05 
c  k            0.38367E-01      85   0.30881E-01   0.13213E+00 0.24163E+04 
c  epsilon      0.95344E+03      50   0.94085E-01   0.24382E+09 0.31807E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021615                            27
a  epsilon          -43.95                            24


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5881          13.311         0.68291         0.11037
v  Velocity[Y]            -12.431          16.763         0.35443         0.26349
v  Velocity[Z]            -28.436          20.367        -0.25741     -0.00038299
v  ǁVelocityǁ          2.0296e-05          31.115          1.8776          2.1919
v  Pressure                -48535           47902           30874           26327
v  k                   2.8977e-08          1.9399        0.011656         0.01136
v  epsilon               1.87e-05      2.7762e+05          128.46          8.7251
v  TurbVisc            7.8795e-13         0.16829      0.00057282       0.0077707
v  total_pressure      4.5147e+05       5.479e+05      5.3087e+05      5.2633e+05


 TIME FOR THE TIME STEP              203:        0.94561E+02

===============================================================


 INSTANT    0.204000000E+03   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         0.198276597E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441498E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27872E+02 0.35551E+01
   Friction velocity        uet   :  0.72685E-02 0.29163E+01
   Friction velocity        uk    :  0.72683E-02 0.28248E+01
   Dimensionless distance   yplus :  0.51405E-04 0.11578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4374
   Nb of faces within the viscous sub-layer     :      24766
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11893E+01     134   0.15689E+00   0.12207E+03 0.55692E+03 
c  Velocity[X]                                      0.33865E+02 
c  Velocity[Y]                                      0.47085E+02 
c  Velocity[Z]                                      0.41119E+02 
c  Pressure     0.71970E-01    1135   0.25221E-01   0.51738E+00 0.14918E+05 
c  k            0.36964E-01      82   0.14237E-01   0.51044E-01 0.16397E+04 
c  epsilon      0.80601E+03      52   0.27106E-01   0.77232E+08 0.18766E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.8529e-05                            18
a    Nb of faces within the viscous sub-layer     :      24746
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11725E+01     140   0.15634E+00   0.16387E+03 0.60518E+03 
c  Velocity[X]                                      0.39760E+02 
c  Velocity[Y]                                      0.64703E+02 
c  Velocity[Z]                                      0.59405E+02 
c  Pressure     0.77315E-01    1311   0.32286E-01   0.55705E+00 0.43019E+05 
c  k            0.38367E-01      85   0.30881E-01   0.13213E+00 0.24163E+04 
c  epsilon      0.95344E+03      50   0.94085E-01   0.24382E+09 0.31807E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021615                            27
a  epsilon          -43.95                            24


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5881          13.311         0.68291         0.11037
v  Velocity[Y]            -12.431          16.763         0.35443         0.26349
v  Velocity[Z]            -28.436          20.367        -0.25741     -0.00038299
v  ǁVelocityǁ          2.0296e-05          31.115          1.8776          2.1919
v  Pressure                -48535           47902           30874           26327
v  k                   2.8977e-08          1.9399        0.011656         0.01136
v  epsilon               1.87e-05      2.7762e+05          128.46          8.7251
v  TurbVisc            7.8795e-13         0.16829      0.00057282       0.0077707
v  total_pressure      4.5147e+05       5.479e+05      5.3087e+05      5.2633e+05


 TIME FOR THE TIME STEP              203:        0.89377E+02

===============================================================


 INSTANT    0.204000000E+03   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.51874E-04 0.11457E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4406
   Nb of faces within the viscous sub-layer     :      24820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12126E+01     132   0.15421E+00   0.92938E+02 0.49008E+03 
c  Velocity[X]                                      0.25480E+02 
c  Velocity[Y]                                      0.33489E+02 
c  Velocity[Z]                                      0.33969E+02 
c  Pressure     0.72916E-01     826   0.22508E-01   0.50616E+00 0.56547E+04 
c  k            0.36979E-01      78   0.65117E-02   0.34627E-01 0.17483E+04 
c  epsilon      0.81965E+03      49   0.20841E-01   0.14896E+09 0.26453E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9535e-05                            16
a  epsilon         -1.6637                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8664          17.052         0.70909         0.11041
v  Velocity[Y]            -13.267           13.86         0.34644         0.26344
v  Velocity[Z]            -30.012          24.151        -0.26905     -0.00015858
v  ǁVelocityǁ          2.1146e-05          34.076           1.946          2.2111
v  Pressure                -51597           48745           30726           26485
v  k                   8.7006e-09          2.4708        0.012185        0.011718
v  epsilon              1.885e-05      3.1472e+05          142.77          8.8469
v  TurbVisc            2.2848e-14         0.16882       0.0005755       0.0082373
v  total_pressure       4.484e+05      5.4875e+05      5.3073e+05      5.2649e+05


 TIME FOR THE TIME STEP              205:        0.72301E+02

===============================================================


 INSTANT    0.206000000E+03   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         0.428387623E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441508E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30706E+02 0.38234E+01
   Friction velocity        uet   :  0.13906E-01 0.30984E+01
   Friction velocity        uk    :  0.13904E-01 0.30919E+01
   Dimensionless distance   yplus :  0.52367E-04 0.11950E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4442
   Nb of faces within the viscous sub-layer     :      24765
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12335E+01     131   0.16180E+00   0.79622E+02 0.44464E+03 
c  Velocity[X]                                      0.21500E+02 
c  Velocity[Y]                                      0.28263E+02 
c  Velocity[Z]                                      0.29859E+02 
c  Pressure     0.77300E-01     700   0.20020E-01   0.51349E+00 0.42584E+04 
c  k            0.37129E-01      75   0.52079E-02   0.48997E-01 0.22639E+04 
c  epsilon      0.83464E+03      52   0.15366E-01   0.15611E+09 0.24555E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initia   Dimensionless distance   yplus :  0.51874E-04 0.11457E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4406
   Nb of faces within the viscous sub-layer     :      24820
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12126E+01     132   0.15421E+00   0.92938E+02 0.49008E+03 
c  Velocity[X]                                      0.25480E+02 
c  Velocity[Y]                                      0.33489E+02 
c  Velocity[Z]                                      0.33969E+02 
c  Pressure     0.72916E-01     826   0.22508E-01   0.50616E+00 0.56547E+04 
c  k            0.36979E-01      78   0.65117E-02   0.34627E-01 0.17483E+04 
c  epsilon      0.81965E+03      49   0.20841E-01   0.14896E+09 0.26453E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.9535e-05                            16
a  epsilon         -1.6637                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.8664          17.052         0.70909         0.11041
v  Velocity[Y]            -13.267           13.86         0.34644         0.26344
v  Velocity[Z]            -30.012          24.151        -0.26905     -0.00015858
v  ǁVelocityǁ          2.1146e-05          34.076           1.946          2.2111
v  Pressure                -51597           48745           30726           26485
v  k                   8.7006e-09          2.4708        0.012185        0.011718
v  epsilon              1.885e-05      3.1472e+05          142.77          8.8469
v  TurbVisc            2.2848e-14         0.16882       0.0005755       0.0082373
v  total_pressure       4.484e+05      5.4875e+05      5.3073e+05      5.2649e+05


 TIME FOR THE TIME STEP              205:        0.69670E+02

=========================   Rel velocity at the wall uiptn : -0.22298E+02 0.39185E+01
   Friction velocity        uet   :  0.15860E-01 0.31827E+01
   Friction velocity        uk    :  0.15858E-01 0.31753E+01
   Dimensionless distance   yplus :  0.53124E-04 0.10976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4464
   Nb of faces within the viscous sub-layer     :      24694
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12509E+01     128   0.16893E+00   0.67895E+02 0.40907E+03 
c  Velocity[X]                                      0.18164E+02 
c  Velocity[Y]                                      0.24977E+02 
c  Velocity[Z]                                      0.24754E+02 
c  Pressure     0.75525E-01     765   0.17514E-01   0.49713E+00 0.22184E+04 
c  k            0.37443E-01      73   0.48647E-02   0.30687E-01 0.15688E+04 
c  epsilon      0.87400E+03      51   0.10617E-01   0.59883E+08 0.13627E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.583e-05                            14
a  epsilon       -0.063945                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5889          19.713          0.7328         0.10967
v  Velocity[Y]            -11.741          13.103         0.33863         0.26381
v  Velocity[Z]            -22.482          24.035        -0.27799      0.00013937
v  ǁVelocityǁ          2.1929e-05          28.614          2.0106          2.2273
v  Pressure                -53763           49173           30749           26645
v  k                   3.6727e-08           2.597        0.013005        0.011946
v  epsilon             1.8748e-05      3.3825e+05          165.85          9.2257
v  TurbVisc            8.1072e-13         0.16883      0.00058883       0.0084884
v  total_pressure      4.4624e+05      5.4917e+05      5.3075e+05      5.2665e+05


 TIME FOR THE TIME STEP              207:        0.65190E+02

===============================================================


 INSTANT    0.208000000E+03   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        -0.975474144E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441502E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18316E+02 0.39631E+01
   Friction velocity        uet   :  0.15742E-01 0.32415E+01
   Friction velocity        uk    :  0.15700E-01 0.32337E+01
   Dimensionless distance   yplus :  0.53270E-04 0.11149E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4544
   Nb of faces within the viscous sub-layer     :      24631
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12642E+01     126   0.16391E+00   0.58844E+02 0.38106E+03 
c  Velocity[X]                                      0.16005E+02 
c  Velocity[Y]                                      0.21819E+02 
c  Velocity[Z]                                      0.21019E+02 
c  Pressure     0.79150E-01    1005   0.14365E-01   0.51012E+00 0.25051E+04 
c  k            0.37765E-01      71   0.41861E-02   0.28177E-01 0.18130E+04 
c  epsilon      0.91894E+03      52   0.96280E-02   0.23296E+09 0.35610   Rel velocity at the wall uiptn : -0.22298E+02 0.39185E+01
   Friction velocity        uet   :  0.15860E-01 0.31827E+01
   Friction velocity        uk    :  0.15858E-01 0.31753E+01
   Dimensionless distance   yplus :  0.53124E-04 0.10976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4464
   Nb of faces within the viscous sub-layer     :      24694
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12509E+01     128   0.16893E+00   0.67895E+02 0.40907E+03 
c  Velocity[X]                                      0.18164E+02 
c  Velocity[Y]                                      0.24977E+02 
c  Velocity[Z]                                      0.24754E+02 
c  Pressure     0.75525E-01     765   0.17514E-01   0.49713E+00 0.22184E+04 
c  k            0.37443E-01      73   0.48647E-02   0.30687E-01 0.15688E+04 
c  epsilon      0.87400E+03      51   0.10617E-01   0.59883E+08 0.13627E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.583e-05                            14
a  epsilon       -0.063945                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.5889          19.713          0.7328         0.10967
v  Velocity[Y]            -11.741          13.103         0.33863         0.26381
v  Velocity[Z]            -22.482          24.035        -0.27799      0.00013937
v  ǁVelocityǁ          2.1929e-05          28.614          2.0106          2.2273
v  Pressure                -53763           49173           30749           26645
v  k                   3.6727e-08           2.597        0.013005        0.011946
v  epsilon             1.8748e-05      3.3825e+05          165.85          9.2257
v  TurbVisc            8.1072e-13         0.16883      0.00058883     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16982E+02 0.42248E+01
   Friction velocity        uet   :  0.14612E-01 0.32876E+01
   Friction velocity        uk    :  0.14608E-01 0.32795E+01
   Dimensionless distance   yplus :  0.53429E-04 0.10675E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4612
   Nb of faces within the viscous sub-layer     :      24479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12755E+01     125   0.17046E+00   0.55875E+02 0.36935E+03 
c  Velocity[X]                                      0.14867E+02 
c  Velocity[Y]                                      0.21236E+02 
c  Velocity[Z]                                      0.19772E+02 
c  Pressure     0.75177E-01     887   0.12168E-01   0.48246E+00 0.12634E+04 
c  k            0.38127E-01      69   0.47162E-02   0.46483E-01 0.24800E+04 
c  epsilon      0.96390E+03      50   0.10740E-01   0.44561E+09 0.44370E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2064e-05                            11
a  epsilon       -0.011494                             9


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7983           14.18         0.75461          0.1096
v  Velocity[Y]            -10.636          12.545         0.33562         0.26346
v  Velocity[Z]            -20.714          22.189        -0.28528      0.00025634
v  ǁVelocityǁ          2.2696e-05          25.567          2.0726           2.241
v  Pressure                -57561           49079           30468           26515
v  k                   5.2156e-09          3.5148        0.013836        0.012106
v  epsilon             1.8583e-05      6.1812e+05          193.56          9.6299
v  TurbVisc            8.4129e-13         0.16883      0.00060027        0.008617
v  total_pressure      4.4244e+05      5.4908e+05      5.3047e+05      5.2651e+05


 TIME FOR THE TIME STEP              209:        0.81756E+02

===============================================================


 INSTANT    0.210000000E+03   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         0.342660216E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441505E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14733E+02 0.43270E+01
   Friction velocity        uet   :  0.12941E-01 0.33138E+01
   Friction velocity        uk    :  0.12936E-01 0.33058E+01
   Dimensionless distance   yplus :  0.54061E-04 0.10706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4668
   Nb of faces within the viscous sub-layer     :      24277
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12835E+01     125   0.16895E+00   0.51457E+02 0.35764E+03 
c  Velocity[X]                                      0.13907E+02 
c  Velocity[Y]                                      0.20422E+02 
c  Velocity[Z]                                      0.17128E+02 
c  Pressure     0.73953E-01     800   0.12------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16982E+02 0.42248E+01
   Friction velocity        uet   :  0.14612E-01 0.32876E+01
   Friction velocity        uk    :  0.14608E-01 0.32795E+01
   Dimensionless distance   yplus :  0.53429E-04 0.10675E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4612
   Nb of faces within the viscous sub-layer     :      24479
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12755E+01     125   0.17046E+00   0.55875E+02 0.36935E+03 
c  Velocity[X]                                      0.14867E+02 
c  Velocity[Y]                                      0.21236E+02 
c  Velocity[Z]                                      0.19772E+02 
c  Pressure     0.75177E-01     887   0.12168E-01   0.48246E+00 0.12634E+04 
c  k            0.38127E-01      69   0.47162E-02   0.46483E-01 0.24800E+04 
c  epsilon      0.96390E+03      50   0.10740E-01   0.44561E+09 0.44370E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.2064e-05                            11
a  epsilon       -0.011494                             9


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.7983           14.18         0.75461          0.1096
v  Velocity[Y]            -10.636          12.545         0.33562         0.26346
v  Velocity[Z]            -20.714          22.189        -0.28528      0.00025634
v  ǁVelocityǁ          2.2696e-05          25.567          2.0726           2.241
v  Pressure                -57561           49079           30468           26515
v  k                   5.2156e-09          3.5148        0.013836        0.012106
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16608E+02 0.44241E+01
   Friction velocity        uet   :  0.99096E-02 0.33344E+01
   Friction velocity        uk    :  0.99055E-02 0.33153E+01
   Dimensionless distance   yplus :  0.54394E-04 0.10700E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4717
   Nb of faces within the viscous sub-layer     :      24106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12918E+01     125   0.17463E+00   0.47375E+02 0.34198E+03 
c  Velocity[X]                                      0.13335E+02 
c  Velocity[Y]                                      0.17874E+02 
c  Velocity[Z]                                      0.16166E+02 
c  Pressure     0.71685E-01    1079   0.11275E-01   0.45680E+00 0.33179E+04 
c  k            0.38797E-01      67   0.38858E-02   0.33962E-01 0.21728E+04 
c  epsilon      0.10379E+04      47   0.11328E-01   0.21572E+09 0.33756E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8483e-05                            10
a  epsilon       -0.001913                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9911          14.009         0.77106         0.10935
v  Velocity[Y]            -10.653          12.251         0.33736         0.26349
v  Velocity[Z]            -20.311          19.535         -0.2909     -0.00010631
v  ǁVelocityǁ          2.3226e-05          24.652          2.1287          2.2529
v  Pressure                -60885           50155           30466           26553
v  k                   3.8707e-08          2.9556        0.014691        0.012224
v  epsilon             1.8517e-05      5.1969e+05          214.01          10.024
v  TurbVisc            8.8801e-13         0.16883      0.00061162       0.0086841
v  total_pressure      4.3912e+05      5.5015e+05      5.3047e+05      5.2655e+05


 TIME FOR THE TIME STEP              211:        0.79336E+02

===============================================================


 INSTANT    0.212000000E+03   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.404591655E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441479E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14314E+02 0.44410E+01
   Friction velocity        uet   :  0.83795E-02 0.33480E+01
   Friction velocity        uk    :  0.83787E-02 0.33380E+01
   Dimensionless distance   yplus :  0.54492E-04 0.10677E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4764
   Nb of faces within the viscous sub-layer     :      23966
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12971E+01     124   0.17416E+00   0.45251E+02 0.33439E+03 
c  Velocity[X]                                      0.12340E+02 
c  Velocity[Y]      ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16608E+02 0.44241E+01
   Friction velocity        uet   :  0.99096E-02 0.33344E+01
   Friction velocity        uk    :  0.99055E-02 0.33153E+01
   Dimensionless distance   yplus :  0.54394E-04 0.10700E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4717
   Nb of faces within the viscous sub-layer     :      24106
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12918E+01     125   0.17463E+00   0.47375E+02 0.34198E+03 
c  Velocity[X]                                      0.13335E+02 
c  Velocity[Y]                                      0.17874E+02 
c  Velocity[Z]                                      0.16166E+02 
c  Pressure     0.71685E-01    1079   0.11275E-01   0.45680E+00 0.33179E+04 
c  k            0.38797E-01      67   0.38858E-02   0.33962E-01 0.21728E+04 
c  epsilon      0.10379E+04      47   0.11328E-01   0.21572E+09 0.33756E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8483e-05                            10
a  epsilon       -0.001913                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -4.9911          14.009         0.77106         0.10935
v  Velocity[Y]            -10.653          12.251         0.33736         0.26349
v  Velocity[Z]            -20.311          19.535         -0.2909     -0.00010631
v  ǁVelocityǁ          2.3226e-05          24.652     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14782E+02 0.44622E+01
   Friction velocity        uet   :  0.87989E-02 0.33450E+01
   Friction velocity        uk    :  0.87972E-02 0.33386E+01
   Dimensionless distance   yplus :  0.55050E-04 0.10422E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4820
   Nb of faces within the viscous sub-layer     :      23841
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13001E+01     123   0.17279E+00   0.41336E+02 0.31478E+03 
c  Velocity[X]                                      0.11727E+02 
c  Velocity[Y]                                      0.15007E+02 
c  Velocity[Z]                                      0.14601E+02 
c  Pressure     0.66734E-01     712   0.11598E-01   0.41810E+00 0.70594E+03 
c  k            0.39228E-01      66   0.33257E-02   0.31582E-01 0.16755E+04 
c  epsilon      0.10733E+04      51   0.62851E-02   0.81036E+08 0.13716E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8576e-05                             9
a  epsilon       -0.018892                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2306          14.004         0.78396         0.10862
v  Velocity[Y]            -10.921            12.2         0.33997          0.2638
v  Velocity[Z]            -20.811          19.053        -0.29669     -0.00037044
v  ǁVelocityǁ          2.3811e-05          25.001          2.1797          2.2633
v  Pressure                -64448           50906           30453           26577
v  k                   4.0461e-08            2.95          0.0155        0.012306
v  epsilon              1.871e-05      5.2424e+05          233.59          10.375
v  TurbVisc            9.4818e-13         0.16883      0.00062232       0.0087162
v  total_pressure      4.3555e+05      5.5091e+05      5.3045e+05      5.2658e+05


 TIME FOR THE TIME STEP              213:        0.71413E+02

===============================================================


 INSTANT    0.214000000E+03   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.450648599E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441496E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14981E+02 0.44763E+01
   Friction velocity        uet   :  0.55866E-02 0.33436E+01
   Friction velocity        uk    :  0.55859E-02 0.33374E+01
   Dimensionless distance   yplus :  0.55154E-04 0.10366E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4862
   Nb of faces within the viscous sub-layer     :      23671
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
------------------------------------------------Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14782E+02 0.44622E+01
   Friction velocity        uet   :  0.87989E-02 0.33450E+01
   Friction velocity        uk    :  0.87972E-02 0.33386E+01
   Dimensionless distance   yplus :  0.55050E-04 0.10422E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4820
   Nb of faces within the viscous sub-layer     :      23841
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13001E+01     123   0.17279E+00   0.41336E+02 0.31478E+03 
c  Velocity[X]                                      0.11727E+02 
c  Velocity[Y]                                      0.15007E+02 
c  Velocity[Z]                                      0.14601E+02 
c  Pressure     0.66734E-01     712   0.11598E-01   0.41810E+00 0.70594E+03 
c  k            0.39228E-01      66   0.33257E-02   0.31582E-01 0.16755E+04 
c  epsilon      0.10733E+04      51   0.62851E-02   0.81036E+08 0.13716E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8576e-05                             9
a  epsilon       -0.018892                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.2306          14.004         0.78396         0.10862
v  Velocity[Y]            -1Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441511E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16284E+02 0.44871E+01
   Friction velocity        uet   :  0.77173E-02 0.33629E+01
   Friction velocity        uk    :  0.77167E-02 0.33555E+01
   Dimensionless distance   yplus :  0.56134E-04 0.10054E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4900
   Nb of faces within the viscous sub-layer     :      23534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13080E+01     120   0.17122E+00   0.33818E+02 0.28617E+03 
c  Velocity[X]                                      0.10037E+02 
c  Velocity[Y]                                      0.11370E+02 
c  Velocity[Z]                                      0.12411E+02 
c  Pressure     0.67585E-01     693   0.90014E-02   0.41176E+00 0.10297E+04 
c  k            0.39823E-01      64   0.35299E-02   0.30947E-01 0.16385E+04 
c  epsilon      0.11108E+04      49   0.69443E-02   0.67873E+08 0.10843E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8229e-05                            13
a  epsilon       -0.034731                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.3324          14.087         0.79661         0.10858
v  Velocity[Y]            -10.864          12.173         0.34346         0.26436
v  Velocity[Z]            -20.964          19.219        -0.30397     -0.00044738
v  ǁVelocityǁ          2.6041e-05          25.278          2.2264          2.2725
v  Pressure                -67802           51338           30422           26584
v  k                    4.314e-08          2.9585        0.016279        0.012388
v  epsilon             1.9275e-05      5.2909e+05          251.42          10.728
v  TurbVisc            1.0156e-12         0.16883      0.00063089       0.0087319
v  total_pressure       4.322e+05      5.5134e+05      5.3042e+05      5.2658e+05


 TIME FOR THE TIME STEP              215:        0.74441E+02

===============================================================


 INSTANT    0.216000000E+03   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        -0.304717835E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441507E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15041E+02 0.44984E+01
   Friction velocity        uet   :  0.95337E-02 0.33734E+01
   Friction velocity        uk    :  0.94059E-02 0.33651E+01
   Dimensionless distance   yplus :  0.57652E-04 0.99923E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4931
   Nb of faces within the viscous sub-layer     :      23378
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441511E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16284E+02 0.44871E+01
   Friction velocity        uet   :  0.77173E-02 0.33629E+01
   Friction velocity        uk    :  0.77167E-02 0.33555E+01
   Dimensionless distance   yplus :  0.56134E-04 0.10054E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4900
   Nb of faces within the viscous sub-layer     :      23534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13080E+01     120   0.17122E+00   0.33818E+02 0.28617E+03 
c  Velocity[X]                                      0.10037E+02 
c  Velocity[Y]                                      0.11370E+02 
c  Velocity[Z]                                      0.12411E+02 
c  Pressure     0.67585E-01     693   0.90014E-02   0.41176E+00 0.10297E+04 
c  k            0.39823E-01      64   0.35299E-02   0.30947E-01 0.16385E+04 
c  epsilon      0.11108E+04      49   0.69443E-02   0.67873E+08 0.10843E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8229e-05                            13
a  epsilon       -0.034731                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.343755347E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441485E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17414E+02 0.45363E+01
   Friction velocity        uet   :  0.11968E-01 0.33816E+01
   Friction velocity        uk    :  0.11964E-01 0.33667E+01
   Dimensionless distance   yplus :  0.58714E-04 0.10205E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4945
   Nb of faces within the viscous sub-layer     :      23230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13116E+01     120   0.17194E+00   0.32308E+02 0.28098E+03 
c  Velocity[X]                                      0.90992E+01 
c  Velocity[Y]                                      0.10350E+02 
c  Velocity[Z]                                      0.12860E+02 
c  Pressure     0.65715E-01     748   0.73946E-02   0.39500E+00 0.23823E+04 
c  k            0.40439E-01      64   0.30939E-02   0.19769E-01 0.12732E+04 
c  epsilon      0.11527E+04      50   0.62469E-02   0.59977E+08 0.14372E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6568e-05                             9
a  epsilon        -0.89521                             9


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.4853          14.474         0.80994         0.10845
v  Velocity[Y]            -10.883          11.882         0.34582         0.26435
v  Velocity[Z]            -21.638          18.493        -0.31202     -0.00050285
v  ǁVelocityǁ          2.8409e-05          26.068          2.2662            2.28
v  Pressure                -70151           51397           30280           26522
v  k                   2.5781e-08          3.4753        0.017024        0.012472
v  epsilon             2.0254e-05      5.5341e+05          270.49          11.062
v  TurbVisc            1.0535e-12         0.16883      0.00063908       0.0087419
v  total_pressure      4.2985e+05       5.514e+05      5.3028e+05      5.2652e+05


 TIME FOR THE TIME STEP              217:        0.72840E+02

===============================================================


 INSTANT    0.218000000E+03   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         0.121566994E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441499E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15826E+02 0.45488E+01
   Friction velocity        uet   :  0.17811E-01 0.33881E+01
   Friction velocity        uk    :  0.17805E-01 0.33768E+01
   Dimensionless distance   yplus :  0.60061E-04 0.99328E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4984
   Nb of faces within the viscous sub-layer     :      23106
   Total nuInlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.343755347E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441485E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17414E+02 0.45363E+01
   Friction velocity        uet   :  0.11968E-01 0.33816E+01
   Friction velocity        uk    :  0.11964E-01 0.33667E+01
   Dimensionless distance   yplus :  0.58714E-04 0.10205E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4945
   Nb of faces within the viscous sub-layer     :      23230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13116E+01     120   0.17194E+00   0.32308E+02 0.28098E+03 
c  Velocity[X]                                      0.90992E+01 
c  Velocity[Y]                                      0.10350E+02 
c  Velocity[Z]                                      0.12860E+02 
c  Pressure     0.65715E-01     748   0.73946E-02   0.39500E+00 0.23823E+04 
c  k            0.40439E-01      64   0.30939E-02   0.19769E-01 0.12732E+04 
c  epsilon      0.11527E+04      50   0.62469E-02   0.59977E+08 0.14372E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6568e-05                             9
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.281736085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441507E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18710E+02 0.45344E+01
   Friction velocity        uet   :  0.16765E-01 0.33934E+01
   Friction velocity        uk    :  0.16761E-01 0.33826E+01
   Dimensionless distance   yplus :  0.62435E-04 0.10339E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5010
   Nb of faces within the viscous sub-layer     :      22974
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13175E+01     118   0.17225E+00   0.30561E+02 0.26902E+03 
c  Velocity[X]                                      0.96277E+01 
c  Velocity[Y]                                      0.92360E+01 
c  Velocity[Z]                                      0.11697E+02 
c  Pressure     0.60992E-01     640   0.63725E-02   0.36661E+00 0.32163E+04 
c  k            0.40973E-01      63   0.37813E-02   0.24346E-01 0.13122E+04 
c  epsilon      0.11677E+04      48   0.39588E-02   0.43498E+08 0.94477E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1134e-05                             7
a  epsilon       -0.038896                             9


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.9133          14.129         0.82334         0.10825
v  Velocity[Y]            -10.518          11.921         0.34666         0.26423
v  Velocity[Z]            -21.199          18.021        -0.31982      -0.0005923
v  ǁVelocityǁ          3.1667e-05           25.51          2.2977          2.2861
v  Pressure                -72248           51485           30110           26424
v  k                   5.2477e-08          3.5304        0.017618        0.012544
v  epsilon             2.1396e-05      5.5379e+05          283.67          11.327
v  TurbVisc             1.062e-12         0.16883      0.00064623       0.0087491
v  total_pressure      4.2775e+05      5.5148e+05      5.3011e+05      5.2642e+05


 TIME FOR THE TIME STEP              219:        0.71668E+02

===============================================================


 INSTANT    0.220000000E+03   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         0.176912213E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441510E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15052E+02 0.45512E+01
   Friction velocity        uet   :  0.21047E-01 0.33974E+01
   Friction velocity        uk    :  0.21023E-01 0.33847E+01
   Dimensionless distance   yplus :  0.63431E-04 0.98710E+01
   ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.281736085E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441507E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18710E+02 0.45344E+01
   Friction velocity        uet   :  0.16765E-01 0.33934E+01
   Friction velocity        uk    :  0.16761E-01 0.33826E+01
   Dimensionless distance   yplus :  0.62435E-04 0.10339E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5010
   Nb of faces within the viscous sub-layer     :      22974
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13175E+01     118   0.17225E+00   0.30561E+02 0.26902E+03 
c  Velocity[X]                                      0.96277E+01 
c  Velocity[Y]                                      0.92360E+01 
c  Velocity[Z]                                      0.11697E+02 
c  Pressure     0.60992E-01     640   0.63725E-02   0.36661E+00 0.32163E+04 
c  k            0.40973E-01      63   0.37813E-02   0.24346E-01 0.13122E+04 
c  epsilon      0.11677E+04      48   0.39588E-02   0.43498E+08 0.94477E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.595782380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441493E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19140E+02 0.45698E+01
   Friction velocity        uet   :  0.19525E-01 0.34064E+01
   Friction velocity        uk    :  0.19518E-01 0.33934E+01
   Dimensionless distance   yplus :  0.65188E-04 0.10380E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5034
   Nb of faces within the viscous sub-layer     :      22729
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13225E+01     118   0.17698E+00   0.29794E+02 0.26603E+03 
c  Velocity[X]                                      0.91078E+01 
c  Velocity[Y]                                      0.93678E+01 
c  Velocity[Z]                                      0.11319E+02 
c  Pressure     0.57046E-01     585   0.61379E-02   0.34250E+00 0.12952E+04 
c  k            0.41914E-01      64   0.56157E-02   0.37459E-01 0.13842E+04 
c  epsilon      0.11942E+04      55   0.56368E-02   0.45793E+08 0.82189E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2126e-05                            10
a  epsilon       -0.019065                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4035          14.414         0.83532         0.10825
v  Velocity[Y]            -10.652           11.89         0.34661         0.26401
v  Velocity[Z]             -21.28           17.88        -0.32679     -0.00062843
v  ǁVelocityǁ           3.521e-05           25.74          2.3218          2.2913
v  Pressure                -73835           51537           30030           26401
v  k                   5.9557e-08          3.5554        0.018176        0.012616
v  epsilon             2.3082e-05      5.6293e+05          295.94          11.599
v  TurbVisc            1.0825e-12         0.16883      0.00065335       0.0087545
v  total_pressure      4.2617e+05      5.5154e+05      5.3003e+05       5.264e+05


 TIME FOR THE TIME STEP              221:        0.71637E+02

===============================================================


 INSTANT    0.222000000E+03   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         0.168603340E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441579E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15088E+02 0.45596E+01
   Friction velocity        uet   :  0.84429E-02 0.34135E+01
   Friction velocity        uk    :  0.84330E-02 0.34004E+01
   Dimensionless distance   yplus :  0.66954E-04 0.98553E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5052
   Nb of faces within the viscous sub-layer     :      22624
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13235E+01     118   0.17689E+00   0.29794E+02 0.26563E+03 
c  Velocity[X]                                      0.91675E+01 
c  Velocity[Y]                                      0.93328E+01 
c  Velocity[Z]                                      0.11294E+02 
c  Pressure     0.56148E-01     750   0.61061E-02   0.33938E+00 0.19903E+04 
c  k            0.42727E-01      63   0.60779E-02   0.40264E-01 0.13032E+04 
c  epsilon      0.12027E+04      48   0.56818E-02   0.60689E+08 0.94842E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.7065e-05                             8
a  epsilon        -0.10977                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8394          15.354         0.84058         0.10823
v  Velocity[Y]            -11.722           11.87         0.34641         0.26397
v  Velocity[Z]            -22.381          18.558        -0.32951     -0.00051138
v  ǁVelocityǁ          3.6849e-05          27.263          2.3315          2.2935
v  Pressure                -74950           51589           29995           26386
v  k                   6.3755e-08          3.5574          0.0184        0.012653
v  epsilon             2.4209e-05      5.6283e+05          301.85          11.724
v  TurbVisc            1.1032e-12         0.16883       0.0006562       0.0087567
v  total_pressure      4.2505e+05      5.5159e+05         5.3e+05      5.2639e+05


 TIME FOR THE TIME STEP              222:        0.77754E+02

===============================================================


 INSTANT    0.223000000E+03   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        -0.218490170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441586E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16580E+02 0.45830E+01
   Friction velocity        uet   :  0.13290E-01 0.34178E+01
   Friction velocity        uk    :  0.13274E-01 0.34057E+01
   Dimensionless distance   yplus :  0.68526E-04 0.10232E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5059
   Nb of faces within the viscous sub-layer     :      22535
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13267E+01     118   0.17115E+00   0.29262E+02 0.26559E+03 
c  Velocity[X]                                      0.89903E+01 
c  Velocity[Y]                                      0.88812E+01 
c  Velocity[Z]                                      0.11391E+02 
c  Pressure     0.54870E-01     882   0.57449E-02   0.32994E+00 0.14778E+04 
c  k            0.43932E-01      63   0.66575E-02   0.50725E-01 0.18027E+04 
c  epsilon      0.12239E+04      48   0.83883E-02   0.31094E+09 0.30026E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -3.775e-05                             9
a  epsilon         -124.75                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7833          14.797         0.84517         0.10827
v  Velocity[Y]            -12.131          11.976         0.34624         0.26382
v  Velocity[Z]            -21.992          18.031        -0.33218     -0.00056414
v  ǁVelocityǁ          3.8491e-05          26.265          2.3396          2.2953
v  Pressure                -75496           51791           30044           26441
v  k                   6.8449e-08          3.5734         0.01862        0.012689
v  epsilon             2.4707e-05      6.0697e+05          308.99          11.839
v  TurbVisc            1.1275e-12         0.16883      0.00065904       0.0087596
v  total_pressure       4.245e+05      5.5179e+05      5.3004e+05      5.2644e+05


 TIME FOR THE TIME STEP              223:        0.79777E+02

===============================================================


 INSTANT    0.224000000E+03   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.332446293E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441616E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16441E+02 0.45757E+01
   Friction velocity        uet   :  0.16006E-01 0.34309E+01
   Friction velocity        uk    :  0.16000E-01 0.34176E+01
   Dimensionless distance   yplus :  0.70110E-04 0.10043E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5070
   Nb of faces within the viscous sub-layer     :      22467
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13290E+01     118   0.17730E+00   0.28513E+02 0.25846E+03 
c  Velocity[X]                                      0.91002E+01 
c  Velocity[Y]                                      0.86759E+01 
c  Velocity[Z]                                      0.10737E+02 
c  Pressure     0.53686E-01     640   0.56001E-02   0.32541E+00 0.11019E+04 
c  k            0.45516E-01      62   0.73349E-02   0.45545E-01 0.12231E+04 
c  epsilon      0.12348E+04      44   0.95489E-02   0.81452E+08 0.14541E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011298                            10
a  epsilon        -0.14425                            11


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -5.8885          14.754         0.84856         0.10839
v  Velocity[Y]            -10.855          11.963         0.34608         0.26371
v  Velocity[Z]             -24.79          18.735        -0.33413     -0.00054979
v  ǁVelocityǁ          4.0687e-05          28.133          2.3464          2.2969
v  Pressure                -76587           51790           30026           26439
v  k                    7.371e-08          3.8671        0.018775        0.012726
v  epsilon             2.7103e-05      5.7004e+05           310.3          11.957
v  TurbVisc            1.1556e-12         0.16883      0.00066153       0.0087622
v  total_pressure      4.2341e+05      5.5179e+05      5.3003e+05      5.2644e+05


 TIME FOR THE TIME STEP              224:        0.63934E+02

===============================================================


 INSTANT    0.225000000E+03   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        -0.929012367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441594E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19382E+02 0.45951E+01
   Friction velocity        uet   :  0.13694E-01 0.34360E+01
   Friction velocity        uk    :  0.13677E-01 0.34227E+01
   Dimensionless distance   yplus :  0.72242E-04 0.10372E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5078
   Nb of faces within the viscous sub-layer     :      22371
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13293E+01     117   0.17412E+00   0.30845E+02 0.26670E+03 
c  Velocity[X]                                      0.92432E+01 
c  Velocity[Y]                                      0.93254E+01 
c  Velocity[Z]                                      0.12276E+02 
c  Pressure     0.52130E-01     764   0.55479E-02   0.31277E+00 0.14193E+04 
c  k            0.47093E-01      62   0.54107E-02   0.25948E-01 0.83986E+03 
c  epsilon      0.12360E+04      46   0.36201E-02   0.16183E+08 0.55323E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.2496e-05                            10
a  epsilon       -0.051693                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7334          14.275         0.85148         0.10817
v  Velocity[Y]            -10.573          11.955         0.34588         0.26362
v  Velocity[Z]            -21.393          18.304        -0.33554     -0.00051604
v  ǁVelocityǁ           4.194e-05          25.483          2.3521          2.2985
v  Pressure                -77404           52003           30052           26476
v  k                   7.9655e-08          4.4339        0.018928        0.012758
v  epsilon             2.8849e-05      5.7159e+05          313.58          12.035
v  TurbVisc            1.1923e-12         0.16883      0.00066402       0.0087649
v  total_pressure       4.226e+05        5.52e+05      5.3005e+05      5.2648e+05


 TIME FOR THE TIME STEP              225:        0.68067E+02

===============================================================


 INSTANT    0.226000000E+03   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         0.704537644E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441592E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY Cv  TurbVisc            1.1556e-12         0.16883      0.00066153       0.0087622
v  total_pressure      4.2341e+05      5.5179e+05      5.3003e+05      5.2644e+05


 TIME FOR THE TIME STEP              224:        0.68685E+02

===============================================================


 INSTANT    0.225000000E+03   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        -0.929012367E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441594E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19382E+02 0.45951E+01
   Friction velocity        uet   :  0.13694E-01 0.34360E+01
   Friction velocity        uk    :  0.13677E-01 0.34227E+01
   Dimensionless distance   yplus :  0.72242E-04 0.10372E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5078
   Nb of faces within the viscous sub-layer     :      22371
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13293E+01     117   0.17412E+00   0.30845E+02 0.26670E+03 
c  Velocity[X]                                      0.92432E+01 
c  Velocity[Y]                                      0.93254E+01 
cv  k                   8.6369e-08          4.5777        0.019067        0.012783
v  epsilon             3.0753e-05      5.7695e+05          317.18          12.121
v  TurbVisc            1.2291e-12         0.17573      0.00066645       0.0087674
v  total_pressure      4.2133e+05       5.522e+05      5.3007e+05      5.2651e+05


 TIME FOR THE TIME STEP              226:        0.66159E+02

===============================================================


 INSTANT    0.227000000E+03   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        -0.927431660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441584E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17122E+02 0.46131E+01
   Friction velocity        uet   :  0.13627E-01 0.34497E+01
   Friction velocity        uk    :  0.13612E-01 0.34364E+01
   Dimensionless distance   yplus :  0.74017E-04 0.10310E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5112
   Nb of faces within the viscous sub-layer     :      22264
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13329E+01     116   0.17132E+00   0.29843E+02 0.25912E+03 
c  Velocity[X]                                      0.91725E+01 
c  Velocity[Y]                                      0.89665E+01 
c  Velocity[Z]                                      0.11704E+02 
c  Pressure     0.50239E-01     714   0.52955E-02   0.30406E+00 0.97522E+03 
c  k            0.49020E-01      61   0.34349E-02   0.13534E-01 0.76483E+03 
c  epsilon      0.12541E+04      44   0.44119E-02   0.18940E+08 0.55771E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6314e-05                            10
a  epsilon        -0.21426                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0218          14.573         0.85522         0.10852
v  Velocity[Y]            -10.519           11.95         0.34522         0.26336
v  Velocity[Z]             -21.59          18.555        -0.33833     -0.00062127
v  ǁVelocityǁ          4.3104e-05          25.869          2.3619          2.3011
v  Pressure                -79405           52375           30094           26533
v  k                   9.3892e-08          4.5528        0.019181        0.012806
v  epsilon             3.2735e-05      5.8138e+05          319.46          12.191
v  TurbVisc            1.2645e-12         0.17217       0.0006685       0.0087697
v  total_pressure      4.2059e+05      5.5237e+05      5.3009e+05      5.2653e+05


 TIME FOR THE TIME STEP              227:        0.70683E+02

===============================================================


 INSTANT    0.228000000E+03   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        -0.120433480E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441584E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0       v  k                   8.6369e-08          4.5777        0.019067        0.012783
v  epsilon             3.0753e-05      5.7695e+05          317.18          12.121
v  TurbVisc            1.2291e-12         0.17573      0.00066645       0.0087674
v  total_pressure      4.2133e+05       5.522e+05      5.3007e+05      5.2651e+05


 TIME FOR THE TIME STEP              226:        0.71460E+02

===============================================================


 INSTANT    0.227000000E+03   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        -0.927431660E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441584E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17122E+02 0.46131E+01
   Friction velocity        uet   :  0.13627E-01 0.34497E+01
   Friction velocity        uk    :  0.13612E-01 0.34364E+01
   Dimensionless distance   yplus :  0.74017E-04 0.10310E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5112
   Nb of faces within the viscous sub-layer     :      22264
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13329E+01     116   0.17v  ǁVelocityǁ          4.3275e-05          27.396           2.366          2.3022
v  Pressure                -80516           52211           30085           26534
v  k                   9.3982e-08          4.3696        0.019247        0.012819
v  epsilon             3.4744e-05      5.8554e+05          321.53          12.229
v  TurbVisc            1.2975e-12         0.16883      0.00067039       0.0087717
v  total_pressure      4.1948e+05      5.5221e+05      5.3008e+05      5.2653e+05


 TIME FOR THE TIME STEP              228:        0.64004E+02

===============================================================


 INSTANT    0.229000000E+03   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.103459858E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441573E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16405E+02 0.46209E+01
   Friction velocity        uet   :  0.13132E-01 0.34580E+01
   Friction velocity        uk    :  0.12970E-01 0.34445E+01
   Dimensionless distance   yplus :  0.75059E-04 0.10182E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5137
   Nb of faces within the viscous sub-layer     :      22195
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13375E+01     117   0.17674E+00   0.29457E+02 0.25721E+03 
c  Velocity[X]                                      0.88296E+01 
c  Velocity[Y]                                      0.88335E+01 
c  Velocity[Z]                                      0.11794E+02 
c  Pressure     0.49611E-01    1057   0.53974E-02   0.30126E+00 0.74893E+03 
c  k            0.48730E-01      59   0.37509E-02   0.14345E-01 0.76538E+03 
c  epsilon      0.12613E+04      44   0.38580E-02   0.14938E+08 0.49058E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.6656e-05                             9
a  epsilon        -0.12774                            11


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4577          14.642         0.85696         0.10841
v  Velocity[Y]            -10.394           11.98         0.34423         0.26309
v  Velocity[Z]            -21.615          19.366        -0.34121     -0.00065071
v  ǁVelocityǁ          4.3341e-05          25.866            2.37           2.303
v  Pressure                -81179           52229           30108           26565
v  k                   5.8492e-08          4.1351        0.019314        0.012832
v  epsilon             3.6784e-05       5.844e+05          322.65          12.262
v  TurbVisc             1.323e-12         0.16883      0.00067173       0.0087734
v  total_pressure      4.1882e+05      5.5223e+05      5.3011e+05      5.2656e+05


 TIME FOR THE TIME STEP              229:        0.73848E+02

===============================================================


 INSTANT    0.230000000E+03   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        -0.759460834E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441610E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15561E+02 0.46167E+01
   Friction velocity        uet   :  0.22200E-01 0.34642E+01
   Friction velocity        uk    :  0.21321E-01 0.34507E+01
   Dimensionless distance   yplus :  0.75169E-04 0.10201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5159
   Nb of faces within the viscous sub-layer     :      22164
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13388E+01     116   0.17516E+00   0.30107E+02 0.25768E+03 
c  Velocity[X]                                      0.92980E+01 
c  Velocity[Y]                                      0.88574E+01 
c  Velocity[Z]                                      0.11952E+02 
c  Pressure     0.47607E-01     610   0.55098E-02   0.29166E+00 0.87456E+03 
c  k            0.48552E-01      58   0.36265E-02   0.14604E-01 0.84205E+03 
c  epsilon      0.12622E+04      40   0.44276E-02   0.27539E+08 0.62322E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010405                             8
a  epsilon         -1.5978                            12


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.0783          15.337          0.8573         0.10852
v  Velocity[Y]            -11.582          12.044         0.34399         0.26302
v  Velocity[Z]            -22.449            18.6        -0.34302     -0.00068799
v  ǁVelocityǁ          4.4457e-05          27.308          2.3738          2.3036
v  Pressure                -82608           52205           30107           26565
v  k                   1.2674e-09          3.9312        0.019363        0.012844
v  epsilon              3.881e-05      5.8997e+05          323.98          12.301
v  TurbVisc            1.3443e-12         0.16883      0.00067317       0.0087746
v  total_pressure      4.1739e+05       5.522e+05      5.3011e+05      5.2657e+05


 TIME FOR THE TIME STEP              230:        0.76090E+02

===============================================================


 INSTANT    0.231000000E+03   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        -0.385996383E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441590E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17420E+02 0.46338E+01
   Friction velocity        uet   :  0.97747E-02 0.34691E+01
   Friction velocity        uk    :  0.99206E-02 0.34556E+01
   Dimensionless distance   yplus :  0.76259E-04 0.10341E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5170
   Nb of faces within the viscous sub-layer     :      22156
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13396E+01     117   0.17258E+00   0.28365E+02 0.25042E+03 
c  Velocity[X]                                      0.88865E+01 
c  Velocity[Y]                                      0.87873E+01 
c  Velocity[Z]                                      0.10692E+02 
c  Pressure     0.47567E-01     797   0.53822E-02   0.28954E+00 0.98662E+03 
c  k            0.48506E-01      58   0.30543E-02   0.14745E-01 0.10738E+04 
c  epsilon      0.12635E+04      44   0.54580E-02   0.57853E+08 0.11092E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.8566e-05                            11
a  epsilon         -2.1762                            12


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.1106          14.606         0.85774         0.10848
v  Velocity[Y]            -10.155          12.181         0.34445         0.26305
v  Velocity[Z]            -21.549          18.646        -0.34481     -0.00059357
v  ǁVelocityǁ          4.4354e-05          25.855          2.3779          2.3042
v  Pressure                -82915           52361           30170           26625
v  k                   3.5009e-09          3.8334        0.019411        0.012854
v  epsilon             1.6203e-06      5.8756e+05          325.91          12.318
v  TurbVisc             1.364e-12         0.16883      0.00067469        0.008776
v  total_pressure      4.1708e+05      5.5236e+05      5.3017e+05      5.2663e+05


 TIME FOR THE TIME STEP              231:        0.76803E+02

===============================================================


 INSTANT    0.232000000E+03   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         0.470819420E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441583E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15543E+02 0.46220E+01
   Friction velocity        uet   :  0.70631E-02 0.34859E+01
   Friction velocity        uk    :  0.72920E-02 0.34666E+01
   Dimensionless distance   yplus :  0.76188E-04 0.10130E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5176
   Nb of faces within the viscous sub-layer     :      22081
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13394E+01     117   0.17343E+00   0.27363E+02 0.24487E+03 
c  Velocity[X]                                      0.85658E+01 
c  Velocity[Y]                                      0.83347E+01 
c  Velocity[Z]                                      0.10462E+02 
c  Pressure     0.46875E-01     584   0.53942E-02   0.28883E+00 0.79636E+03 
c  k            0.48522E-01      57   0.28509E-02   0.14656E-01 0.12038E+04 
c  epsilon      0.12763E+04      41   0.41778E-02   0.10050E+09 0.18208E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.8242e-05                            10
a  epsilon         -1.4521                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7269          14.641         0.85812         0.10847
v  Velocity[Y]            -10.684          12.138         0.34503         0.26287
v  Velocity[Z]            -23.139          18.487        -0.34662     -0.00065049
v  ǁVelocityǁ          4.4388e-05          27.384          2.3829          2.3048
v  Pressure                -83884           52651           30173           26633
v  k                   1.1844e-07          3.7608        0.019485        0.012866
v  epsilon             4.2805e-05      5.9192e+05          330.39          12.367
v  TurbVisc            1.3776e-12         0.16883      0.00067587       0.0087767
v  total_pressure      4.1612e+05      5.5265e+05      5.3017e+05      5.2663e+05


 TIME FOR THE TIME STEP              232:        0.64914E+02

===============================================================


 INSTANT    0.233000000E+03   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        -0.146347901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441581E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15926E+02 0.46384E+01
   Friction velocity        uet   :  0.25876E-01 0.34862E+01
   Friction velocity        uk    :  0.25426E-01 0.34727E+01
   Dimensionless distance   yplus :  0.76200E-04 0.99696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5197
   Nb of faces within the viscous sub-layer     :      22055
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13417E+01     116   0.17455E+00   0.28483E+02 0.24953E+03 
c  Velocity[X]                                      0.86009E+01 
c  Velocity[Y]                                      0.88400E+01 
c  Velocity[Z]                                      0.11042E+02 
c  Pressure     0.45262E-01     681   0.53941E-02   0.27860E+00 0.68622E+03 
c  k            0.48813E-01      57   0.33661E-02   0.16230E-01 0.11481E+04 
c  epsilon      0.12765E+04      41   0.58331E-02   0.85223E+08 0.16153E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00015626                            12
a  epsilon         -136.37                            16


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4607          14.619         0.85853         0.10841
v  Velocity[Y]            -10.132          12.168         0.34606         0.26297
v  Velocity[Z]            -21.724          19.098        -0.34851     -0.00061319
v  ǁVelocityǁ          4.4991e-05          26.027          2.3876          2.3055
v  Pressure                -84349           52827           30211           26673
v  k                    1.228e-07          3.7753        0.019504        0.012875
v  epsilon             4.4748e-05      5.9112e+05          328.38          12.389
v  TurbVisc            1.3896e-12         0.16883      0.00067707       0.0087776
v  total_pressure      4.1565e+05      5.5283e+05      5.3021e+05      5.2667e+05


 TIME FOR THE TIME STEP              233:        0.69758E+02

===============================================================


 INSTANT    0.234000000E+03   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.7269          14.641         0.85812         0.10847
v  Velocity[Y]            -10.684          12.138         0.34503         0.26287
v  Velocity[Z]            -23.139          18.487        -0.34662     -0.00065049
v  ǁVelocityǁ          4.4388e-05          27.384          2.3829          2.3048
v  Pressure                -83884           52651           30173           26633
v  k                   1.1844e-07          3.7608        0.019485        0.012866
v  epsilon             4.2805e-05      5.9192e+05          330.39          12.367
v  TurbVisc            1.3776e-12         0.16883      0.00067587       0.0087767
v  total_pressure      4.1612e+05      5.5265e+05      5.3017e+05      5.2663e+05


 TIME FOR THE TIME STEP              232:        0.67944E+02

===============================================================


 INSTANT    0.233000000E+03   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        -0.146347901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441581E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15926E+02 0.46384E+01
   Friction velocity        uet   :  0.25876E-01 0.34862E+01
   Friction velocity        uk    :  0.25426E-01 0.34727E+01
   Dimensionless distance   yplus :  0.76200E-04 0.99696E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5197
   Nb of faces within the viscous sub-layer     :      2
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4807          15.328         0.85878         0.10844
v  Velocity[Y]            -11.187          12.186         0.34742         0.26289
v  Velocity[Z]            -22.135          18.729        -0.35054     -0.00065455
v  ǁVelocityǁ          4.5119e-05          27.086          2.3923          2.3061
v  Pressure                -84969           52767           30233           26689
v  k                   1.2694e-07          3.7411        0.019525        0.012883
v  epsilon             4.6654e-05      5.9468e+05          327.63          12.427
v  TurbVisc            1.4041e-12         0.16883      0.00067821       0.0087778
v  total_pressure      4.1503e+05      5.5277e+05      5.3023e+05      5.2669e+05


 TIME FOR THE TIME STEP              234:        0.69618E+02

===============================================================


 INSTANT    0.235000000E+03   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        -0.958643375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441600E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16256E+02 0.46514E+01
   Friction velocity        uet   :  0.19599E-01 0.34996E+01
   Friction velocity        uk    :  0.19544E-01 0.34860E+01
   Dimensionless distance   yplus :  0.76809E-04 0.10146E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5204
   Nb of faces within the viscous sub-layer     :      21965
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13417E+01     116   0.17584E+00   0.28123E+02 0.24950E+03 
c  Velocity[X]                                      0.86522E+01 
c  Velocity[Y]                                      0.87377E+01 
c  Velocity[Z]                                      0.10733E+02 
c  Pressure     0.46844E-01     897   0.56129E-02   0.28750E+00 0.50715E+03 
c  k            0.49170E-01      61   0.28693E-02   0.11403E-01 0.96848E+03 
c  epsilon      0.12824E+04      51   0.36097E-02   0.51285E+08 0.12668E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.4933e-05                            12
a  epsilon         -2.0292                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4689          14.598         0.85903         0.10855
v  Velocity[Y]            -9.8649          12.239         0.34881         0.26296
v  Velocity[Z]            -21.751           18.89         -0.3523     -0.00061384
v  ǁVelocityǁ          4.4948e-05          25.884           2.397          2.3068
v  Pressure                -85224           52959           30293           26745
v  k                   4.7483e-08          3.6786        0.019591        0.012887
v  epsilon             4.8568e-05      5.9586e+05          331.13          12.448
v  TurbVisc            1.4125e-12         0.16883       0.0006794       0.0087781
v  total_pressure      4.1478e+05      5.5296e+05      5.3029e+05      5.2675e+05


 TIME FOR THE TIME STEP              235:        0.69324E+02

===============================================================


 INSTANT    0.236000000E+03   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

--------------------------------------------
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4807          15.328         0.85878         0.10844
v  Velocity[Y]            -11.187          12.186         0.34742         0.26289
v  Velocity[Z]            -22.135          18.729        -0.35054     -0.00065455
v  ǁVelocityǁ          4.5119e-05          27.086          2.3923          2.3061
v  Pressure                -84969           52767           30233           26689
v  k                   1.2694e-07          3.7411        0.019525        0.012883
v  epsilon             4.6654e-05      5.9468e+05          327.63          12.427
v  TurbVisc            1.4041e-12         0.16883      0.00067821       0.0087778
v  total_pressure      4.1503e+05      5.5277e+05      5.3023e+05      5.2669e+05


 TIME FOR THE TIME STEP              234:        0.84366E+02

===============================================================


 INSTANT    0.235000000E+03   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        -0.958643375E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441600E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16256E+02 0.46514E+01
   Friction velocity        uet   :  0.19599E-01 0.34996E+01
   Friction velocity        uk    :  0.19544E-01 0.34860E+01
   Dimensionless distance   yplus :  0.76809E-04 0-  -------  --------------  --------------  ------------  ------------
a  k           -6.2264e-05                            11
a  epsilon         -2.6887                            11


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2258          14.369         0.85877         0.10839
v  Velocity[Y]            -10.073          12.162          0.3505         0.26287
v  Velocity[Z]             -23.44          19.061        -0.35413     -0.00060013
v  ǁVelocityǁ          4.6346e-05          27.463          2.4018          2.3071
v  Pressure                -85621           53016           30296           26744
v  k                   2.1015e-08          3.6581         0.01964        0.012895
v  epsilon             5.0294e-05      5.9572e+05          330.77          12.488
v  TurbVisc            1.4225e-12         0.16883      0.00067961       0.0087777
v  total_pressure      4.1438e+05      5.5302e+05       5.303e+05      5.2674e+05


 TIME FOR THE TIME STEP              236:        0.61465E+02

===============================================================


 INSTANT    0.237000000E+03   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         0.309873690E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441587E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14843E+02 0.46535E+01
   Friction velocity        uet   :  0.26346E-01 0.35081E+01
   Friction velocity        uk    :  0.26226E-01 0.34945E+01
   Dimensionless distance   yplus :  0.77793E-04 0.99924E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5201
   Nb of faces within the viscous sub-layer     :      21912
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13410E+01     115   0.17210E+00   0.28488E+02 0.24860E+03 
c  Velocity[X]                                      0.87899E+01 
c  Velocity[Y]                                      0.85449E+01 
c  Velocity[Z]                                      0.11154E+02 
c  Pressure     0.47109E-01     826   0.53736E-02   0.28836E+00 0.99812E+03 
c  k            0.49935E-01      59   0.27930E-02   0.13286E-01 0.82289E+03 
c  epsilon      0.12895E+04      44   0.38784E-02   0.34354E+08 0.84217E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019216                            13
a  epsilon          -2.765                            13


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3159          14.681         0.85886         0.10841
v  Velocity[Y]            -9.8195          12.174         0.35241         0.26292
v  Velocity[Z]            -21.754          19.914        -0.35582     -0.00063563
v  ǁVelocityǁ          4.6405e-05          26.053          2.4064          2.3077
v  Pressure                -85613           53245           30340           26777
v  k                    1.384e-07          3.6629        0.019671        0.012898
v  epsilon             5.1838e-05      5.9716e+05          331.09          12.504
v  TurbVisc            1.4373e-12         0.16883      0.00068058       0.0087775
v  total_pressure      4.1439e+05      5.5324e+05      5.3034e+05      5.2678e+05


 TIME FOR THE TIME STEP              237:        0.69517E+02

===============================================================


 INSTANT    0.238000000E+03   TIME STEP NUMBER             238
 -  -------  --------------  --------------  ------------  ------------
a  k           -6.2264e-05                            11
a  epsilon         -2.6887                            11


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2258          14.369         0.85877         0.10839
v  Velocity[Y]            -10.073          12.162          0.3505         0.26287
v  Velocity[Z]             -23.44          19.061        -0.35413     -0.00060013
v  ǁVelocityǁ          4.6346e-05          27.463          2.4018          2.3071
v  Pressure                -85621           53016           30296           26744
v  k                   2.1015e-08          3.6581         0.01964        0.012895
v  epsilon             5.0294e-05      5.9572e+05          330.77          12.488
v  TurbVisc            1.4225e-12         0.16883      0.00067961       0.0087777
v  total_pressure      4.1438e+05      5.5302e+05       5.303e+05      5.2674e+05


 TIME FOR THE TIME STEP              236:        0.69742E+02

===============================================================


 INSTANT    0.237000000E+03   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         0.309873690E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441587E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14843E+02 0.46535E+01
   Friction velocity        u
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020586                            11
a  epsilon         -3.2914                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5255          14.796         0.85903         0.10857
v  Velocity[Y]            -10.734          12.175         0.35411         0.26297
v  Velocity[Z]            -22.003          19.225         -0.3573     -0.00058715
v  ǁVelocityǁ          4.6978e-05          26.643          2.4111          2.3081
v  Pressure                -86089           53277           30366           26803
v  k                   1.4207e-07          3.7823        0.019755        0.012902
v  epsilon             5.3248e-05      6.0188e+05          334.04           12.55
v  TurbVisc            1.4473e-12         0.16883      0.00068137       0.0087769
v  total_pressure      4.1391e+05      5.5328e+05      5.3037e+05       5.268e+05


 TIME FOR THE TIME STEP              238:        0.69654E+02

===============================================================


 INSTANT    0.239000000E+03   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.157750898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441586E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16810E+02 0.46626E+01
   Friction velocity        uet   :  0.25361E-01 0.35149E+01
   Friction velocity        uk    :  0.26408E-01 0.35012E+01
   Dimensionless distance   yplus :  0.78060E-04 0.10226E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5214
   Nb of faces within the viscous sub-layer     :      21834
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13419E+01     114   0.17169E+00   0.27928E+02 0.24907E+03 
c  Velocity[X]                                      0.86784E+01 
c  Velocity[Y]                                      0.89198E+01 
c  Velocity[Z]                                      0.10329E+02 
c  Pressure     0.46470E-01     662   0.50622E-02   0.28430E+00 0.89666E+03 
c  k            0.50079E-01      59   0.43641E-02   0.20836E-01 0.12068E+04 
c  epsilon      0.13066E+04      41   0.51054E-02   0.12408E+09 0.21055E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00022752                            13
a  epsilon         -2.9821                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8544          15.013          0.8591         0.10855
v  Velocity[Y]            -9.7497          12.378         0.35591         0.26307
v  Velocity[Z]            -21.936          18.394         -0.3588     -0.00062198
v  ǁVelocityǁ          4.8584e-05          26.186          2.4154          2.3087
v  Pressure                -86127           53448           30357           26794
v  k                   1.4579e-07          4.2038        0.019793        0.012911
v  epsilon             5.4147e-05      5.9759e+05          335.64           12.57
v  TurbVisc            1.4574e-12         0.16883      0.00068222       0.0087765
v  total_pressure      4.1387e+05      5.5345e+05      5.3036e+05      5.2679e+05


 TIME FOR THE TIME STEP              239:        
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020586                            11
a  epsilon         -3.2914                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5255          14.796         0.85903         0.10857
v  Velocity[Y]            -10.734          12.175         0.35411         0.26297
v  Velocity[Z]            -22.003          19.225         -0.3573     -0.00058715
v  ǁVelocityǁ          4.6978e-05          26.643          2.4111          2.3081
v  Pressure                -86089           53277           30366           26803
v  k                   1.4207e-07          3.7823        0.019755        0.012902
v  epsilon             5.3248e-05      6.0188e+05          334.04           12.55
v  TurbVisc            1.4473e-12         0.16883      0.00068137       0.0087769
v  total_pressure      4.1391e+05      5.5328e+05      5.3037e+05       5.268e+05


 TIME FOR THE TIME STEP              238:        0.80183E+02

===============================================================


 INSTANT    0.239000000E+03   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.157750898E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441586E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         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  epsilon      0.13012E+04      49   0.78208E-02   0.14413E+09 0.22219E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00013342                            16
a  epsilon         -4.1424                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2145          15.147         0.85912         0.10868
v  Velocity[Y]            -10.678          12.146         0.35776         0.26302
v  Velocity[Z]            -22.723           19.21         -0.3601     -0.00049239
v  ǁVelocityǁ           4.826e-05          26.955          2.4195           2.309
v  Pressure                -86604           53508           30357           26793
v  k                   1.4962e-07          4.6102        0.019853        0.012921
v  epsilon             5.4939e-05      6.0338e+05          337.23          12.601
v  TurbVisc            1.4745e-12          8.2114      0.00071254       0.0087787
v  total_pressure       4.134e+05      5.5351e+05      5.3036e+05      5.2679e+05


 TIME FOR THE TIME STEP              240:        0.70842E+02

===============================================================


 INSTANT    0.241000000E+03   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.320559732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441587E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18875E+02 0.46630E+01
   Friction velocity        uet   :  0.25541E-01 0.35116E+01
   Friction velocity        uk    :  0.25856E-01 0.34980E+01
   Dimensionless distance   yplus :  0.79048E-04 0.10533E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5230
   Nb of faces within the viscous sub-layer     :      21783
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13416E+01     114   0.17503E+00   0.28378E+02 0.24987E+03 
c  Velocity[X]                                      0.89459E+01 
c  Velocity[Y]                                      0.86480E+01 
c  Velocity[Z]                                      0.10784E+02 
c  Pressure     0.48054E-01     628   0.56338E-02   0.29452E+00 0.16269E+04 
c  k            0.50872E-01      61   0.42220E-02   0.21162E-01 0.91889E+03 
c  epsilon      0.13073E+04      41   0.44964E-02   0.51775E+08 0.12080E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00032138                            16
a  epsilon         -2.9896                            21


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5911          14.961         0.85951         0.10862
v  Velocity[Y]            -9.8639          12.083         0.35923         0.26304
v  Velocity[Z]             -21.92           21.22        -0.36111     -0.00058892
v  ǁVelocityǁ           4.802e-05          26.171          2.4235          2.3097
v  Pressure                -86619           53723           30450           26865
v  k                    1.536e-07          4.9697        0.019889        0.012927
v  epsilon             5.5632e-05      5.9915e+05          336.13          12.627
v  TurbVisc            1.4856e-12         0.16883     c  epsilon      0.13012E+04      49   0.78208E-02   0.14413E+09 0.22219E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00013342                            16
a  epsilon         -4.1424                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2145          15.147         0.85912         0.10868
v  Velocity[Y]            -10.678          12.146         0.35776         0.26302
v  Velocity[Z]            -22.723           19.21         -0.3601     -0.00049239
v  ǁVelocityǁ           4.826e-05          26.955          2.4195           2.309
v  Pressure                -86604           53508           30357           26793
v  k                   1.4962e-07          4.6102        0.019853        0.012921
v  epsilon             5.4939e-05      6.0338e+05          337.23          12.601
v  TurbVisc            1.4745e-12          8.2114      0.00071254       0.0087787
v  total_pressure       4.134e+05      5.5351e+05      5.3036e+05      5.2679e+05


 TIME FOR THE TIME STEP              240:        0.63130E+02

===============================================================


 INSTANT    0.241000000E+03   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.320559732E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441587E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
 c  Pressure     0.46150E-01     656   0.50081E-02   0.28460E+00 0.76574E+03 
c  k            0.51236E-01      60   0.37703E-02   0.12330E-01 0.60619E+03 
c  epsilon      0.13095E+04      39   0.38406E-02   0.11767E+08 0.37781E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012688                            11
a  epsilon          -4.775                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4577          14.799         0.85963         0.10863
v  Velocity[Y]            -10.797          12.162          0.3605         0.26297
v  Velocity[Z]            -22.289          18.977        -0.36179     -0.00059195
v  ǁVelocityǁ          4.9206e-05          26.886          2.4272          2.3102
v  Pressure                -87013           53642           30368           26809
v  k                   1.5772e-07          5.1431        0.019924        0.012934
v  epsilon             5.6267e-05      6.0115e+05          335.88           12.65
v  TurbVisc            1.4966e-12         0.17786      0.00068588       0.0087768
v  total_pressure      4.1299e+05      5.5364e+05      5.3037e+05      5.2681e+05


 TIME FOR THE TIME STEP              242:        0.74354E+02

===============================================================


 INSTANT    0.243000000E+03   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        -0.294441173E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441491E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16855E+02 0.46670E+01
   Friction velocity        uet   :  0.25908E-01 0.35117E+01
   Friction velocity        uk    :  0.25789E-01 0.34980E+01
   Dimensionless distance   yplus :  0.79768E-04 0.10232E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5240
   Nb of faces within the viscous sub-layer     :      21749
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13416E+01     112   0.17214E+00   0.28091E+02 0.25086E+03 
c  Velocity[X]                                      0.87229E+01 
c  Velocity[Y]                                      0.85656E+01 
c  Velocity[Z]                                      0.10802E+02 
c  Pressure     0.46918E-01     499   0.48525E-02   0.28672E+00 0.17011E+04 
c  k            0.51376E-01      60   0.29151E-02   0.12838E-01 0.91767E+03 
c  epsilon      0.13076E+04      41   0.38378E-02   0.45904E+08 0.10725E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00026084                            14
a  epsilon          -3.433                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8659          14.575         0.85994         0.10877
v  Velocity[Y]            -11.637          12.074         0.36188         0.26311
v  Velocity[Z]            -21.896          18.438        -0.36255     -0.00057576
v  ǁVelocityǁ          4.9019e-05          25.975          2.4303          2.3104
v  Pressure                -87033           53779           30384           26813
v  k                   1.6191e-07          5.1919        0.01999c  Pressure     0.46150E-01     656   0.50081E-02   0.28460E+00 0.76574E+03 
c  k            0.51236E-01      60   0.37703E-02   0.12330E-01 0.60619E+03 
c  epsilon      0.13095E+04      39   0.38406E-02   0.11767E+08 0.37781E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012688                            11
a  epsilon          -4.775                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4577          14.799         0.85963         0.10863
v  Velocity[Y]            -10.797          12.162          0.3605         0.26297
v  Velocity[Z]            -22.289          18.977        -0.36179     -0.00059195
v  ǁVelocityǁ          4.9206e-05          26.886          2.4272          2.3102
v  Pressure                -87013           53642           30368           26809
v  k                   1.5772e-07          5.1431        0.019924        0.012934
v  epsilon             5.6267e-05      6.0115e+05          335.88           12.65
v  TurbVisc            1.4966e-12         0.17786      0.00068588       0.0087768
v  total_pressure      4.1299e+05      5.5364e+05      5.3037e+05      5.2681e+05


 TIME FOR THE TIME STEP              242:        0.68796E+02

===============================================================


 INSTANT    0.243000000E+03   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        -0.294441173E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441491E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0    c  Velocity[X]                                      0.88026E+01 
c  Velocity[Y]                                      0.85470E+01 
c  Velocity[Z]                                      0.10285E+02 
c  Pressure     0.46261E-01     856   0.48051E-02   0.28453E+00 0.95041E+03 
c  k            0.51059E-01      59   0.31769E-02   0.16561E-01 0.13475E+04 
c  epsilon      0.13107E+04      40   0.51813E-02   0.15988E+09 0.22658E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00026106                            16
a  epsilon         -5.4238                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9467          14.878         0.86011         0.10857
v  Velocity[Y]            -10.169           12.15         0.36277         0.26305
v  Velocity[Z]            -22.517          20.084        -0.36291     -0.00055406
v  ǁVelocityǁ          4.8737e-05          26.947          2.4335           2.311
v  Pressure                -87637           53882           30417           26848
v  k                    1.237e-07           5.045        0.020065        0.012941
v  epsilon             3.1011e-05       6.027e+05          341.52           12.69
v  TurbVisc            1.5141e-12         0.17922      0.00068793       0.0087776
v  total_pressure      4.1236e+05      5.5388e+05      5.3042e+05      5.2685e+05


 TIME FOR THE TIME STEP              244:        0.76130E+02

===============================================================


 INSTANT    0.245000000E+03   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        -0.256372628E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441491E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16551E+02 0.46678E+01
   Friction velocity        uet   :  0.21909E-01 0.35033E+01
   Friction velocity        uk    :  0.21892E-01 0.34897E+01
   Dimensionless distance   yplus :  0.79252E-04 0.10196E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5233
   Nb of faces within the viscous sub-layer     :      21688
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13417E+01     112   0.16932E+00   0.28181E+02 0.25136E+03 
c  Velocity[X]                                      0.90921E+01 
c  Velocity[Y]                                      0.83884E+01 
c  Velocity[Z]                                      0.10701E+02 
c  Pressure     0.45516E-01     752   0.47982E-02   0.27733E+00 0.79612E+03 
c  k            0.50859E-01      62   0.33404E-02   0.11712E-01 0.98984E+03 
c  epsilon      0.13148E+04      55   0.83864E-02   0.94119E+08 0.17973E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0001868                            12
a  epsilon         -3.0254                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.2568           14.41         0.86077         0.10857
v  Velocity[Y]            -10.829          12.059         0.36363         0.26295
v  Velocity[Z]            -21.514          20.978        -0.36352     -0.00064723
v  ǁVelocityǁ          4.9329e-05c  Velocity[X]                                      0.88026E+01 
c  Velocity[Y]                                      0.85470E+01 
c  Velocity[Z]                                      0.10285E+02 
c  Pressure     0.46261E-01     856   0.48051E-02   0.28453E+00 0.95041E+03 
c  k            0.51059E-01      59   0.31769E-02   0.16561E-01 0.13475E+04 
c  epsilon      0.13107E+04      40   0.51813E-02   0.15988E+09 0.22658E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00026106                            16
a  epsilon         -5.4238                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9467          14.878         0.86011         0.10857
v  Velocity[Y]            -10.169           12.15         0.36277         0.26305
v  Velocity[Z]            -22.517          20.084        -0.36291     -0.00055406
v  ǁVelocityǁ          4.8737e-05          26.947          2.4335           2.311
v  Pressure                -87637           53882           30417           26848
v  k                    1.237e-07           5.045        0.020065        0.012941
v  epsilon             3.1011e-05       6.027e+05          341.52           12.69
v  TurbVisc            1.5141e-12         0.17922      0.00068793       0.0087776
v  total_pressure      4.1236e+05      5.5388e+05      5.3042e+05      5.2685e+05


 TIME FOR THE TIME STEP              244:        0.77700E+02

===============================================================


 INSTANT    0.245000000E+03   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        -0.256372628E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441491E+00
Free inlet      -----------------------------------------------------------------------------
c  Velocity     0.13422E+01     112   0.17751E+00   0.28242E+02 0.24998E+03 
c  Velocity[X]                                      0.88568E+01 
c  Velocity[Y]                                      0.82419E+01 
c  Velocity[Z]                                      0.11143E+02 
c  Pressure     0.44232E-01     593   0.46914E-02   0.27255E+00 0.11380E+04 
c  k            0.50691E-01      58   0.32762E-02   0.11734E-01 0.88221E+03 
c  epsilon      0.13073E+04      40   0.47457E-02   0.44610E+08 0.10904E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021041                            12
a  epsilon          -2.687                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1477           14.97         0.86138         0.10838
v  Velocity[Y]             -9.851          12.155         0.36432         0.26307
v  Velocity[Z]            -22.472          19.384        -0.36434     -0.00065794
v  ǁVelocityǁ          4.8873e-05          27.112          2.4393           2.312
v  Pressure                -88317           53819           30393           26840
v  k                   1.6809e-07          4.9246        0.020136        0.012949
v  epsilon             5.8527e-05      6.0272e+05             342          12.712
v  TurbVisc            1.5292e-12         0.16888       0.0006893       0.0087788
v  total_pressure      4.1168e+05      5.5382e+05      5.3039e+05      5.2684e+05


 TIME FOR THE TIME STEP              246:        0.61854E+02

===============================================================


 INSTANT    0.247000000E+03   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        -0.254478148E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441590E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17744E+02 0.46580E+01
   Friction velocity        uet   :  0.24869E-01 0.34935E+01
   Friction velocity        uk    :  0.24849E-01 0.34800E+01
   Dimensionless distance   yplus :  0.79402E-04 0.10388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5231
   Nb of faces within the viscous sub-layer     :      21650
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13424E+01     111   0.17573E+00   0.28758E+02 0.25598E+03 
c  Velocity[X]                                      0.87215E+01 
c  Velocity[Y]                                      0.86601E+01 
c  Velocity[Z]                                      0.11376E+02 
c  Pressure     0.44876E-01     724   0.45992E-02   0.27360E+00 0.93962E+03 
c  k            0.51115E-01      57   0.43966E-02   0.16995E-01 0.10617E+04 
c  epsilon      0.13181E+04      41   0.56426E-02   0.60255E+08 0.11340E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019502                            13
a  epsilon         -2.5301                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0116          14.516         0.86239         0.10852
v  Velocity[Y]            -10.984          1-----------------------------------------------------------------------------
c  Velocity     0.13422E+01     112   0.17751E+00   0.28242E+02 0.24998E+03 
c  Velocity[X]                                      0.88568E+01 
c  Velocity[Y]                                      0.82419E+01 
c  Velocity[Z]                                      0.11143E+02 
c  Pressure     0.44232E-01     593   0.46914E-02   0.27255E+00 0.11380E+04 
c  k            0.50691E-01      58   0.32762E-02   0.11734E-01 0.88221E+03 
c  epsilon      0.13073E+04      40   0.47457E-02   0.44610E+08 0.10904E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021041                            12
a  epsilon          -2.687                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1477           14.97         0.86138         0.10838
v  Velocity[Y]             -9.851          12.155         0.36432         0.26307
v  Velocity[Z]            -22.472          19.384        -0.36434     -0.00065794
v  ǁVelocityǁ          4.8873e-05          27.112          2.4393           2.312
v  Pressure                -88317           53819           30393           26840
v  k                   1.6809e-07          4.9246        0.020136        0.012949
v  epsilon             5.8527e-05      6.0272e+05             342          12.712
v  TurbVisc            1.5292e-12         0.16888       0.0006893       0.0087788
v  total_pressure      4.1168e+05      5.5382e+05      5.3039e+05      5.2684e+05


 TIME FOR THE TIME STEP              246:        0.67500E+02

===============================================================


 INSTANT    0.247000000E+03   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        -0.254478148E-17
Rough wall                6           0         0.00-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13414E+01     112   0.17059E+00   0.28247E+02 0.25119E+03 
c  Velocity[X]                                      0.86347E+01 
c  Velocity[Y]                                      0.87252E+01 
c  Velocity[Z]                                      0.10887E+02 
c  Pressure     0.44610E-01     716   0.49736E-02   0.27430E+00 0.61514E+03 
c  k            0.50488E-01      58   0.48462E-02   0.25347E-01 0.85682E+03 
c  epsilon      0.13123E+04      44   0.40458E-02   0.33778E+08 0.68040E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021004                            17
a  epsilon         -2.5333                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0207          14.811         0.86343         0.10836
v  Velocity[Y]            -10.015          12.182         0.36511         0.26302
v  Velocity[Z]            -23.197          21.789          -0.366      -0.0005477
v  ǁVelocityǁ          4.8828e-05           27.17          2.4449           2.313
v  Pressure                -88987           53938           30461           26912
v  k                   1.2284e-07          4.2478        0.020234        0.012947
v  epsilon             5.9003e-05      6.0275e+05          344.03          12.729
v  TurbVisc            1.5282e-12         0.16883      0.00069072       0.0087802
v  total_pressure      4.1101e+05      5.5394e+05      5.3046e+05      5.2691e+05


 TIME FOR THE TIME STEP              248:        0.67757E+02

===============================================================


 INSTANT    0.249000000E+03   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        -0.147422417E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441499E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16932E+02 0.46559E+01
   Friction velocity        uet   :  0.22458E-01 0.34847E+01
   Friction velocity        uk    :  0.22432E-01 0.34734E+01
   Dimensionless distance   yplus :  0.79426E-04 0.10269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5234
   Nb of faces within the viscous sub-layer     :      21607
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13427E+01     111   0.16880E+00   0.29267E+02 0.24949E+03 
c  Velocity[X]                                      0.88882E+01 
c  Velocity[Y]                                      0.83784E+01 
c  Velocity[Z]                                      0.12001E+02 
c  Pressure     0.44321E-01     912   0.46319E-02   0.26973E+00 0.19619E+04 
c  k            0.49935E-01      59   0.41287E-02   0.23645E-01 0.13470E+04 
c  epsilon      0.13199E+04      41   0.64973E-02   0.14490E+09 0.21787E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019533                            13
a  epsilon         -1.0555                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  ------------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13414E+01     112   0.17059E+00   0.28247E+02 0.25119E+03 
c  Velocity[X]                                      0.86347E+01 
c  Velocity[Y]                                      0.87252E+01 
c  Velocity[Z]                                      0.10887E+02 
c  Pressure     0.44610E-01     716   0.49736E-02   0.27430E+00 0.61514E+03 
c  k            0.50488E-01      58   0.48462E-02   0.25347E-01 0.85682E+03 
c  epsilon      0.13123E+04      44   0.40458E-02   0.33778E+08 0.68040E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021004                            17
a  epsilon         -2.5333                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0207          14.811         0.86343         0.10836
v  Velocity[Y]            -10.015          12.182         0.36511         0.26302
v  Velocity[Z]            -23.197          21.789          -0.366      -0.0005477
v  ǁVelocityǁ          4.8828e-05           27.17          2.4449           2.313
v  Pressure                -88987           53938           30461           26912
v  k                   1.2284e-07          4.2478        0.020234        0.012947
v  epsilon             5.9003e-05      6.0275e+05          344.03          12.729
v  TurbVisc            1.5282e-12         0.16883      0.00069072       0.0087802
v  total_pressure      4.1101e+05      5.5394e+05      5.3046e+05      5.2691e+05


 TIME FOR THE TIME STEP              248:        0.76085E+02

===============================================================


 INSTANT    0.249000000E+03   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-----------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13437E+01     111   0.17655E+00   0.29485E+02 0.25259E+03 
c  Velocity[X]                                      0.93886E+01 
c  Velocity[Y]                                      0.86138E+01 
c  Velocity[Z]                                      0.11483E+02 
c  Pressure     0.44084E-01     898   0.50026E-02   0.27142E+00 0.58878E+03 
c  k            0.49523E-01      61   0.40806E-02   0.20368E-01 0.12273E+04 
c  epsilon      0.13155E+04      41   0.79750E-02   0.10911E+09 0.18802E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021963                            12
a  epsilon         -4.1819                            16


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9139          14.398         0.86664         0.10851
v  Velocity[Y]            -10.669          12.103         0.36618         0.26308
v  Velocity[Z]            -24.465          19.112        -0.36788     -0.00054867
v  ǁVelocityǁ          4.7995e-05          28.182          2.4502           2.314
v  Pressure                -89477           53682           30560           26997
v  k                   4.8705e-09          3.6862        0.020332        0.012942
v  epsilon              5.857e-05      6.0339e+05          346.29           12.73
v  TurbVisc            1.5279e-12         0.16883      0.00069151       0.0087813
v  total_pressure      4.1052e+05      5.5368e+05      5.3056e+05        5.27e+05


 TIME FOR THE TIME STEP              250:        0.73237E+02

===============================================================


 INSTANT    0.251000000E+03   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.679323405E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441608E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16587E+02 0.46451E+01
   Friction velocity        uet   :  0.17971E-01 0.34776E+01
   Friction velocity        uk    :  0.17943E-01 0.34641E+01
   Dimensionless distance   yplus :  0.78600E-04 0.10225E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5226
   Nb of faces within the viscous sub-layer     :      21501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13436E+01     112   0.17299E+00   0.29921E+02 0.25587E+03 
c  Velocity[X]                                      0.92891E+01 
c  Velocity[Y]                                      0.90494E+01 
c  Velocity[Z]                                      0.11582E+02 
c  Pressure     0.44033E-01     700   0.51351E-02   0.26771E+00 0.52528E+03 
c  k            0.49043E-01      62   0.41065E-02   0.16682E-01 0.83148E+03 
c  epsilon      0.13176E+04      49   0.45921E-02   0.29389E+08 0.66377E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020657                            11
a  epsilon          -1.632                            16


  **   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13437E+01     111   0.17655E+00   0.29485E+02 0.25259E+03 
c  Velocity[X]                                      0.93886E+01 
c  Velocity[Y]                                      0.86138E+01 
c  Velocity[Z]                                      0.11483E+02 
c  Pressure     0.44084E-01     898   0.50026E-02   0.27142E+00 0.58878E+03 
c  k            0.49523E-01      61   0.40806E-02   0.20368E-01 0.12273E+04 
c  epsilon      0.13155E+04      41   0.79750E-02   0.10911E+09 0.18802E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021963                            12
a  epsilon         -4.1819                            16


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9139          14.398         0.86664         0.10851
v  Velocity[Y]            -10.669          12.103         0.36618         0.26308
v  Velocity[Z]            -24.465          19.112        -0.36788     -0.00054867
v  ǁVelocityǁ          4.7995e-05          28.182          2.4502           2.314
v  Pressure                -89477           53682           30560           26997
v  k                   4.8705e-09          3.6862        0.020332        0.012942
v  epsilon              5.857e-05      6.0339e+05          346.29           12.73
v  TurbVisc            1.5279e-12         0.16883      0.00069151       0.0087813
v  total_pressure      4.1052e+05      5.5368e+05      5.3056e+05        5.27e+05


 TIME FOR THE TIME STEP              250:        0.75923E+02

===============================================================


 INSTANT    0.251000000E+03   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      -----------------------------   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5226
   Nb of faces within the viscous sub-layer     :      21493
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13434E+01     111   0.17110E+00   0.30015E+02 0.25181E+03 
c  Velocity[X]                                      0.97931E+01 
c  Velocity[Y]                                      0.86399E+01 
c  Velocity[Z]                                      0.11582E+02 
c  Pressure     0.44684E-01     863   0.52854E-02   0.27361E+00 0.10529E+04 
c  k            0.48774E-01      61   0.33736E-02   0.10966E-01 0.56701E+03 
c  epsilon      0.13117E+04      46   0.38531E-02   0.87509E+07 0.33299E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020774                            11
a  epsilon         -3.0608                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8768          15.052         0.86978         0.10835
v  Velocity[Y]            -10.694          12.142         0.36754         0.26319
v  Velocity[Z]            -22.126          19.724         -0.3698     -0.00068817
v  ǁVelocityǁ          4.7513e-05          26.554          2.4554          2.3151
v  Pressure                -89346           53672           30614           27047
v  k                   1.6067e-07          3.6582        0.020403        0.012936
v  epsilon             5.8024e-05      5.9721e+05          347.52          12.715
v  TurbVisc            1.5228e-12         0.16883      0.00069202       0.0087824
v  total_pressure      4.1065e+05      5.5367e+05      5.3061e+05      5.2705e+05


 TIME FOR THE TIME STEP              252:        0.71424E+02

===============================================================


 INSTANT    0.253000000E+03   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        -0.777610170E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441605E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16517E+02 0.46417E+01
   Friction velocity        uet   :  0.18181E-01 0.34678E+01
   Friction velocity        uk    :  0.18153E-01 0.34606E+01
   Dimensionless distance   yplus :  0.78276E-04 0.10230E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5222
   Nb of faces within the viscous sub-layer     :      21461
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13455E+01     112   0.17243E+00   0.28322E+02 0.24632E+03 
c  Velocity[X]                                      0.92757E+01 
c  Velocity[Y]                                      0.86692E+01 
c  Velocity[Z]                                      0.10377E+02 
c  Pressure     0.45171E-01     678   0.57541E-02   0.27424E+00 0.62540E+03 
c  k            0.49042E-01      60   0.37056E-02   0.15815E-01 0.11167E+04 
c  epsilon      0.13276E+04      41   0.54772E-02   0.78724E+08 0.16323E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------    ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5226
   Nb of faces within the viscous sub-layer     :      21493
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13434E+01     111   0.17110E+00   0.30015E+02 0.25181E+03 
c  Velocity[X]                                      0.97931E+01 
c  Velocity[Y]                                      0.86399E+01 
c  Velocity[Z]                                      0.11582E+02 
c  Pressure     0.44684E-01     863   0.52854E-02   0.27361E+00 0.10529E+04 
c  k            0.48774E-01      61   0.33736E-02   0.10966E-01 0.56701E+03 
c  epsilon      0.13117E+04      46   0.38531E-02   0.87509E+07 0.33299E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020774                            11
a  epsilon         -3.0608                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8768          15.052         0.86978         0.10835
v  Velocity[Y]            -10.694          12.142         0.36754         0.26319
v  Velocity[Z]            -22.126          19.724         -0.3698     -0.00068817
v  ǁVelocityǁ          4.7513e-05          26.554          2.4554          2.3151
v  Pressure                -89346           53672           30614           27047
v  k                   1.6067e-07          3.6582        0.020403        0.012936
v  epsilon             5.8024e-05      5.9721e+05          347.52          12.715
v  TurbVisc            1.5228e-12         0.16883      0.00069202       0.0087824
v  total_pressure      4.1065e+05      5.5367e+05      5.3061e+05      5.2705e+05


 TIME FOR THE TIME STEP              252:        0.78016E+02

===============================================================


 INSTANT    0.253000   Friction velocity        uet   :  0.14138E-01 0.34959E+01
   Friction velocity        uk    :  0.14069E-01 0.34737E+01
   Dimensionless distance   yplus :  0.77643E-04 0.10453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5216
   Nb of faces within the viscous sub-layer     :      21432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13458E+01     113   0.17702E+00   0.28592E+02 0.24925E+03 
c  Velocity[X]                                      0.89860E+01 
c  Velocity[Y]                                      0.86200E+01 
c  Velocity[Z]                                      0.10986E+02 
c  Pressure     0.43671E-01     845   0.58295E-02   0.26749E+00 0.75894E+03 
c  k            0.49522E-01      58   0.39650E-02   0.11045E-01 0.58385E+03 
c  epsilon      0.13249E+04      38   0.46988E-02   0.11451E+08 0.42093E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020011                            11
a  epsilon         -2.7407                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2754          14.624         0.87261         0.10819
v  Velocity[Y]            -11.281          12.183         0.36831         0.26318
v  Velocity[Z]            -24.026          19.458        -0.37205      -0.0007093
v  ǁVelocityǁ          4.7758e-05          27.599          2.4609          2.3167
v  Pressure                -89680           53637           30723           27137
v  k                   1.5732e-07          4.0309        0.020489        0.012943
v  epsilon             5.7253e-05      5.9699e+05          350.32          12.739
v  TurbVisc            1.5136e-12         0.16883       0.0006925       0.0087835
v  total_pressure      4.1032e+05      5.5364e+05      5.3072e+05      5.2714e+05


 TIME FOR THE TIME STEP              254:        0.83745E+02

===============================================================


 INSTANT    0.255000000E+03   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         0.728802985E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441596E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18852E+02 0.46388E+01
   Friction velocity        uet   :  0.16188E-01 0.34659E+01
   Friction velocity        uk    :  0.15778E-01 0.34574E+01
   Dimensionless distance   yplus :  0.78508E-04 0.10300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5213
   Nb of faces within the viscous sub-layer     :      21410
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13456E+01     111   0.17063E+00   0.30145E+02 0.25905E+03 
c  Velocity[X]                                      0.95828E+01 
c  Velocity[Y]                                      0.87220E+01 
c  Velocity[Z]                                      0.11840E+02 
c  Pressure     0.42104E-01     659   0.52304E-02   0.25570E+00 0.56898E+03 
c  k            0.49392E-01      59   0.28975E-02   0.10072E-01 0.88312E+03 
c  epsilon      0.13161E+04      40   0.48713E-02   0.45591E+08 0.12406E+05 
-------------------------------------------------------   Friction velocity        uet   :  0.14138E-01 0.34959E+01
   Friction velocity        uk    :  0.14069E-01 0.34737E+01
   Dimensionless distance   yplus :  0.77643E-04 0.10453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5216
   Nb of faces within the viscous sub-layer     :      21432
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13458E+01     113   0.17702E+00   0.28592E+02 0.24925E+03 
c  Velocity[X]                                      0.89860E+01 
c  Velocity[Y]                                      0.86200E+01 
c  Velocity[Z]                                      0.10986E+02 
c  Pressure     0.43671E-01     845   0.58295E-02   0.26749E+00 0.75894E+03 
c  k            0.49522E-01      58   0.39650E-02   0.11045E-01 0.58385E+03 
c  epsilon      0.13249E+04      38   0.46988E-02   0.11451E+08 0.42093E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020011                            11
a  epsilon         -2.7407                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.2754          14.624         0.87261         0.10819
v  Velocity[Y]            -11.281          12.183         0.36831         0.26318
v  Velocity[Z]            -24.026          19.458        -0.37205      -0.0007093
v  ǁVelocityǁ          4.7758e-05          27.599          2.4609          2.3167
v  Pressure                -89680           53637           30723           27137
v  k                   1.5732e-07          4.0309        0.020489        0.012943
v  epsilon             5.7253e-05      5.9699e+05          350.32          12.739
v  TurbVisc            1.5136e-12         0.16883       0.0006925       0.0087835
v  total_pressure      4.1032e+05      5.5364e+05                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14809E+02 0.46272E+01
   Friction velocity        uet   :  0.22179E-01 0.34870E+01
   Friction velocity        uk    :  0.22121E-01 0.34648E+01
   Dimensionless distance   yplus :  0.77615E-04 0.99232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5214
   Nb of faces within the viscous sub-layer     :      21388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13471E+01     112   0.17412E+00   0.29150E+02 0.25179E+03 
c  Velocity[X]                                      0.90697E+01 
c  Velocity[Y]                                      0.87310E+01 
c  Velocity[Z]                                      0.11349E+02 
c  Pressure     0.43597E-01     772   0.53370E-02   0.26481E+00 0.11335E+04 
c  k            0.49363E-01      57   0.32713E-02   0.97526E-02 0.88387E+03 
c  epsilon      0.13227E+04      45   0.47780E-02   0.45317E+08 0.11972E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019857                            12
a  epsilon         -2.7664                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3392          14.441          0.8742         0.10815
v  Velocity[Y]             -10.92          12.169          0.3692          0.2632
v  Velocity[Z]             -24.28          19.358         -0.3738     -0.00057944
v  ǁVelocityǁ           4.617e-05          27.918          2.4656          2.3182
v  Pressure                -89932           53564           30805           27201
v  k                   1.5331e-07          3.9987        0.020571        0.012949
v  epsilon             5.6146e-05      5.9605e+05             352          12.765
v  TurbVisc            1.5085e-12         0.16883      0.00069321       0.0087851
v  total_pressure      4.1007e+05      5.5356e+05      5.3081e+05       5.272e+05


 TIME FOR THE TIME STEP              256:        0.77311E+02

===============================================================


 INSTANT    0.257000000E+03   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        -0.263470501E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19392E+02 0.46394E+01
   Friction velocity        uet   :  0.20275E-01 0.34703E+01
   Friction velocity        uk    :  0.20244E-01 0.34581E+01
   Dimensionless distance   yplus :  0.77073E-04 0.10382E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5217
   Nb of faces within the viscous sub-layer     :      21374
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13481E+01     112   0.17087E+00   0.29215E+02 0.25146E+03 
c  Velocity[X]                                      0.93182E+01 
c  Velocity[Y]                                      0.87774E+01 
c  Velocity[Z]                                      0.11119E+02 
c  Pressure     0.43457E-01     772   0.47541E-02   0.26352E+00 0.80036E+03 
c  k            0.49311E-0                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14809E+02 0.46272E+01
   Friction velocity        uet   :  0.22179E-01 0.34870E+01
   Friction velocity        uk    :  0.22121E-01 0.34648E+01
   Dimensionless distance   yplus :  0.77615E-04 0.99232E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5214
   Nb of faces within the viscous sub-layer     :      21388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13471E+01     112   0.17412E+00   0.29150E+02 0.25179E+03 
c  Velocity[X]                                      0.90697E+01 
c  Velocity[Y]                                      0.87310E+01 
c  Velocity[Z]                                      0.11349E+02 
c  Pressure     0.43597E-01     772   0.53370E-02   0.26481E+00 0.11335E+04 
c  k            0.49363E-01      57   0.32713E-02   0.97526E-02 0.88387E+03 
c  epsilon      0.13227E+04      45   0.47780E-02   0.45317E+08 0.11972E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019857                            12
a  epsilon         -2.7664                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3392          14.441          0.8742         0.10815
v  Velocity[Y]             -10.92          12.169          0.3692          0.2632
v  Velocity[Z]             -24.28          19.358         -0.3738     -0.00057944
v  ǁVelocityǁ           4.617e-05          27.918          2.4656          2.3182
v  Pressure                -89932           53564           30805           27201
v  k                   1.5331e-07          3.9987        0.020571        0.012949
v  epsilon             5.6146e-05      5.9605e+05             352    ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18128E+02 0.46354E+01
   Friction velocity        uet   :  0.17353E-01 0.34975E+01
   Friction velocity        uk    :  0.16877E-01 0.34753E+01
   Dimensionless distance   yplus :  0.77594E-04 0.10621E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5229
   Nb of faces within the viscous sub-layer     :      21363
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13496E+01     111   0.17446E+00   0.29062E+02 0.25014E+03 
c  Velocity[X]                                      0.88413E+01 
c  Velocity[Y]                                      0.87148E+01 
c  Velocity[Z]                                      0.11505E+02 
c  Pressure     0.43706E-01     711   0.49655E-02   0.26585E+00 0.97688E+03 
c  k            0.48821E-01      57   0.35501E-02   0.10023E-01 0.86521E+03 
c  epsilon      0.13228E+04      37   0.49236E-02   0.43821E+08 0.12044E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020566                            12
a  epsilon         -2.3143                            21


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3873          15.045         0.87469         0.10819
v  Velocity[Y]            -10.717          12.174         0.37048         0.26326
v  Velocity[Z]             -22.23          19.638        -0.37432     -0.00064245
v  ǁVelocityǁ          4.6304e-05          26.794          2.4693          2.3196
v  Pressure                -90019           53543           30827           27224
v  k                   1.4866e-07          3.6666        0.020603        0.012951
v  epsilon             5.4714e-05      5.9818e+05          352.48          12.787
v  TurbVisc            1.5032e-12         0.16883      0.00069334        0.008786
v  total_pressure      4.0998e+05      5.5354e+05      5.3083e+05      5.2722e+05


 TIME FOR THE TIME STEP              258:        0.73690E+02

===============================================================


 INSTANT    0.259000000E+03   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        -0.250100158E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441578E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16211E+02 0.46451E+01
   Friction velocity        uet   :  0.14474E-01 0.34797E+01
   Friction velocity        uk    :  0.14431E-01 0.34663E+01
   Dimensionless distance   yplus :  0.77233E-04 0.10181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5248
   Nb of faces within the viscous sub-layer     :      21347
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13501E+01     110   0.17225E+00   0.28367E+02 0.25078E+03 
c  Velocity[X]                                      0.89008E+01 
c  Velocity[Y]                                      0.85258E+01 
c  Velocity[Z]          ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18128E+02 0.46354E+01
   Friction velocity        uet   :  0.17353E-01 0.34975E+01
   Friction velocity        uk    :  0.16877E-01 0.34753E+01
   Dimensionless distance   yplus :  0.77594E-04 0.10621E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5229
   Nb of faces within the viscous sub-layer     :      21363
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13496E+01     111   0.17446E+00   0.29062E+02 0.25014E+03 
c  Velocity[X]                                      0.88413E+01 
c  Velocity[Y]                                      0.87148E+01 
c  Velocity[Z]                                      0.11505E+02 
c  Pressure     0.43706E-01     711   0.49655E-02   0.26585E+00 0.97688E+03 
c  k            0.48821E-01      57   0.35501E-02   0.10023E-01 0.86521E+03 
c  epsilon      0.13228E+04      37   0.49236E-02   0.43821E+08 0.12044E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020566                            12
a  epsilon         -2.3143                            21


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3873          15.045         0.87469         0.10819
v  Velocity[Y]            -10.717          12.174         0.37048         0.26326
v  Velocity[Z]             -22.23          19.638        -0.37432     -0.00064245
v  ǁVelocityǁ          4.6304e-05          26.794          2.4693          2.3196
v  Pressure                -90019   Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14807E+02 0.46360E+01
   Friction velocity        uet   :  0.20519E-01 0.35030E+01
   Friction velocity        uk    :  0.20458E-01 0.34806E+01
   Dimensionless distance   yplus :  0.76634E-04 0.98445E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5256
   Nb of faces within the viscous sub-layer     :      21316
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13504E+01     110   0.17279E+00   0.27710E+02 0.24656E+03 
c  Velocity[X]                                      0.88364E+01 
c  Velocity[Y]                                      0.84511E+01 
c  Velocity[Z]                                      0.10422E+02 
c  Pressure     0.46346E-01     790   0.54501E-02   0.28208E+00 0.50839E+03 
c  k            0.48010E-01      57   0.38634E-02   0.12189E-01 0.64187E+03 
c  epsilon      0.13296E+04      37   0.37040E-02   0.12283E+08 0.44580E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021257                            12
a  epsilon         -2.4272                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4969          14.765         0.87411         0.10818
v  Velocity[Y]            -10.783          12.159         0.37194         0.26322
v  Velocity[Z]            -22.665          20.011        -0.37447     -0.00059408
v  ǁVelocityǁ           4.651e-05          26.643           2.472          2.3206
v  Pressure                -90242           53507           30913           27280
v  k                   1.4337e-07           3.662        0.020627        0.012957
v  epsilon              5.297e-05      5.9742e+05          351.72            12.8
v  TurbVisc            1.4932e-12         0.16883      0.00069332       0.0087865
v  total_pressure      4.0976e+05      5.5351e+05      5.3091e+05      5.2728e+05


 TIME FOR THE TIME STEP              260:        0.65251E+02

===============================================================


 INSTANT    0.261000000E+03   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.181849664E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441594E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.46467E+01
   Friction velocity        uet   :  0.20582E-01 0.34715E+01
   Friction velocity        uk    :  0.20405E-01 0.34647E+01
   Dimensionless distance   yplus :  0.77463E-04 0.10115E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5271
   Nb of faces within the viscous sub-layer     :      21294
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13517E+01     11Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14807E+02 0.46360E+01
   Friction velocity        uet   :  0.20519E-01 0.35030E+01
   Friction velocity        uk    :  0.20458E-01 0.34806E+01
   Dimensionless distance   yplus :  0.76634E-04 0.98445E+01
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5256
   Nb of faces within the viscous sub-layer     :      21316
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13504E+01     110   0.17279E+00   0.27710E+02 0.24656E+03 
c  Velocity[X]                                      0.88364E+01 
c  Velocity[Y]                                      0.84511E+01 
c  Velocity[Z]                                      0.10422E+02 
c  Pressure     0.46346E-01     790   0.54501E-02   0.28208E+00 0.50839E+03 
c  k            0.48010E-01      57   0.38634E-02   0.12189E-01 0.64187E+03 
c  epsilon      0.13296E+04      37   0.37040E-02   0.12283E+08 0.44580E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021257                            12
a  epsilon         -2.4272                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4969          14.765         0.87411         0.10818
v  Velocity[Y]            -10.783          12.159         0.37194         0.26322
v  VelocitFree outlet               3          46         0.989441593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18412E+02 0.46405E+01
   Friction velocity        uet   :  0.16090E-01 0.35040E+01
   Friction velocity        uk    :  0.16041E-01 0.34817E+01
   Dimensionless distance   yplus :  0.76699E-04 0.10662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5282
   Nb of faces within the viscous sub-layer     :      21298
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13540E+01     109   0.17942E+00   0.27772E+02 0.24880E+03 
c  Velocity[X]                                      0.86424E+01 
c  Velocity[Y]                                      0.84441E+01 
c  Velocity[Z]                                      0.10685E+02 
c  Pressure     0.45696E-01     767   0.51483E-02   0.27727E+00 0.77702E+03 
c  k            0.48264E-01      57   0.45950E-02   0.23733E-01 0.10690E+04 
c  epsilon      0.13302E+04      38   0.44301E-02   0.86692E+08 0.17764E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019503                            11
a  epsilon         -2.1044                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6669           14.66         0.87333          0.1082
v  Velocity[Y]             -10.85          12.225         0.37338         0.26312
v  Velocity[Z]            -22.272          19.289        -0.37436     -0.00070136
v  ǁVelocityǁ          4.5309e-05          26.688          2.4735          2.3216
v  Pressure                -90525           53278           30980           27320
v  k                   1.3748e-07          4.0165        0.020684        0.012975
v  epsilon             5.0962e-05      6.0048e+05          353.75          12.842
v  TurbVisc            1.4909e-12         0.16883      0.00069376       0.0087874
v  total_pressure      4.0947e+05      5.5328e+05      5.3098e+05      5.2732e+05


 TIME FOR THE TIME STEP              262:        0.70036E+02

===============================================================


 INSTANT    0.263000000E+03   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.197405491E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441596E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16682E+02 0.46481E+01
   Friction velocity        uet   :  0.16816E-01 0.34860E+01
   Friction velocity        uk    :  0.16765E-01 0.34729E+01
   Dimensionless distance   yplus :  0.76369E-04 0.10241E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5285
   Nb of faces within the viscous sub-layer     :      21289
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------------------------Free outlet               3          46         0.989441593E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18412E+02 0.46405E+01
   Friction velocity        uet   :  0.16090E-01 0.35040E+01
   Friction velocity        uk    :  0.16041E-01 0.34817E+01
   Dimensionless distance   yplus :  0.76699E-04 0.10662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5282
   Nb of faces within the viscous sub-layer     :      21298
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13540E+01     109   0.17942E+00   0.27772E+02 0.24880E+03 
c  Velocity[X]                                      0.86424E+01 
c  Velocity[Y]                                      0.84441E+01 
c  Velocity[Z]                                      0.10685E+02 
c  Pressure     0.45696E-01     767   0.51483E-02   0.27727E+00 0.77702E+03 
c  k            0.48264E-01      57   0.45950E-02   0.23733E-01 0.10690E+04 
c  epsilon      0.13302E+04      38   0.44301E-02   0.86692E+08 0.17764E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00019503                            11
a  epsilon         -2.1044                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  -------------Smooth wall               5       41000         0.848873402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441580E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16371E+02 0.46354E+01
   Friction velocity        uet   :  0.13418E-01 0.35037E+01
   Friction velocity        uk    :  0.14730E-01 0.34814E+01
   Dimensionless distance   yplus :  0.77243E-04 0.10088E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5302
   Nb of faces within the viscous sub-layer     :      21292
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13533E+01     110   0.17649E+00   0.26527E+02 0.24481E+03 
c  Velocity[X]                                      0.84409E+01 
c  Velocity[Y]                                      0.85852E+01 
c  Velocity[Z]                                      0.95011E+01 
c  Pressure     0.48150E-01     894   0.66745E-02   0.29175E+00 0.53553E+03 
c  k            0.50152E-01      62   0.42185E-02   0.25378E-01 0.89862E+03 
c  epsilon      0.13273E+04      39   0.55059E-02   0.49033E+08 0.12472E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020721                            11
a  epsilon         -2.0017                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4145          14.905          0.8729         0.10821
v  Velocity[Y]            -11.051          12.202         0.37466         0.26293
v  Velocity[Z]            -23.007          21.426        -0.37434     -0.00073407
v  ǁVelocityǁ          4.5653e-05          27.541          2.4746          2.3218
v  Pressure                -90623           53504           31012           27327
v  k                   1.3117e-07          4.5898        0.020721        0.013004
v  epsilon             4.8762e-05      5.9626e+05           352.6          12.904
v  TurbVisc            1.4856e-12         0.16883      0.00069475       0.0087888
v  total_pressure      4.0938e+05       5.535e+05      5.3101e+05      5.2733e+05


 TIME FOR THE TIME STEP              264:        0.78359E+02

===============================================================


 INSTANT    0.265000000E+03   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         0.606994569E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441605E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17608E+02 0.46492E+01
   Friction velocity        uet   :  0.16332E-01 0.34751E+01
   Friction velocity        uk    :  0.16283E-01 0.34676E+01
   Dimensionless distance   yplus :  0.76700E-04 0.10364E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5302
   Nb of faces within the viscous sub-layer     :      21306
   Total number of wall faces                   :      41000
--------------Smooth wall               5       41000         0.848873402E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441580E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16371E+02 0.46354E+01
   Friction velocity        uet   :  0.13418E-01 0.35037E+01
   Friction velocity        uk    :  0.14730E-01 0.34814E+01
   Dimensionless distance   yplus :  0.77243E-04 0.10088E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5302
   Nb of faces within the viscous sub-layer     :      21292
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13533E+01     110   0.17649E+00   0.26527E+02 0.24481E+03 
c  Velocity[X]                                      0.84409E+01 
c  Velocity[Y]                                      0.85852E+01 
c  Velocity[Z]                                      0.95011E+01 
c  Pressure     0.48150E-01     894   0.66745E-02   0.29175E+00 0.53553E+03 
c  k            0.50152E-01      62   0.42185E-02   0.25378E-01 0.89862E+03 
c  epsilon      0.13273E+04      39   0.55059E-02   0.49033E+08 0.12472E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020721                            11
a  epsilon         -2.0017                            17


  ** Computed fieldBoundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.587263426E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18656E+02 0.46336E+01
   Friction velocity        uet   :  0.15078E-01 0.34980E+01
   Friction velocity        uk    :  0.15034E-01 0.34766E+01
   Dimensionless distance   yplus :  0.76158E-04 0.10692E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5306
   Nb of faces within the viscous sub-layer     :      21299
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13542E+01     111   0.17563E+00   0.27443E+02 0.24674E+03 
c  Velocity[X]                                      0.87187E+01 
c  Velocity[Y]                                      0.82704E+01 
c  Velocity[Z]                                      0.10454E+02 
c  Pressure     0.45657E-01     840   0.50698E-02   0.27674E+00 0.96820E+03 
c  k            0.51155E-01      63   0.35712E-02   0.14058E-01 0.48083E+03 
c  epsilon      0.13333E+04      40   0.33178E-02   0.59901E+07 0.27070E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00029544                            13
a  epsilon         -1.4157                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0211          14.704         0.87292          0.1084
v  Velocity[Y]            -11.177          12.246         0.37553         0.26304
v  Velocity[Z]            -22.607          19.421        -0.37386     -0.00075754
v  ǁVelocityǁ          4.6083e-05          27.008          2.4755          2.3224
v  Pressure                -90688           53866           31155           27432
v  k                   1.2473e-07          4.9181        0.020739        0.013025
v  epsilon              4.645e-05      5.9673e+05          351.66          12.955
v  TurbVisc            1.4769e-12         0.19494      0.00069533       0.0087909
v  total_pressure      4.0931e+05      5.5387e+05      5.3115e+05      5.2743e+05


 TIME FOR THE TIME STEP              266:        0.62120E+02

===============================================================


 INSTANT    0.267000000E+03   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         0.559476527E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441602E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18462E+02 0.46353E+01
   Friction velocity        uet   :  0.14843E-01 0.34616E+01
   Friction velocity        uk    :  0.14800E-01 0.34536E+01
   Dimensionless distance   yplus :  0.77183E-04 0.10456E+02
   ------------------------------------------------------
   Nb of Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.587263426E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18656E+02 0.46336E+01
   Friction velocity        uet   :  0.15078E-01 0.34980E+01
   Friction velocity        uk    :  0.15034E-01 0.34766E+01
   Dimensionless distance   yplus :  0.76158E-04 0.10692E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5306
   Nb of faces within the viscous sub-layer     :      21299
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13542E+01     111   0.17563E+00   0.27443E+02 0.24674E+03 
c  Velocity[X]                                      0.87187E+01 
c  Velocity[Y]                                      0.82704E+01 
c  Velocity[Z]                                      0.10454E+02 
c  Pressure     0.45657E-01     840   0.50698E-02   0.27674E+00 0.96820E+03 
c  k            0.51155E-01      63   0.35712E-02   0.14058E-01 0.48083E+03 
c  epsilon      0.13333E+04      40   0.33178E-02   0.59901E+07 0.27070E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  --------
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.579876691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441606E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18487E+02 0.46248E+01
   Friction velocity        uet   :  0.12493E-01 0.34818E+01
   Friction velocity        uk    :  0.12458E-01 0.34623E+01
   Dimensionless distance   yplus :  0.76619E-04 0.10458E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5299
   Nb of faces within the viscous sub-layer     :      21284
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13555E+01     112   0.17885E+00   0.27476E+02 0.24482E+03 
c  Velocity[X]                                      0.85866E+01 
c  Velocity[Y]                                      0.87532E+01 
c  Velocity[Z]                                      0.10136E+02 
c  Pressure     0.46644E-01     711   0.51054E-02   0.28049E+00 0.82331E+03 
c  k            0.51349E-01      62   0.41713E-02   0.12745E-01 0.68495E+03 
c  epsilon      0.13400E+04      40   0.37039E-02   0.20364E+08 0.63986E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00022869                            13
a  epsilon        -0.43118                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.3688          14.629         0.87377          0.1086
v  Velocity[Y]            -11.082          12.243         0.37635         0.26297
v  Velocity[Z]            -24.139          19.968         -0.3734     -0.00078713
v  ǁVelocityǁ          4.4942e-05           27.13          2.4769          2.3229
v  Pressure                -90725           54114           31268           27508
v  k                    1.184e-07          4.9916        0.020794        0.013039
v  epsilon             4.4134e-05      5.9394e+05          353.31          12.998
v  TurbVisc            1.4717e-12         0.20957      0.00069635       0.0087931
v  total_pressure      4.0927e+05      5.5411e+05      5.3127e+05      5.2751e+05


 TIME FOR THE TIME STEP              268:        0.74095E+02

===============================================================


 INSTANT    0.269000000E+03   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         0.145073807E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441506E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20924E+02 0.46415E+01
   Friction velocity        uet   :  0.17225E-01 0.34585E+01
   Friction velocity        uk    :  0.16748E-01 
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.579876691E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441606E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18487E+02 0.46248E+01
   Friction velocity        uet   :  0.12493E-01 0.34818E+01
   Friction velocity        uk    :  0.12458E-01 0.34623E+01
   Dimensionless distance   yplus :  0.76619E-04 0.10458E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5299
   Nb of faces within the viscous sub-layer     :      21284
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13555E+01     112   0.17885E+00   0.27476E+02 0.24482E+03 
c  Velocity[X]                                      0.85866E+01 
c  Velocity[Y]                                      0.87532E+01 
c  Velocity[Z]                                      0.10136E+02 
c  Pressure     0.46644E-01     711   0.51054E-02   0.28049E+00 0.82331E+03 
c  k            0.51349E-01      62   0.41713E-02   0.12745E-01 0.68495E+03 
c  epsilon      0.13400E+04      40   0.37039E-02   0.20364E+08 0.63986E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippin===============================================================


 INSTANT    0.270000000E+03   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        -0.214927844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441503E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19502E+02 0.48821E+01
   Friction velocity        uet   :  0.18809E-01 0.34698E+01
   Friction velocity        uk    :  0.18756E-01 0.34510E+01
   Dimensionless distance   yplus :  0.76781E-04 0.10599E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5319
   Nb of faces within the viscous sub-layer     :      21256
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13546E+01     111   0.17442E+00   0.26850E+02 0.24544E+03 
c  Velocity[X]                                      0.83700E+01 
c  Velocity[Y]                                      0.86982E+01 
c  Velocity[Z]                                      0.97817E+01 
c  Pressure     0.44569E-01     846   0.52410E-02   0.26916E+00 0.71959E+03 
c  k            0.51815E-01      59   0.46649E-02   0.12070E-01 0.80783E+03 
c  epsilon      0.13410E+04      40   0.56452E-02   0.41252E+08 0.11860E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017666                            11
a  epsilon          -0.529                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.6868          14.914         0.87507         0.10858
v  Velocity[Y]            -10.697          12.257         0.37698         0.26288
v  Velocity[Z]            -21.882          19.445        -0.37239     -0.00077331
v  ǁVelocityǁ           4.544e-05          26.234          2.4782          2.3233
v  Pressure                -90823           54204           31310           27541
v  k                   1.1228e-07          5.1985        0.020826        0.013048
v  epsilon              4.188e-05      5.9621e+05           353.2          13.028
v  TurbVisc            1.4691e-12         0.19059      0.00069687       0.0087943
v  total_pressure      4.0918e+05       5.542e+05      5.3131e+05      5.2754e+05


 TIME FOR THE TIME STEP              270:        0.68022E+02

===============================================================


 INSTANT    0.271000000E+03   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        -0.247846240E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441607E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------===============================================================


 INSTANT    0.270000000E+03   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        -0.214927844E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441503E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19502E+02 0.48821E+01
   Friction velocity        uet   :  0.18809E-01 0.34698E+01
   Friction velocity        uk    :  0.18756E-01 0.34510E+01
   Dimensionless distance   yplus :  0.76781E-04 0.10599E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5319
   Nb of faces within the viscous sub-layer     :      21256
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13546E+01     111   0.17442E+00   0.26850E+02 0.24544E+03 
c  Velocity[X]                                      0.83700E+01 
c  Velocity[Y]                                      0.86982E+01 
c  Velocity[Z]                                      0.97817E+01 
c  Pressure     0.44569E-01     846   0.52410E-02   0.26916E+00 0.71959E+03 
c  k            0.51815E-01      59   0.46649E-02   0.12070E-01 0.80783E+03 
c  epsilon      0.13410E+04 v  total_pressure      4.0949e+05       5.541e+05      5.3137e+05      5.2759e+05


 TIME FOR THE TIME STEP              271:        0.71153E+02

===============================================================


 INSTANT    0.272000000E+03   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        -0.592076017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15407E+02 0.48211E+01
   Friction velocity        uet   :  0.18203E-01 0.34552E+01
   Friction velocity        uk    :  0.17654E-01 0.34427E+01
   Dimensionless distance   yplus :  0.76560E-04 0.10244E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5328
   Nb of faces within the viscous sub-layer     :      21255
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13564E+01     110   0.17737E+00   0.26293E+02 0.24278E+03 
c  Velocity[X]                                      0.82235E+01 
c  Velocity[Y]                                      0.86141E+01 
c  Velocity[Z]                                      0.94550E+01 
c  Pressure     0.41427E-01     785   0.45043E-02   0.25040E+00 0.57206E+03 
c  k            0.50877E-01      57   0.39282E-02   0.10760E-01 0.57920E+03 
c  epsilon      0.13524E+04      38   0.40963E-02   0.90658E+07 0.37695E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017405                            11
a  epsilon        -0.48278                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4653          14.808         0.87678         0.10848
v  Velocity[Y]            -10.597          12.304         0.37766         0.26288
v  Velocity[Z]             -21.17          20.385        -0.37156     -0.00079216
v  ǁVelocityǁ          4.5879e-05          25.558          2.4799          2.3239
v  Pressure                -90783           54156           31411           27626
v  k                    1.064e-07          4.4751         0.02082        0.013045
v  epsilon             3.9711e-05      5.9065e+05          352.64          13.034
v  TurbVisc            1.4655e-12         0.17076      0.00069714       0.0087944
v  total_pressure      4.0922e+05      5.5416e+05      5.3141e+05      5.2763e+05


 TIME FOR THE TIME STEP              272:        0.71907E+02

===============================================================


 INSTANT    0.273000000E+03   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000        -0.423312744E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441483E+00
Free inlet               13           0         0.000000000E+00
Convective 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  total_pressure      4.0949e+05       5.541e+05      5.3137e+05      5.2759e+05


 TIME FOR THE TIME STEP              271:        0.73108E+02

===============================================================


 INSTANT    0.272000000E+03   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        -0.592076017E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15407E+02 0.48211E+01
   Friction velocity        uet   :  0.18203E-01 0.34552E+01
   Friction velocity        uk    :  0.17654E-01 0.34427E+01
   Dimensionless distance   yplus :  0.76560E-04 0.10244E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5328
   Nb of faces within the viscous sub-layer     :      21255
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13564E+01     110   0.17737E+00   0.26293E+02 0.24278E+03 
c  Velocity[X]                                      0.82235E+01 
c  Velocity[Y]                                      0.86141E+01 
c  Velocity[Z]                                      0.94550E+01 
c  Pressure     0.v  epsilon             3.8653e-05      5.9304e+05          353.51          13.038
v  TurbVisc            1.4682e-12         0.16883      0.00069689       0.0087944
v  total_pressure      4.0944e+05      5.5433e+05      5.3148e+05      5.2768e+05


 TIME FOR THE TIME STEP              273:        0.64338E+02

===============================================================


 INSTANT    0.274000000E+03   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        -0.235787881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441568E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19016E+02 0.49972E+01
   Friction velocity        uet   :  0.21512E-01 0.34619E+01
   Friction velocity        uk    :  0.20787E-01 0.34463E+01
   Dimensionless distance   yplus :  0.76366E-04 0.10738E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5339
   Nb of faces within the viscous sub-layer     :      21245
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13565E+01     111   0.18080E+00   0.27799E+02 0.24823E+03 
c  Velocity[X]                                      0.86310E+01 
c  Velocity[Y]                                      0.86724E+01 
c  Velocity[Z]                                      0.10496E+02 
c  Pressure     0.40367E-01     641   0.42607E-02   0.24314E+00 0.48087E+03 
c  k            0.50756E-01      61   0.40468E-02   0.13644E-01 0.68391E+03 
c  epsilon      0.13513E+04      51   0.36718E-02   0.21555E+08 0.50032E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017121                            11
a  epsilon        -0.48165                            14


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9373           14.95         0.87847         0.10856
v  Velocity[Y]            -11.024          12.334         0.37831         0.26284
v  Velocity[Z]            -21.764          20.174        -0.37171     -0.00068158
v  ǁVelocityǁ          4.4598e-05          25.047          2.4822          2.3244
v  Pressure                -91117           54324           31457           27669
v  k                   1.0076e-07          4.2379        0.020867        0.013045
v  epsilon             3.7594e-05      5.9409e+05          354.22          13.067
v  TurbVisc            1.4658e-12         0.16883      0.00069664        0.008794
v  total_pressure      4.0888e+05      5.5432e+05      5.3146e+05      5.2767e+05


 TIME FOR THE TIME STEP              274:        0.68534E+02

===============================================================


 INSTANT    0.275000000E+03   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         0.189482100E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441598E+00
Free inlet               13           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  epsilon             3.8653e-05      5.9304e+05          353.51          13.038
v  TurbVisc            1.4682e-12         0.16883      0.00069689       0.0087944
v  total_pressure      4.0944e+05      5.5433e+05      5.3148e+05      5.2768e+05


 TIME FOR THE TIME STEP              273:        0.63170E+02

===============================================================


 INSTANT    0.274000000E+03   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        -0.235787881E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441568E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19016E+02 0.49972E+01
   Friction velocity        uet   :  0.21512E-01 0.34619E+01
   Friction velocity        uk    :  0.20787E-01 0.34463E+01
   Dimensionless distance   yplus :  0.76366E-04 0.10738E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5339
   Nb of faces within the viscous sub-layer     :      21245
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13565E+01     111   0.18080E+00   0.27799E+02 0.24823E+03 
c  Velocity[X]                                   v  Pressure                -91217           54495           31511           27708
v  k                   2.5061e-08          4.4581        0.020852         0.01304
v  epsilon             3.6562e-05      5.8961e+05          353.48           13.06
v  TurbVisc            1.4618e-12         0.16883      0.00069641       0.0087937
v  total_pressure      4.0878e+05      5.5449e+05      5.3151e+05      5.2771e+05


 TIME FOR THE TIME STEP              275:        0.62750E+02

===============================================================


 INSTANT    0.276000000E+03   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        -0.354010929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441532E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21118E+02 0.56581E+01
   Friction velocity        uet   :  0.16281E-01 0.34658E+01
   Friction velocity        uk    :  0.15853E-01 0.34533E+01
   Dimensionless distance   yplus :  0.76818E-04 0.10771E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5337
   Nb of faces within the viscous sub-layer     :      21236
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13568E+01     111   0.17466E+00   0.27279E+02 0.24625E+03 
c  Velocity[X]                                      0.84411E+01 
c  Velocity[Y]                                      0.89217E+01 
c  Velocity[Z]                                      0.99161E+01 
c  Pressure     0.39036E-01     698   0.41173E-02   0.23440E+00 0.67159E+03 
c  k            0.51199E-01      61   0.52925E-02   0.15992E-01 0.71643E+03 
c  epsilon      0.13519E+04      40   0.56846E-02   0.16900E+08 0.51549E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.000279                            11
a  epsilon        -0.45478                            13


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9455          14.983         0.87972         0.10841
v  Velocity[Y]            -10.503           12.69         0.37912         0.26311
v  Velocity[Z]            -21.308          20.611        -0.37198     -0.00067714
v  ǁVelocityǁ          4.4671e-05          25.652          2.4846          2.3251
v  Pressure                -91481           54557           31520           27719
v  k                   9.5419e-08          4.6561        0.020875        0.013047
v  epsilon             1.2162e-05      5.9206e+05           354.2          13.071
v  TurbVisc            1.4609e-12         0.16883      0.00069598       0.0087934
v  total_pressure      4.0852e+05      5.5456e+05      5.3152e+05      5.2772e+05


 TIME FOR THE TIME STEP              276:        0.62745E+02

===============================================================


 INSTANT    0.277000000E+03   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        -0.370116154E-21
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441590E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15 v  Pressure                -91217           54495           31511           27708
v  k                   2.5061e-08          4.4581        0.020852         0.01304
v  epsilon             3.6562e-05      5.8961e+05          353.48           13.06
v  TurbVisc            1.4618e-12         0.16883      0.00069641       0.0087937
v  total_pressure      4.0878e+05      5.5449e+05      5.3151e+05      5.2771e+05


 TIME FOR THE TIME STEP              275:        0.64835E+02

===============================================================


 INSTANT    0.276000000E+03   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        -0.354010929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441532E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21118E+02 0.56581E+01
   Friction velocity        uet   :  0.16281E-01 0.34658E+01
   Friction velocity        uk    :  0.15853E-01 0.34533E+01
   Dimensionless distance   yplus :  0.76818E-04 0.10771E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5337
   Nb of faces within the viscous sub-layer     :      21236
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------v  Velocity[Z]            -22.264          18.434        -0.37223     -0.00080806
v  ǁVelocityǁ          4.4234e-05          25.805          2.4856          2.3255
v  Pressure                -91500           54704           31556           27752
v  k                    9.287e-08          4.9435        0.020884         0.01305
v  epsilon             3.0276e-05      5.9083e+05          354.34          13.092
v  TurbVisc            1.4584e-12         0.16883      0.00069613       0.0087937
v  total_pressure       4.085e+05       5.547e+05      5.3156e+05      5.2775e+05


 TIME FOR THE TIME STEP              277:        0.72932E+02

===============================================================


 INSTANT    0.278000000E+03   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.253502374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441501E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16195E+02 0.51912E+01
   Friction velocity        uet   :  0.95937E-02 0.34535E+01
   Friction velocity        uk    :  0.96825E-02 0.34345E+01
   Dimensionless distance   yplus :  0.75970E-04 0.10776E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5347
   Nb of faces within the viscous sub-layer     :      21221
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13565E+01     109   0.17765E+00   0.26839E+02 0.24575E+03 
c  Velocity[X]                                      0.84831E+01 
c  Velocity[Y]                                      0.85557E+01 
c  Velocity[Z]                                      0.97999E+01 
c  Pressure     0.37978E-01     663   0.39789E-02   0.22839E+00 0.91178E+03 
c  k            0.51895E-01      62   0.56254E-02   0.21364E-01 0.93544E+03 
c  epsilon      0.13533E+04      41   0.71131E-02   0.77591E+08 0.13664E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00031211                            11
a  epsilon        -0.53067                            21


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6.868          15.125         0.88029         0.10847
v  Velocity[Y]            -10.689          12.415         0.37975         0.26314
v  Velocity[Z]            -21.087          20.126        -0.37269     -0.00075661
v  ǁVelocityǁ          4.5221e-05          25.938          2.4868          2.3258
v  Pressure                -91869           54800           31580           27776
v  k                   9.0425e-08          5.0466        0.020913        0.013055
v  epsilon             3.3621e-05      5.9191e+05          353.83          13.103
v  TurbVisc            1.4572e-12         0.17263      0.00069618       0.0087937
v  total_pressure      4.0813e+05       5.548e+05      5.3158e+05      5.2778e+05


 TIME FOR THE TIME STEP              278:        0.73988E+02

===============================================================


 INSTANT    0.279000000E+03   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         0.233625355E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.0000v  Velocity[Z]            -22.264          18.434        -0.37223     -0.00080806
v  ǁVelocityǁ          4.4234e-05          25.805          2.4856          2.3255
v  Pressure                -91500           54704           31556           27752
v  k                    9.287e-08          4.9435        0.020884         0.01305
v  epsilon             3.0276e-05      5.9083e+05          354.34          13.092
v  TurbVisc            1.4584e-12         0.16883      0.00069613       0.0087937
v  total_pressure       4.085e+05       5.547e+05      5.3156e+05      5.2775e+05


 TIME FOR THE TIME STEP              277:        0.63834E+02

===============================================================


 INSTANT    0.278000000E+03   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall               5       41000         0.253502374E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441501E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16195E+02 0.51912E+01
   Friction velocity        uet   :  0.95937E-02 0.34535E+01
   Friction velocity        uk    :  0.96825E-02 0.34345E+01
   Dimensionless distance   yplus :  0.75970E-04 0.10776E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5347
   Nb of faces within the viscous sub-layer     :      21221
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------v  Velocity[X]            -6.8385          15.038         0.88052          0.1084
v  Velocity[Y]            -11.575          13.493         0.38033         0.26312
v  Velocity[Z]            -23.685          18.962        -0.37317     -0.00084129
v  ǁVelocityǁ          4.5108e-05            26.7           2.488          2.3263
v  Pressure                -91993           54894           31604           27796
v  k                   2.6148e-08          4.3796        0.020919        0.013051
v  epsilon             3.2707e-05      5.9083e+05          353.74          13.097
v  TurbVisc            1.4595e-12         0.17391      0.00069632       0.0087939
v  total_pressure      4.0801e+05      5.5489e+05       5.316e+05       5.278e+05


 TIME FOR THE TIME STEP              279:        0.65103E+02

===============================================================


 INSTANT    0.280000000E+03   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        -0.242695721E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441595E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19808E+02 0.52482E+01
   Friction velocity        uet   :  0.16764E-01 0.34474E+01
   Friction velocity        uk    :  0.16753E-01 0.34349E+01
   Dimensionless distance   yplus :  0.76773E-04 0.10622E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5349
   Nb of faces within the viscous sub-layer     :      21223
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13576E+01     109   0.18020E+00   0.27514E+02 0.24681E+03 
c  Velocity[X]                                      0.83632E+01 
c  Velocity[Y]                                      0.89526E+01 
c  Velocity[Z]                                      0.10198E+02 
c  Pressure     0.36450E-01     604   0.39516E-02   0.21929E+00 0.48218E+03 
c  k            0.51169E-01      62   0.52544E-02   0.18754E-01 0.55764E+03 
c  epsilon      0.13558E+04      39   0.32196E-02   0.77514E+07 0.33324E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00032911                            13
a  epsilon        -0.55962                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4074          15.028         0.88086         0.10834
v  Velocity[Y]            -10.877          12.584         0.38058         0.26321
v  Velocity[Z]            -20.123           20.32        -0.37358     -0.00072476
v  ǁVelocityǁ          4.5236e-05          25.606          2.4894          2.3267
v  Pressure                -92743           54968           31620           27818
v  k                   8.5884e-08          4.0026        0.020941        0.013052
v  epsilon             3.1831e-05      5.8998e+05          354.05          13.115
v  TurbVisc            7.3332e-13         0.16883      0.00069576       0.0087937
v  total_pressure      4.0726e+05      5.5497e+05      5.3162e+05      5.2782e+05


 TIME FOR THE TIME STEP              280:        0.72864E+02

===============================================================


 INSTANT    0.281000000E+03   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.989441543E+00
Smooth wall       v  Velocity[X]            -6.8385          15.038         0.88052          0.1084
v  Velocity[Y]            -11.575          13.493         0.38033         0.26312
v  Velocity[Z]            -23.685          18.962        -0.37317     -0.00084129
v  ǁVelocityǁ          4.5108e-05            26.7           2.488          2.3263
v  Pressure                -91993           54894           31604           27796
v  k                   2.6148e-08          4.3796        0.020919        0.013051
v  epsilon             3.2707e-05      5.9083e+05          353.74          13.097
v  TurbVisc            1.4595e-12         0.17391      0.00069632       0.0087939
v  total_pressure      4.0801e+05      5.5489e+05       5.316e+05       5.278e+05


 TIME FOR THE TIME STEP              279:        0.65650E+02

===============================================================


 INSTANT    0.280000000E+03   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        -0.242695721E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441595E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19808E+02 0.52482E+01
   Friction velocity        uet   :  0.16764E-01 0.34474E+01
   Friction velocity        uk    :  0.16753E-01 0.34349E+01
   Dimensionless distance   yplus :  0.76773E-04 0.10622E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5349
   Nb of faces within the viscous sub-layer     :      21223
   Total number of wall faces                   :      4
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4095          14.867         0.88089          0.1085
v  Velocity[Y]            -11.481          12.396         0.38091         0.26328
v  Velocity[Z]            -23.174          20.247        -0.37395     -0.00077394
v  ǁVelocityǁ           4.581e-05          26.254          2.4906          2.3271
v  Pressure                -92659           55055           31611           27814
v  k                   8.3803e-08           3.786         0.02098        0.013053
v  epsilon             3.1001e-05      5.8995e+05          354.85          13.132
v  TurbVisc            1.4596e-12         0.16883      0.00069563       0.0087937
v  total_pressure      4.0734e+05      5.5506e+05      5.3161e+05      5.2781e+05


 TIME FOR THE TIME STEP              281:        0.70178E+02

===============================================================


 INSTANT    0.282000000E+03   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        -0.100907698E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17794E+02 0.54625E+01
   Friction velocity        uet   :  0.18987E-01 0.34510E+01
   Friction velocity        uk    :  0.18400E-01 0.34320E+01
   Dimensionless distance   yplus :  0.77486E-04 0.10868E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5359
   Nb of faces within the viscous sub-layer     :      21188
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+01     111   0.17406E+00   0.27142E+02 0.24739E+03 
c  Velocity[X]                                      0.87000E+01 
c  Velocity[Y]                                      0.85952E+01 
c  Velocity[Z]                                      0.98472E+01 
c  Pressure     0.35983E-01     608   0.34135E-02   0.21584E+00 0.43898E+03 
c  k            0.51094E-01      60   0.37752E-02   0.98346E-02 0.58432E+03 
c  epsilon      0.13535E+04      38   0.39130E-02   0.13016E+08 0.44683E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0003375                            13
a  epsilon        -0.63769                            16


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1898           15.06         0.88087          0.1084
v  Velocity[Y]            -11.051          13.592         0.38118         0.26325
v  Velocity[Z]            -20.031          19.846        -0.37428     -0.00067099
v  ǁVelocityǁ          4.6128e-05          25.479          2.4917          2.3273
v  Pressure                -93326           55080           31598           27807
v  k                   8.1847e-08          3.7691        0.021006        0.013057
v  epsilon             3.0217e-05       5.888e+05          355.52          13.142
v  TurbVisc            1.4685e-12         0.16883      0.00069554       0.0087935
v  total_pressure      4.0667e+05      5.5508e+05       5.316e+05      5.2781e+05


 TIME FOR THE TIME STEP              282:        0.56957E+02

===============================================================


 INSTANT    0.283000000E+03   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces  
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4095          14.867         0.88089          0.1085
v  Velocity[Y]            -11.481          12.396         0.38091         0.26328
v  Velocity[Z]            -23.174          20.247        -0.37395     -0.00077394
v  ǁVelocityǁ           4.581e-05          26.254          2.4906          2.3271
v  Pressure                -92659           55055           31611           27814
v  k                   8.3803e-08           3.786         0.02098        0.013053
v  epsilon             3.1001e-05      5.8995e+05          354.85          13.132
v  TurbVisc            1.4596e-12         0.16883      0.00069563       0.0087937
v  total_pressure      4.0734e+05      5.5506e+05      5.3161e+05      5.2781e+05


 TIME FOR THE TIME STEP              281:        0.67750E+02

===============================================================


 INSTANT    0.282000000E+03   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        -0.100907698E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17794E+02 0.54625E+01
   Friction velocity        uet   :  0.18987E-01 0.34510E+01
   Friction velocity        uk    :  0.18400E-01 0.34320E+01
   Dimensionless distance   yplus :  0.77486E-04 0.10868E+02
   ------------------------------------------------------
  a  k           -0.00036428                            15
a  epsilon        -0.77215                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8889          14.867         0.88082         0.10843
v  Velocity[Y]            -11.176          12.518         0.38162         0.26326
v  Velocity[Z]            -22.473          18.368         -0.3746     -0.00072445
v  ǁVelocityǁ           4.579e-05          25.951          2.4928          2.3278
v  Pressure                -93429           55188           31619           27823
v  k                   8.0026e-08          3.6816        0.021017        0.013057
v  epsilon             2.9477e-05      5.8814e+05          354.94          13.157
v  TurbVisc            1.4699e-12         0.16883      0.00069546       0.0087936
v  total_pressure      4.0657e+05      5.5519e+05      5.3162e+05      5.2782e+05


 TIME FOR THE TIME STEP              283:        0.71139E+02

===============================================================


 INSTANT    0.284000000E+03   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        -0.106530804E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441603E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.53448E+01
   Friction velocity        uet   :  0.20429E-01 0.34331E+01
   Friction velocity        uk    :  0.21936E-01 0.34207E+01
   Dimensionless distance   yplus :  0.77375E-04 0.10754E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5365
   Nb of faces within the viscous sub-layer     :      21183
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13581E+01     110   0.17682E+00   0.25950E+02 0.24095E+03 
c  Velocity[X]                                      0.82984E+01 
c  Velocity[Y]                                      0.84285E+01 
c  Velocity[Z]                                      0.92226E+01 
c  Pressure     0.35636E-01     662   0.32731E-02   0.21391E+00 0.87361E+03 
c  k            0.51076E-01      58   0.43165E-02   0.10841E-01 0.55934E+03 
c  epsilon      0.13514E+04      41   0.40542E-02   0.82947E+07 0.38356E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00037246                            14
a  epsilon        -0.62447                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.5154          15.049         0.88059         0.10848
v  Velocity[Y]            -11.082          12.469         0.38179         0.26335
v  Velocity[Z]            -21.668          20.384        -0.37464     -0.00074032
v  ǁVelocityǁ           4.692e-05          25.813          2.4938          2.3283
v  Pressure                -94110           55191           31614           27827
v  k                   7.8338e-08          3.8289        0.021041        0.013061
v  epsilon             2.8765e-05      5.8686e+05           355.8          13.162
v  TurbVisc            1.4723e-12         0.16883      0.00069535        0.008793
v  total_pressure      4.0589e+05      5.5519e+05      5.3161e+05      5.2783e+05


 TIME FOR THE TIME STEP              284:        0.70016E+02

===============================================================


 INSTANT    0.285000000E+03   TIME STEP NUMBER             285
 ============================================================= 




   *a  k           -0.00036428                            15
a  epsilon        -0.77215                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8889          14.867         0.88082         0.10843
v  Velocity[Y]            -11.176          12.518         0.38162         0.26326
v  Velocity[Z]            -22.473          18.368         -0.3746     -0.00072445
v  ǁVelocityǁ           4.579e-05          25.951          2.4928          2.3278
v  Pressure                -93429           55188           31619           27823
v  k                   8.0026e-08          3.6816        0.021017        0.013057
v  epsilon             2.9477e-05      5.8814e+05          354.94          13.157
v  TurbVisc            1.4699e-12         0.16883      0.00069546       0.0087936
v  total_pressure      4.0657e+05      5.5519e+05      5.3162e+05      5.2782e+05


 TIME FOR THE TIME STEP              283:        0.71973E+02

===============================================================


 INSTANT    0.284000000E+03   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        -0.106530804E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441603E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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 0.53448E+01
   Friction velocity        uet   :  0.20429E-01 0.34331E+01
   Friction velocity        uk    :  0.
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00037671                            14
a  epsilon        -0.78107                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8249          14.798         0.88014         0.10849
v  Velocity[Y]            -11.298            12.4         0.38222          0.2634
v  Velocity[Z]            -22.894          19.541         -0.3751     -0.00077582
v  ǁVelocityǁ            4.59e-05          26.041          2.4948          2.3286
v  Pressure                -94351           55178           31592           27805
v  k                   7.6792e-08          3.7999        0.021052        0.013063
v  epsilon             2.8103e-05      5.8446e+05          355.65          13.177
v  TurbVisc            1.4781e-12         0.16883      0.00069531       0.0087932
v  total_pressure      4.0565e+05      5.5518e+05      5.3159e+05      5.2781e+05


 TIME FOR THE TIME STEP              285:        0.75005E+02

===============================================================


 INSTANT    0.286000000E+03   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        -0.736776380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441581E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18538E+02 0.58766E+01
   Friction velocity        uet   :  0.13920E-01 0.34343E+01
   Friction velocity        uk    :  0.13654E-01 0.34339E+01
   Dimensionless distance   yplus :  0.77626E-04 0.11415E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5365
   Nb of faces within the viscous sub-layer     :      21161
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13589E+01     111   0.17425E+00   0.26685E+02 0.24405E+03 
c  Velocity[X]                                      0.81938E+01 
c  Velocity[Y]                                      0.87910E+01 
c  Velocity[Z]                                      0.97005E+01 
c  Pressure     0.36237E-01     751   0.29561E-02   0.21708E+00 0.99687E+03 
c  k            0.51347E-01      57   0.39244E-02   0.12957E-01 0.43621E+03 
c  epsilon      0.13491E+04      41   0.28242E-02   0.35187E+07 0.20867E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00036331                            13
a  epsilon        -0.61923                            16


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.9358          15.168         0.87949          0.1084
v  Velocity[Y]             -11.32          12.596         0.38238         0.26336
v  Velocity[Z]            -23.267          19.957        -0.37558     -0.00069783
v  ǁVelocityǁ          4.5542e-05          26.251          2.4956          2.3292
v  Pressure                -94515           55206           31655           27857
v  k                   7.5374e-08          4.0856        0.021073        0.013072
v  epsilon             2.7496e-05      5.8454e+05          355.81            13.2
v  TurbVisc            1.4822e-12         0.16883      0.00069501       0.0087928
v  total_pressure      4.0548e+05      5.5521e+05      5.3165e+05      5.2786e+05


 TIME FOR THE TIME STEP              286:        0.69839E+02

==========================================================
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00037671                            14
a  epsilon        -0.78107                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.8249          14.798         0.88014         0.10849
v  Velocity[Y]            -11.298            12.4         0.38222          0.2634
v  Velocity[Z]            -22.894          19.541         -0.3751     -0.00077582
v  ǁVelocityǁ            4.59e-05          26.041          2.4948          2.3286
v  Pressure                -94351           55178           31592           27805
v  k                   7.6792e-08          3.7999        0.021052        0.013063
v  epsilon             2.8103e-05      5.8446e+05          355.65          13.177
v  TurbVisc            1.4781e-12         0.16883      0.00069531       0.0087932
v  total_pressure      4.0565e+05      5.5518e+05      5.3159e+05      5.2781e+05


 TIME FOR THE TIME STEP              285:        0.73053E+02

===============================================================


 INSTANT    0.286000000E+03   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        -0.736776380E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441581E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00034639                            13
a  epsilon         -0.8595                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.1534          14.959         0.87894         0.10851
v  Velocity[Y]            -11.241          12.626          0.3826          0.2635
v  Velocity[Z]            -22.187          18.202        -0.37588     -0.00075134
v  ǁVelocityǁ          4.6293e-05           24.82          2.4965          2.3295
v  Pressure                -94519           55228           31603           27817
v  k                   7.4104e-08          4.4269        0.021094        0.013077
v  epsilon             2.6941e-05      5.8776e+05          356.25          13.214
v  TurbVisc            1.4858e-12         0.16883      0.00069507       0.0087931
v  total_pressure      4.0548e+05      5.5523e+05       5.316e+05      5.2782e+05


 TIME FOR THE TIME STEP              287:        0.65199E+02

===============================================================


 INSTANT    0.288000000E+03   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         0.164730640E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441586E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17261E+02 0.55656E+01
   Friction velocity        uet   :  0.72425E-02 0.34205E+01
   Friction velocity        uk    :  0.76268E-02 0.34341E+01
   Dimensionless distance   yplus :  0.78039E-04 0.12157E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5364
   Nb of faces within the viscous sub-layer     :      21167
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13581E+01     110   0.17587E+00   0.26689E+02 0.24442E+03 
c  Velocity[X]                                      0.84808E+01 
c  Velocity[Y]                                      0.85657E+01 
c  Velocity[Z]                                      0.96428E+01 
c  Pressure     0.37441E-01     698   0.32469E-02   0.22385E+00 0.57014E+03 
c  k            0.51603E-01      57   0.50815E-02   0.14457E-01 0.44086E+03 
c  epsilon      0.13424E+04      37   0.37730E-02   0.39922E+07 0.22498E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00035269                            13
a  epsilon         -1.2548                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1932           15.33         0.87853         0.10847
v  Velocity[Y]            -11.307          13.061         0.38268         0.26353
v  Velocity[Z]            -22.899          20.303        -0.37608     -0.00080309
v  ǁVelocityǁ          4.6249e-05          25.589          2.4977          2.3301
v  Pressure                -94913           55317           31641           27850
v  k                    7.296e-08          4.5205        0.021091         0.01308
v  epsilon             2.6435e-05      5.8747e+05          355.91          13.208
v  TurbVisc             1.493e-12         0.16883      0.00069511       0.0087929
v  total_pressure      4.0509e+05      5.5532e+05-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00034639                            13
a  epsilon         -0.8595                            15


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.1534          14.959         0.87894         0.10851
v  Velocity[Y]            -11.241          12.626          0.3826          0.2635
v  Velocity[Z]            -22.187          18.202        -0.37588     -0.00075134
v  ǁVelocityǁ          4.6293e-05           24.82          2.4965          2.3295
v  Pressure                -94519           55228           31603           27817
v  k                   7.4104e-08          4.4269        0.021094        0.013077
v  epsilon             2.6941e-05      5.8776e+05          356.25          13.214
v  TurbVisc            1.4858e-12         0.16883      0.00069507       0.0087931
v  total_pressure      4.0548e+05      5.5523e+05       5.316e+05      5.2782e+05


 TIME FOR THE TIME STEP              287:        0.70177E+02

===============================================================


 INSTANT    0.288000000E+03   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         0.164730640E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441586E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------c  k            0.51779E-01      59   0.46769E-02   0.12599E-01 0.45385E+03 
c  epsilon      0.13564E+04      39   0.45908E-02   0.36376E+07 0.20983E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00034941                            14
a  epsilon        -0.74573                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5051           14.75         0.87827          0.1085
v  Velocity[Y]            -11.273           12.42         0.38288         0.26348
v  Velocity[Z]             -20.96          21.658         -0.3764     -0.00079128
v  ǁVelocityǁ          4.6179e-05          24.469          2.4986          2.3302
v  Pressure                -95199           55323           31629           27837
v  k                   7.1944e-08          4.5086        0.021125        0.013087
v  epsilon             2.5974e-05      5.8584e+05          356.55          13.247
v  TurbVisc            1.4958e-12         0.16883      0.00069499       0.0087931
v  total_pressure       4.048e+05      5.5532e+05      5.3163e+05      5.2784e+05


 TIME FOR THE TIME STEP              289:        0.70890E+02

===============================================================


 INSTANT    0.290000000E+03   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        -0.707210501E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441505E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16918E+02 0.54063E+01
   Friction velocity        uet   :  0.87980E-02 0.34209E+01
   Friction velocity        uk    :  0.87699E-02 0.34312E+01
   Dimensionless distance   yplus :  0.77881E-04 0.11634E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5386
   Nb of faces within the viscous sub-layer     :      21146
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13588E+01     108   0.17761E+00   0.26491E+02 0.24235E+03 
c  Velocity[X]                                      0.80681E+01 
c  Velocity[Y]                                      0.84302E+01 
c  Velocity[Z]                                      0.99931E+01 
c  Pressure     0.37180E-01     608   0.32614E-02   0.22109E+00 0.74575E+03 
c  k            0.51655E-01      58   0.49894E-02   0.16381E-01 0.53951E+03 
c  epsilon      0.13497E+04      38   0.51606E-02   0.57090E+07 0.30333E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00037331                            13
a  epsilon        -0.69469                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8115           14.94         0.87788         0.10845
v  Velocity[Y]            -11.495          12.439         0.38269         0.26357
v  Velocity[Z]            -21.504          21.325        -0.37653     -0.00068218
v  ǁVelocityǁ          4.6801e-05          24.995          2.4996          2.3308
v  Pressure                -95697           55371           31643           27852
v  k                   7.1051e-08          4.3368        0.021122        0.013088
v  epsilon             2.5559e-05      5.8593e+05          c  k            0.51779E-01      59   0.46769E-02   0.12599E-01 0.45385E+03 
c  epsilon      0.13564E+04      39   0.45908E-02   0.36376E+07 0.20983E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00034941                            14
a  epsilon        -0.74573                            17


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.5051           14.75         0.87827          0.1085
v  Velocity[Y]            -11.273           12.42         0.38288         0.26348
v  Velocity[Z]             -20.96          21.658         -0.3764     -0.00079128
v  ǁVelocityǁ          4.6179e-05          24.469          2.4986          2.3302
v  Pressure                -95199           55323           31629           27837
v  k                   7.1944e-08          4.5086        0.021125        0.013087
v  epsilon             2.5974e-05      5.8584e+05          356.55          13.247
v  TurbVisc            1.4958e-12         0.16883      0.00069499       0.0087931
v  total_pressure       4.048e+05      5.5532e+05      5.3163e+05      5.2784e+05


 TIME FOR THE TIME STEP              289:        0.73320E+02

===============================================================


 INSTANT    0.290000000E+03   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        -0.707210501E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441505E+00
Free inlet               13           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[Z]                                      0.11267E+02 
c  Pressure     0.37412E-01     493   0.38031E-02   0.22252E+00 0.36894E+03 
c  k            0.51838E-01      61   0.38905E-02   0.12934E-01 0.49629E+03 
c  epsilon      0.13490E+04      48   0.34022E-02   0.52081E+07 0.30651E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0003456                            11
a  epsilon         -0.6055                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3146          14.715         0.87778         0.10847
v  Velocity[Y]            -11.371          14.142         0.38274         0.26365
v  Velocity[Z]            -22.465          18.276         -0.3768     -0.00076438
v  ǁVelocityǁ          4.5865e-05          25.331          2.5005          2.3309
v  Pressure                -95754           55438           31632           27843
v  k                   7.0267e-08          4.5294        0.021151        0.013095
v  epsilon             2.5183e-05       5.838e+05          356.61          13.253
v  TurbVisc            1.5022e-12         0.17431      0.00069492       0.0087931
v  total_pressure      4.0425e+05      5.5544e+05      5.3163e+05      5.2784e+05


 TIME FOR THE TIME STEP              291:        0.58807E+02

===============================================================


 INSTANT    0.292000000E+03   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         0.304839658E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16778E+02 0.48785E+01
   Friction velocity        uet   :  0.80457E-02 0.34230E+01
   Friction velocity        uk    :  0.80429E-02 0.34282E+01
   Dimensionless distance   yplus :  0.77750E-04 0.11298E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5386
   Nb of faces within the viscous sub-layer     :      21126
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13582E+01     110   0.17506E+00   0.27314E+02 0.24576E+03 
c  Velocity[X]                                      0.83609E+01 
c  Velocity[Y]                                      0.88508E+01 
c  Velocity[Z]                                      0.10102E+02 
c  Pressure     0.38312E-01     501   0.36065E-02   0.22837E+00 0.40065E+03 
c  k            0.52117E-01      62   0.49815E-02   0.18481E-01 0.55389E+03 
c  epsilon      0.13496E+04      41   0.37697E-02   0.97803E+07 0.35967E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00033713                            13
a  epsilon        -0.60911                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7.488          14.882         0.87777         0.10845
v  Velocity[Y]            -11.152          12.408         0.38235         0.26356
v  Velocity[Z]            -21.812          19.972        -0.37711      -0.0008626
v  ǁVelocityǁ          4.5768e-05          25.253          2.5015          2.3313
v  Pressure                -96138           55382           31635           27845c  Velocity[Z]                                      0.11267E+02 
c  Pressure     0.37412E-01     493   0.38031E-02   0.22252E+00 0.36894E+03 
c  k            0.51838E-01      61   0.38905E-02   0.12934E-01 0.49629E+03 
c  epsilon      0.13490E+04      48   0.34022E-02   0.52081E+07 0.30651E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0003456                            11
a  epsilon         -0.6055                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3146          14.715         0.87778         0.10847
v  Velocity[Y]            -11.371          14.142         0.38274         0.26365
v  Velocity[Z]            -22.465          18.276         -0.3768     -0.00076438
v  ǁVelocityǁ          4.5865e-05          25.331          2.5005          2.3309
v  Pressure                -95754           55438           31632           27843
v  k                   7.0267e-08          4.5294        0.021151        0.013095
v  epsilon             2.5183e-05       5.838e+05          356.61          13.253
v  TurbVisc            1.5022e-12         0.17431      0.00069492       0.0087931
v  total_pressure      4.0425e+05      5.5544e+05      5.3163e+05      5.2784e+05


 TIME FOR THE TIME STEP              291:        0.67897E+02

===============================================================


 INSTANT    0.292000000E+03   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         0.304839658E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441591E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15   c  Velocity     0.13576E+01     110   0.17601E+00   0.26725E+02 0.24128E+03 
c  Velocity[X]                                      0.80511E+01 
c  Velocity[Y]                                      0.87415E+01 
c  Velocity[Z]                                      0.99325E+01 
c  Pressure     0.36737E-01     769   0.41094E-02   0.21953E+00 0.11370E+04 
c  k            0.52590E-01      63   0.34990E-02   0.11106E-01 0.58261E+03 
c  epsilon      0.13560E+04      41   0.51689E-02   0.12011E+08 0.40378E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00033483                            12
a  epsilon        -0.58618                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9497          14.745         0.87786         0.10837
v  Velocity[Y]            -10.985          12.394         0.38216         0.26378
v  Velocity[Z]            -22.287          19.987        -0.37708     -0.00069572
v  ǁVelocityǁ          4.6649e-05           25.22          2.5027          2.3316
v  Pressure                -96145           55319           31585           27807
v  k                   6.8976e-08          5.3527        0.021178        0.013106
v  epsilon               2.45e-05      5.8267e+05          356.77          13.282
v  TurbVisc            1.4983e-12         0.20436      0.00069525       0.0087932
v  total_pressure      4.0385e+05      5.5532e+05      5.3159e+05      5.2781e+05


 TIME FOR THE TIME STEP              293:        0.65528E+02

===============================================================


 INSTANT    0.294000000E+03   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         0.375804149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441484E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16391E+02 0.46992E+01
   Friction velocity        uet   :  0.11293E-01 0.34220E+01
   Friction velocity        uk    :  0.11289E-01 0.34244E+01
   Dimensionless distance   yplus :  0.78471E-04 0.10604E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5391
   Nb of faces within the viscous sub-layer     :      21105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13564E+01     109   0.17679E+00   0.26774E+02 0.24467E+03 
c  Velocity[X]                                      0.81922E+01 
c  Velocity[Y]                                      0.88630E+01 
c  Velocity[Z]                                      0.97193E+01 
c  Pressure     0.37238E-01     567   0.41757E-02   0.22392E+00 0.36932E+03 
c  k            0.52939E-01      63   0.31476E-02   0.91734E-02 0.50293E+03 
c  epsilon      0.13451E+04      42   0.46483E-02   0.73897E+07 0.35202E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00032392                            12
a  epsilon        -0.73437                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.4731          14.961         0.87824         0.10844
v  Velocity[Y]            -11.269          12.435         0.38187         0.26362
v  Velocity[Z]            -22.057       c  Velocity     0.13576E+01     110   0.17601E+00   0.26725E+02 0.24128E+03 
c  Velocity[X]                                      0.80511E+01 
c  Velocity[Y]                                      0.87415E+01 
c  Velocity[Z]                                      0.99325E+01 
c  Pressure     0.36737E-01     769   0.41094E-02   0.21953E+00 0.11370E+04 
c  k            0.52590E-01      63   0.34990E-02   0.11106E-01 0.58261E+03 
c  epsilon      0.13560E+04      41   0.51689E-02   0.12011E+08 0.40378E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00033483                            12
a  epsilon        -0.58618                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.9497          14.745         0.87786         0.10837
v  Velocity[Y]            -10.985          12.394         0.38216         0.26378
v  Velocity[Z]            -22.287          19.987        -0.37708     -0.00069572
v  ǁVelocityǁ          4.6649e-05           25.22          2.5027          2.3316
v  Pressure                -96145           55319           31585           27807
v  k                   6.8976e-08          5.3527        0.021178        0.013106
v  epsilon               2.45e-05      5.8267e+05          356.77          13.282
v  TurbVisc            1.4983e-12         0.20436      0.00069525       0.0087932
v  total_pressure      4.0385e+05      5.5532e+05      5.3159e+05      5.2781e+05


 TIME FOR THE TIME STEP              293:        0.69346E+02

===============================================================


 INSTANT    0.294000000E+03   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         0.375804149E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+01     111   0.17614E+00   0.26222E+02 0.24135E+03 
c  Velocity[X]                                      0.82289E+01 
c  Velocity[Y]                                      0.85950E+01 
c  Velocity[Z]                                      0.93978E+01 
c  Pressure     0.35129E-01     593   0.36572E-02   0.20910E+00 0.52275E+03 
c  k            0.53161E-01      61   0.39657E-02   0.99631E-02 0.41468E+03 
c  epsilon      0.13626E+04      39   0.53402E-02   0.43176E+07 0.24188E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00031536                            12
a  epsilon        -0.57815                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4491          14.425         0.87874         0.10858
v  Velocity[Y]            -10.953          12.315         0.38162         0.26352
v  Velocity[Z]            -21.593          18.092        -0.37769     -0.00073484
v  ǁVelocityǁ          4.5498e-05          25.278          2.5052          2.3324
v  Pressure                -96865           55368           31596           27816
v  k                   6.7932e-08          5.6165        0.021226        0.013114
v  epsilon              2.389e-05      5.8392e+05          357.49          13.304
v  TurbVisc            1.4951e-12         0.21369      0.00069583       0.0087932
v  total_pressure      4.0313e+05      5.5537e+05       5.316e+05      5.2782e+05


 TIME FOR THE TIME STEP              295:        0.59952E+02

===============================================================


 INSTANT    0.296000000E+03   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         0.114996895E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441513E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15218E+02 0.56167E+01
   Friction velocity        uet   :  0.12206E-01 0.34153E+01
   Friction velocity        uk    :  0.12202E-01 0.34093E+01
   Dimensionless distance   yplus :  0.77486E-04 0.11236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5392
   Nb of faces within the viscous sub-layer     :      21075
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13572E+01     110   0.17677E+00   0.26083E+02 0.24150E+03 
c  Velocity[X]                                      0.83774E+01 
c  Velocity[Y]                                      0.85222E+01 
c  Velocity[Z]                                      0.91835E+01 
c  Pressure     0.36849E-01     716   0.34369E-02   0.21959E+00 0.29536E+03 
c  k            0.53106E-01      60   0.34650E-02   0.11113E-01 0.57840E+03 
c  epsilon      0.13523E+04      40   0.46800E-02   0.93672E+07 0.34984E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00032922                            12
a  epsilon        -0.70369                            20


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3533          15.42   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+01     111   0.17614E+00   0.26222E+02 0.24135E+03 
c  Velocity[X]                                      0.82289E+01 
c  Velocity[Y]                                      0.85950E+01 
c  Velocity[Z]                                      0.93978E+01 
c  Pressure     0.35129E-01     593   0.36572E-02   0.20910E+00 0.52275E+03 
c  k            0.53161E-01      61   0.39657E-02   0.99631E-02 0.41468E+03 
c  epsilon      0.13626E+04      39   0.53402E-02   0.43176E+07 0.24188E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00031536                            12
a  epsilon        -0.57815                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4491          14.425         0.87874         0.10858
v  Velocity[Y]            -10.953          12.315         0.38162         0.26352
v  Velocity[Z]            -21.593          18.092        -0.37769     -0.00073484
v  ǁVelocityǁ          4.5498e-05          25.278          2.5052          2.3324
v  Pressure                -96865           55368           31596           27816
v  k                   6.7932e-08          5.6165        0.021226        0.013114
v  epsilon              2.389e-05      5.8392e+05          357.49          13.304
v  TurbVisc            1.4951e-12         0.21369      0.00069583       0.0087932
v  total_pressure      4.0313e+05      5.5537e+05       5.316e+05      5.2782e+05


 TIME FOR THE TIME STEP              295:        0.63346E+02

===============================================================


 INSTANT    0.296000000E+03   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.   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13560E+01     110   0.17489E+00   0.27694E+02 0.24247E+03 
c  Velocity[X]                                      0.83899E+01 
c  Velocity[Y]                                      0.85818E+01 
c  Velocity[Z]                                      0.10722E+02 
c  Pressure     0.35579E-01     682   0.34949E-02   0.21176E+00 0.26704E+03 
c  k            0.53130E-01      58   0.51019E-02   0.18447E-01 0.58456E+03 
c  epsilon      0.13651E+04      39   0.40417E-02   0.86298E+07 0.38442E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0004936                            13
a  epsilon         -16.023                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3991          15.004         0.88013         0.10848
v  Velocity[Y]            -10.675          12.368         0.38107         0.26373
v  Velocity[Z]            -20.437          18.948        -0.37794      -0.0007059
v  ǁVelocityǁ          4.5683e-05          23.555          2.5081          2.3331
v  Pressure                -97331           55341           31585           27806
v  k                   6.7025e-08          5.3436        0.021254        0.013114
v  epsilon             2.3364e-05      5.8264e+05             Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13574E+01     111   0.17614E+00   0.26222E+02 0.24135E+03 
c  Velocity[X]                                      0.82289E+01 
c  Velocity[Y]                                      0.85950E+01 
c  Velocity[Z]                                      0.93978E+01 
c  Pressure     0.35129E-01     593   0.36572E-02   0.20910E+00 0.52275E+03 
c  k            0.53161E-01      61   0.39657E-02   0.99631E-02 0.41468E+03 
c  epsilon      0.13626E+04      39   0.53402E-02   0.43176E+07 0.24188E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00031536                            12
a  epsilon        -0.57815                            18


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -6.4491          14.425         0.87874         0.10858
v  Velocity[Y]            -10.953          12.315         0.38162         0.26352
v  Velocity[Z]            -21.593          18.092        -0.37769     -0.00073484
v  ǁVelocityǁ          4.5498e-05          25.278          2.5052          2.3324
v  Pressure                -96865           55368           31596           27816
v  k                   6.7932e-08          5.6165        0.021226        0.013114
v  epsilon              2.389e-05      5.8392e+05          357.49          13.304
v  TurbVisc            1.4951e-12         0.21369      0.00069583       0.0087932
v  total_pressure      4.0313e+05      5.5537e+05       5.316e+05      5.2782e+05


 TIME FOR THE TIME STEP              295:        0.70234E+02

===============================================================


 INSTANT    0.296000000E+03   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         0.114996895E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441513E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15218   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13560E+01     110   0.17489E+00   0.27694E+02 0.24247E+03 
c  Velocity[X]                                      0.83899E+01 
c  Velocity[Y]                                      0.85818E+01 
c  Velocity[Z]                                      0.10722E+02 
c  Pressure     0.35579E-01     682   0.34949E-02   0.21176E+00 0.26704E+03 
c  k            0.53130E-01      58   0.51019E-02   0.18447E-01 0.58456E+03 
c  epsilon      0.13651E+04      39   0.40417E-02   0.86298E+07 0.38442E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0004936                            13
a  epsilon         -16.023                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.3991          15.004         0.88013         0.10848
v  Velocity[Y]            -10.675          12.368         0.38107         0.26373
v  Velocity[Z]            -20.437          18.948        -0.37794      -0.0007059
v  ǁVelocityǁ          4.5683e-05          23.555          2.5081          2.3331
v  Pressure                -97331           55341           31585           27806
v  k                   6.7025e-08          5.3436        0.021254        0.013114
v  epsilon             2.3364e-05      5.8264e+05          358.04          13.324
v  TurbVisc            1.4913e-12          0.2019      0.00069624        0.008793
v  total_pressure      4.0267e+05      5.5534e+05      5.3158e+05      5.2781e+05


 TIME FOR THE TIME STEP              297:        0.70597E+02

===============================================================


 INSTANT    0.298000000E+03   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Ma   Nb of faces within the viscous sub-layer     :      21060
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13553E+01     109   0.17702E+00   0.25575E+02 0.24075E+03 
c  Velocity[X]                                      0.81065E+01 
c  Velocity[Y]                                      0.83105E+01 
c  Velocity[Z]                                      0.91578E+01 
c  Pressure     0.32740E-01     587   0.31241E-02   0.19531E+00 0.35906E+03 
c  k            0.52047E-01      58   0.47308E-02   0.20657E-01 0.56121E+03 
c  epsilon      0.13650E+04      44   0.37629E-02   0.90779E+07 0.33649E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00030864                            12
a  epsilon         -0.7425                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.3753          14.861         0.88149         0.10859
v  Velocity[Y]            -10.932          12.337         0.38089         0.26361
v  Velocity[Z]            -20.608          18.529        -0.37775     -0.00072348
v  ǁVelocityǁ          4.6723e-05          23.981          2.5105          2.3343
v  Pressure                -97431           55393           31563           27792
v  k                    6.621e-08          4.3581        0.021279        0.013107
v  epsilon             2.2775e-05      5.8146e+05          359.18          13.314
v  TurbVisc            1.4976e-12         0.18393      0.00069669       0.0087927
v  total_pressure      4.0257e+05      5.5539e+05      5.3156e+05      5.2779e+05


 TIME FOR THE TIME STEP              299:        0.62863E+02

===============================================================


 INSTANT    0.300000000E+03   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         0.917569742E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.989441504E+00
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14933E+02 0.54304E+01
   Friction velocity        uet   :  0.14096E-01 0.34243E+01
   Friction velocity        uk    :  0.14074E-01 0.34221E+01
   Dimensionless distance   yplus :  0.78570E-04 0.11486E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5384
   Nb of faces within the viscous sub-layer     :      21057
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13552E+01     110   0.17785E+00   0.25808E+02 0.24109E+03 
c  Velocity[X]                                      0.80130E+01 
c  Velocity[Y]                                      0.88403E+01 
c  Velocity[Z]                                      0.89545E+01 
c  Pressure     0.34180E-01     582   0.32411E-02   0.20389E+00 0.32551E+03 
c  k            0.51843E-01      60   0.44239E-02   0.13358E-01 0.53074E+03 
c  epsilon      0.13559E+04      39   0.36060E-02   0.59810E+07 0.29656E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00030362                            11
a    Nb of faces within the viscous sub-layer     :      21060
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13553E+01     109   0.17702E+00   0.25575E+02 0.24075E+03 
c  Velocity[X]                                      0.81065E+01 
c  Velocity[Y]                                      0.83105E+01 
c  Velocity[Z]                                      0.91578E+01 
c  Pressure     0.32740E-01     587   0.31241E-02   0.19531E+00 0.35906E+03 
c  k            0.52047E-01      58   0.47308E-02   0.20657E-01 0.56121E+03 
c  epsilon      0.13650E+04      44   0.37629E-02   0.90779E+07 0.33649E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00030864                            12
a  epsilon         -0.7425                            19


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.3753          14.861         0.88149         0.10859
v  Velocity[Y]            -10.932          12.337         0.38089         0.26361
v  Velocity[Z]            -20.608          18.529        -0.37775     -0.00072348
v  ǁVelocityǁ          4.6723e-05          23.981          2.5105          2.3343
v  Pressure                -97431           55393           31563           27792
v  k                    6.621e-08          4.3581        0.021279        0.013107
v  epsilon             2.2775e-05      5.8146e+05          359.18          13.314
v  TurbVisc            1.4976e-12         0.18393      0.00069669       0.0087927
v  total_pressure      4.0257e+05      5.5539e+05      5.3156e+05      5.2779e+05


 TIME FOR THE TIME STEP              299:        0.71294E+02

===============================================================


 INSTANT    0.300000000E+03   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.78266E-04 0.10640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5396
   Nb of faces within the viscous sub-layer     :      21054
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14399E+01     134   0.16776E+00   0.48190E+04 0.14966E+04 
c  Velocity[X]                                      0.58063E+03 
c  Velocity[Y]                                      0.10584E+04 
c  Velocity[Z]                                      0.31800E+04 
c  Pressure     0.43980E-01    1470   0.27512E+00   0.25740E+00 0.31153E+06 
c  k            0.72175E-01     105   0.11982E-01   0.33675E+00 0.11603E+04 
c  epsilon      0.13771E+04      65   0.81834E-02   0.81860E+07 0.31638E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -0.3387                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1481          40.699          1.0235         0.17503
v  Velocity[Y]            -33.872          44.067         0.58234         0.42338
v  Velocity[Z]            -54.806          37.257        -0.38622      -0.0022439
v  ǁVelocityǁ          4.6223e-05          73.044          2.8411          3.4809
v  Pressure                -41622       1.974e+05      1.1696e+05      1.0582e+05
v  k                   6.6779e-08          3.5836          0.0215        0.015277
v  epsilon             2.2441e-05      5.8197e+05          360.17          13.761
v  TurbVisc             1.516e-12         0.16883      0.00069706       0.0087928
v  total_pressure      4.5838e+05       6.974e+05      6.1696e+05      6.0582e+05


 TIME FOR THE TIME STEP              301:        0.84849E+02

===============================================================


 INSTANT    0.302000000E+03   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         0.700374192E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444449E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71979E+02 0.47240E+01
   Friction velocity        uet   :  0.27079E-01 0.49472E+01
   Friction velocity        uk    :  0.26713E-01 0.36607E+01
   Dimensionless distance   yplus :  0.78088E-04 0.15917E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6825
   Nb of faces within the viscous sub-layer     :      18813
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30831E+01     150   0.16397E+00   0.21623E+04 0.17216E+04 
c  Velocity[X]                                      0.46302E+03 
c  Velocity[Y]                                      0.65384E+03 
c  Velocity[Z]                                      0.10455E+04 
c  Pressure     0.17526E+00    1236   0.13191E+00   0.74019E+00 0.26536E+06 
c  k            0.88372E-01     101   0.23103E-01   0.14066E+01 0.49977E+04 
c  epsilon      0.34775E+04      61   0.64928E-01   0.25070E+10 0.39697E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to    Dimensionless distance   yplus :  0.78266E-04 0.10640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5396
   Nb of faces within the viscous sub-layer     :      21054
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14399E+01     134   0.16776E+00   0.48190E+04 0.14966E+04 
c  Velocity[X]                                      0.58063E+03 
c  Velocity[Y]                                      0.10584E+04 
c  Velocity[Z]                                      0.31800E+04 
c  Pressure     0.43980E-01    1470   0.27512E+00   0.25740E+00 0.31153E+06 
c  k            0.72175E-01     105   0.11982E-01   0.33675E+00 0.11603E+04 
c  epsilon      0.13771E+04      65   0.81834E-02   0.81860E+07 0.31638E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -0.3387                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.1481          40.699          1.0235         0.17503
v  Velocity[Y]            -33.872          44.067         0.58234         0.42338
v  Velocity[Z]            -54.806          37.257        -0.38622      -0.0022439
v  ǁVelocityǁ          4.6223e-05          73.044          2.8411          3.4809
v  Pressure                -41622       1.974e+05      1.1696e+05      1.0582e+05
v  k                   6.6779e-08          3.5836          0.0215        0.015277
v  epsilon             2.2441e-05      5.8197e+05          360.17          13.761
v  TurbVisc             1.516e-12         0.16883      0.00069706       0.0087928
v  total_pressure      4.5838e+05       6.974e+05      6.1696e+05      6.0582e+05


 TIME FOR THE TIME STEP              301:        0.10493E+03

===============================================================


 INSTANT    0.302000   Friction velocity        uet   :  0.10058E-01 0.51775E+01
   Friction velocity        uk    :  0.10056E-01 0.37795E+01
   Dimensionless distance   yplus :  0.79833E-04 0.17501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6662
   Nb of faces within the viscous sub-layer     :      18802
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28147E+01     143   0.15865E+00   0.10383E+04 0.11781E+04 
c  Velocity[X]                                      0.25500E+03 
c  Velocity[Y]                                      0.38928E+03 
c  Velocity[Z]                                      0.39402E+03 
c  Pressure     0.14855E+00    1058   0.39748E-01   0.65061E+00 0.43966E+05 
c  k            0.84159E-01      93   0.31641E-01   0.67363E+00 0.34110E+04 
c  epsilon      0.24492E+04      55   0.11433E+00   0.20639E+10 0.68079E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1483e-05                             2
a  epsilon         -1.3395                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.669           29.91          1.1075         0.17582
v  Velocity[Y]            -25.452          38.641         0.58926          0.4168
v  Velocity[Z]            -58.802          32.668        -0.43099     -0.00082133
v  ǁVelocityǁ          4.9588e-05          66.645          3.0323          3.4694
v  Pressure           -1.1585e+05      1.1751e+05           75670           64263
v  k                   6.9123e-08          3.7747        0.025211        0.019443
v  epsilon             2.3107e-05       9.758e+05          466.79          18.476
v  TurbVisc            1.5371e-12         0.21596      0.00079491        0.011301
v  total_pressure      3.8415e+05      6.1751e+05      5.7567e+05      5.6426e+05


 TIME FOR THE TIME STEP              303:        0.87913E+02

===============================================================


 INSTANT    0.304000000E+03   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         0.211510162E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94475E+02 0.48517E+01
   Friction velocity        uet   :  0.44040E-02 0.48417E+01
   Friction velocity        uk    :  0.44037E-02 0.39355E+01
   Dimensionless distance   yplus :  0.80798E-04 0.16272E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6765
   Nb of faces within the viscous sub-layer     :      18788
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28646E+01     138   0.16036E+00   0.83184E+03 0.11446E+04 
c  Velocity[X]                                      0.21977E+03 
c  Velocity[Y]                                      0.33330E+03 
c  Velocity[Z]                                      0.27877E+03 
c  Pressure     0.13756E+00    1295   0.30529E-01   0.59831E+00 0.19039E+05 
c  k            0.81309E-01      90   0.12569E-01   0.37360E+00 0.36636E+04 
c  epsilon      0.21521E+04      52   0.24916E-01   0.31986E+10 0.86975E+05 
-------------------------------------------------------   Friction velocity        uet   :  0.10058E-01 0.51775E+01
   Friction velocity        uk    :  0.10056E-01 0.37795E+01
   Dimensionless distance   yplus :  0.79833E-04 0.17501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6662
   Nb of faces within the viscous sub-layer     :      18802
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28147E+01     143   0.15865E+00   0.10383E+04 0.11781E+04 
c  Velocity[X]                                      0.25500E+03 
c  Velocity[Y]                                      0.38928E+03 
c  Velocity[Z]                                      0.39402E+03 
c  Pressure     0.14855E+00    1058   0.39748E-01   0.65061E+00 0.43966E+05 
c  k            0.84159E-01      93   0.31641E-01   0.67363E+00 0.34110E+04 
c  epsilon      0.24492E+04      55   0.11433E+00   0.20639E+10 0.68079E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1483e-05                             2
a  epsilon         -1.3395                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.669           29.91          1.1075         0.17582
v  Velocity[Y]            -25.452          38.641         0.58926          0.4168
v  Velocity[Z]            -58.802          32.668        -0.43099     -0.00082133
v  ǁVelocityǁ          4.9588e-05          66.645          3.0323          3.4694
v  Pressure           -1.1585e+05      1.1751e+05           75670           64263
v  k                   6.9123e-08          3.7747        0.025211        0.019443
v  epsilon             2.3107e-05       9.758e+05          466.79          18.476
v  TurbVisc            1.5371e-12         0.21596      0.00079491        0.011301
v  total_pressure      3.8415e+05      6.1751e+05                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75485E+02 0.50851E+01
   Friction velocity        uet   :  0.82531E-02 0.41229E+01
   Friction velocity        uk    :  0.82524E-02 0.41069E+01
   Dimensionless distance   yplus :  0.82104E-04 0.15686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6755
   Nb of faces within the viscous sub-layer     :      18892
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29309E+01     135   0.16135E+00   0.59795E+03 0.96321E+03 
c  Velocity[X]                                      0.15827E+03 
c  Velocity[Y]                                      0.19950E+03 
c  Velocity[Z]                                      0.24018E+03 
c  Pressure     0.15900E+00    1007   0.31321E-01   0.66465E+00 0.67577E+04 
c  k            0.80972E-01      87   0.83759E-02   0.19599E+00 0.24771E+04 
c  epsilon      0.21361E+04      53   0.19158E-01   0.12312E+10 0.50792E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7691e-06                             3
a  epsilon        -0.68571                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8287          36.091          1.1616         0.17625
v  Velocity[Y]            -28.877          23.825         0.57027         0.41668
v  Velocity[Z]            -65.404          41.095        -0.45904     -0.00041853
v  ǁVelocityǁ           5.287e-05          74.769          3.1725          3.5054
v  Pressure           -1.2684e+05      1.2063e+05           75343           64981
v  k                   7.0438e-08          4.2592        0.026545        0.020479
v  epsilon             2.4519e-05      9.8681e+05          548.99          18.754
v  TurbVisc            1.5763e-12         0.21627      0.00081504        0.012368
v  total_pressure      3.7316e+05      6.2063e+05      5.7534e+05      5.6498e+05


 TIME FOR THE TIME STEP              305:        0.85403E+02

===============================================================


 INSTANT    0.306000000E+03   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         0.469227169E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83141E+02 0.52625E+01
   Friction velocity        uet   :  0.12002E-01 0.45324E+01
   Friction velocity        uk    :  0.11999E-01 0.42614E+01
   Dimensionless distance   yplus :  0.83188E-04 0.15641E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6849
   Nb of faces within the viscous sub-layer     :      18911
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29937E+01     134   0.17127E+00   0.63390E+03 0.99450E+03 
c  Velocity[X]                                      0.15534E+03 
c  Velocity[Y]                                      0.16511E+03 
c  Velocity[Z]                                      0.31344E+03 
c  Pressure     0.14894E+00     807   0.24777E-01   0.59460E+00 0.47070E+04 
c  k            0.82035E-0                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75485E+02 0.50851E+01
   Friction velocity        uet   :  0.82531E-02 0.41229E+01
   Friction velocity        uk    :  0.82524E-02 0.41069E+01
   Dimensionless distance   yplus :  0.82104E-04 0.15686E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6755
   Nb of faces within the viscous sub-layer     :      18892
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29309E+01     135   0.16135E+00   0.59795E+03 0.96321E+03 
c  Velocity[X]                                      0.15827E+03 
c  Velocity[Y]                                      0.19950E+03 
c  Velocity[Z]                                      0.24018E+03 
c  Pressure     0.15900E+00    1007   0.31321E-01   0.66465E+00 0.67577E+04 
c  k            0.80972E-01      87   0.83759E-02   0.19599E+00 0.24771E+04 
c  epsilon      0.21361E+04      53   0.19158E-01   0.12312E+10 0.50792E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7691e-06                             3
a  epsilon        -0.68571                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.8287          36.091          1.1616         0.17625
v  Velocity[Y]            -28.877          23.825         0.57027         0.41668
v  Velocity[Z]            -65.404          41.095        -0.45904     -0.00041853
v  ǁVelocityǁ           5.287e-05          74.769          3.1725          3.5054
v  Pressure           -1.2684e+05      1.2063e+05           75343           64981
v  k                   7.0438e-08          4.2592        0.026545        0.020479
v  epsilon             2.4519e-05      9.8681e+05          548.99    ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.73303E+02 0.54264E+01
   Friction velocity        uet   :  0.15277E-01 0.44101E+01
   Friction velocity        uk    :  0.15272E-01 0.43895E+01
   Dimensionless distance   yplus :  0.84605E-04 0.15761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6909
   Nb of faces within the viscous sub-layer     :      18897
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30402E+01     132   0.16770E+00   0.46598E+03 0.81607E+03 
c  Velocity[X]                                      0.11460E+03 
c  Velocity[Y]                                      0.14765E+03 
c  Velocity[Z]                                      0.20374E+03 
c  Pressure     0.14263E+00     995   0.23133E-01   0.57143E+00 0.21426E+04 
c  k            0.83216E-01      82   0.75509E-02   0.16358E+00 0.30588E+04 
c  epsilon      0.23860E+04      50   0.12639E-01   0.31549E+10 0.76354E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.3881e-05                             5
a  epsilon         -5.3327                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0647          38.428           1.204         0.17471
v  Velocity[Y]            -22.821          23.129         0.55434         0.41715
v  Velocity[Z]            -47.906           43.45         -0.4791      0.00020641
v  ǁVelocityǁ          5.4902e-05          61.414          3.3016          3.5337
v  Pressure            -1.349e+05       1.218e+05           75327           65375
v  k                   3.8265e-08           5.262        0.028078        0.021126
v  epsilon             2.6333e-05      1.8946e+06          646.43          19.537
v  TurbVisc            1.6634e-12          0.2163      0.00083947        0.012991
v  total_pressure       3.651e+05       6.218e+05      5.7533e+05      5.6537e+05


 TIME FOR THE TIME STEP              307:        0.87143E+02

===============================================================


 INSTANT    0.308000000E+03   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         0.525784409E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58538E+02 0.54882E+01
   Friction velocity        uet   :  0.18483E-01 0.45270E+01
   Friction velocity        uk    :  0.18477E-01 0.44770E+01
   Dimensionless distance   yplus :  0.84716E-04 0.14487E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7025
   Nb of faces within the viscous sub-layer     :      18766
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30825E+01     129   0.17411E+00   0.40103E+03 0.75837E+03 
c  Velocity[X]                                      0.10719E+03 
c  Velocity[Y]                                      0.13132E+03 
c  Velocity[Z]          ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.73303E+02 0.54264E+01
   Friction velocity        uet   :  0.15277E-01 0.44101E+01
   Friction velocity        uk    :  0.15272E-01 0.43895E+01
   Dimensionless distance   yplus :  0.84605E-04 0.15761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6909
   Nb of faces within the viscous sub-layer     :      18897
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30402E+01     132   0.16770E+00   0.46598E+03 0.81607E+03 
c  Velocity[X]                                      0.11460E+03 
c  Velocity[Y]                                      0.14765E+03 
c  Velocity[Z]                                      0.20374E+03 
c  Pressure     0.14263E+00     995   0.23133E-01   0.57143E+00 0.21426E+04 
c  k            0.83216E-01      82   0.75509E-02   0.16358E+00 0.30588E+04 
c  epsilon      0.23860E+04      50   0.12639E-01   0.31549E+10 0.76354E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.3881e-05                             5
a  epsilon         -5.3327                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -7.0647          38.428           1.204         0.17471
v  Velocity[Y]            -22.821          23.129         0.55434         0.41715
v  Velocity[Z]            -47.906           43.45         -0.4791      0.00020641
v  ǁVelocityǁ          5.4902e-05          61.414          3.3016          3.5337
v  Pressure            -1.349e+05   Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40169E+02 0.55479E+01
   Friction velocity        uet   :  0.23013E-01 0.45058E+01
   Friction velocity        uk    :  0.23005E-01 0.45406E+01
   Dimensionless distance   yplus :  0.84971E-04 0.13181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7099
   Nb of faces within the viscous sub-layer     :      18653
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31122E+01     128   0.17776E+00   0.32872E+03 0.70189E+03 
c  Velocity[X]                                      0.84292E+02 
c  Velocity[Y]                                      0.12025E+03 
c  Velocity[Z]                                      0.12418E+03 
c  Pressure     0.14340E+00     826   0.15683E-01   0.55604E+00 0.21679E+04 
c  k            0.85699E-01      79   0.83427E-02   0.16811E+00 0.36351E+04 
c  epsilon      0.27624E+04      50   0.14968E-01   0.94268E+10 0.13142E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.4344e-05                             4
a  epsilon        -0.46013                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.4796          25.476          1.2447         0.17449
v  Velocity[Y]            -19.111           21.91         0.55338         0.41645
v  Velocity[Z]            -37.141          35.438        -0.49289       0.0002815
v  ǁVelocityǁ          5.7385e-05          45.039          3.4308           3.561
v  Pressure           -1.4512e+05      1.2181e+05           74622           65092
v  k                   6.9848e-08          7.9988        0.030058        0.021555
v  epsilon             2.8724e-05      4.0639e+06          750.84          20.504
v  TurbVisc            1.7996e-12          0.2163      0.00086207        0.013341
v  total_pressure      3.5488e+05      6.2181e+05      5.7462e+05      5.6509e+05


 TIME FOR THE TIME STEP              309:        0.77625E+02

===============================================================


 INSTANT    0.310000000E+03   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         0.186850127E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39551E+02 0.71378E+01
   Friction velocity        uet   :  0.20795E-01 0.45623E+01
   Friction velocity        uk    :  0.20789E-01 0.45468E+01
   Dimensionless distance   yplus :  0.86420E-04 0.13127E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7202
   Nb of faces within the viscous sub-layer     :      18474
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31337E+01     12Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40169E+02 0.55479E+01
   Friction velocity        uet   :  0.23013E-01 0.45058E+01
   Friction velocity        uk    :  0.23005E-01 0.45406E+01
   Dimensionless distance   yplus :  0.84971E-04 0.13181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7099
   Nb of faces within the viscous sub-layer     :      18653
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31122E+01     128   0.17776E+00   0.32872E+03 0.70189E+03 
c  Velocity[X]                                      0.84292E+02 
c  Velocity[Y]                                      0.12025E+03 
c  Velocity[Z]                                      0.12418E+03 
c  Pressure     0.14340E+00     826   0.15683E-01   0.55604E+00 0.21679E+04 
c  k            0.85699E-01      79   0.83427E-02   0.16811E+00 0.36351E+04 
c  epsilon      0.27624E+04      50   0.14968E-01   0.94268E+10 0.13142E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.4344e-05                             4
a  epsilon        -0.46013                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.4796          25.476          1.2447         0.17449
v  Velocity[Y]            -19.111           21.91         0.55338         0.41645
v  VelocitFree outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47047E+02 0.72113E+01
   Friction velocity        uet   :  0.11649E-01 0.48060E+01
   Friction velocity        uk    :  0.31129E-01 0.46190E+01
   Dimensionless distance   yplus :  0.87247E-04 0.13691E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7327
   Nb of faces within the viscous sub-layer     :      18235
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31557E+01     128   0.17506E+00   0.27247E+03 0.64090E+03 
c  Velocity[X]                                      0.72836E+02 
c  Velocity[Y]                                      0.10533E+03 
c  Velocity[Z]                                      0.94309E+02 
c  Pressure     0.13285E+00     698   0.13918E-01   0.50600E+00 0.27379E+04 
c  k            0.92583E-01      76   0.58223E-02   0.20484E+00 0.29711E+04 
c  epsilon      0.30817E+04      49   0.11726E-01   0.28267E+10 0.49464E+05 
------------------------------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40169E+02 0.55479E+01
   Friction velocity        uet   :  0.23013E-01 0.45058E+01
   Friction velocity        uk    :  0.23005E-01 0.45406E+01
   Dimensionless distance   yplus :  0.84971E-04 0.13181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7099
   Nb of faces within the viscous sub-layer     :      18653
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31122E+01     128   0.17776E+00   0.32872E+03 0.70189E+03 
c  Velocity[X]                                      0.84292E+02 
c  Velocity[Y]                                      0.12025E+03 
c  Velocity[Z]                                      0.12418E+03 
c  Pressure     0.14340E+00     826   0.15683E-01   0.55604E+00 0.21679E+04 
c  k            0.85699E-01      79   0.83427E-02   0.16811E+00 0.36351E+04 
c  epsilon      0.27624E+04      50   0.14968E-01   0.94268E+10 0.13142E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.4344e-05                             4
a  epsilon        -0.46013                             8


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.4796          25.476          1.2447         0.17449
v  Velocity[Y]            -19.111           21.91         0.55338         0.41645
v  Velocity[Z]            -37.141          35.438        -0.49289       0.0002815
v  ǁVelocityǁ          5.7385e-05          45.039          3.4308           3.561
v  Pressure           -1.4512e+05      1.2181e+05           74622           65092
v  k                   6.9848e-08          7.9988        0.030058        0.021555
v  epsilon             2.8724e-05      4.0639e+06          750.84          20.504
v  TurbVisc            1.7996e-12          0.2163      0.00086207        0.013341
v  total_pressure      3.5488e+05      6.2181e+05      5.7462e+05      5.6509e+05


 TIME FOR THE TIME STEP              309:        0.77505E+02

===============================================================


 INSTANT    0.310000000E+03   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARYFree outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47047E+02 0.72113E+01
   Friction velocity        uet   :  0.11649E-01 0.48060E+01
   Friction velocity        uk    :  0.31129E-01 0.46190E+01
   Dimensionless distance   yplus :  0.87247E-04 0.13691E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7327
   Nb of faces within the viscous sub-layer     :      18235
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31557E+01     128   0.17506E+00   0.27247E+03 0.64090E+03 
c  Velocity[X]                                      0.72836E+02 
c  Velocity[Y]                                      0.10533E+03 
c  Velocity[Z]                                      0.94309E+02 
c  Pressure     0.13285E+00     698   0.13918E-01   0.50600E+00 0.27379E+04 
c  k            0.92583E-01      76   0.58223E-02   0.20484E+00 0.29711E+04 
c  epsilon      0.30817E+04      49   0.11726E-01   0.28267E+10 0.49464E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.4759e-05                             6
a  epsilon        -0.25106                            10


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  -------------Smooth wall               5       41000        -0.123596764E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60102E+02 0.62459E+01
   Friction velocity        uet   :  0.15812E-01 0.48756E+01
   Friction velocity        uk    :  0.15810E-01 0.46401E+01
   Dimensionless distance   yplus :  0.90836E-04 0.14874E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7515
   Nb of faces within the viscous sub-layer     :      17761
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31974E+01     127   0.17721E+00   0.23724E+03 0.59684E+03 
c  Velocity[X]                                      0.63436E+02 
c  Velocity[Y]                                      0.84025E+02 
c  Velocity[Z]                                      0.89779E+02 
c  Pressure     0.12330E+00     824   0.12873E-01   0.46367E+00 0.20535E+04 
c  k            0.88458E-01      74   0.77898E-02   0.22520E+00 0.37536E+04 
c  epsilon      0.32220E+04      49   0.13050E-01   0.61400E+10 0.93369E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012013                             6
a  epsilon        -0.55436                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.1772          25.193          1.3044         0.17266
v  Velocity[Y]            -19.052          20.799         0.57582         0.41701
v  Velocity[Z]            -37.714          33.248        -0.50849     -0.00015429
v  ǁVelocityǁ          7.0568e-05          45.356          3.6551          3.6059
v  Pressure           -1.6567e+05      1.2732e+05           75372           65830
v  k                   1.4869e-08           7.033        0.034632        0.022122
v  epsilon             1.4273e-05      2.9772e+06          966.14          22.612
v  TurbVisc            2.2472e-12          0.2163      0.00090299        0.013639
v  total_pressure      3.3433e+05      6.2732e+05      5.7537e+05      5.6583e+05


 TIME FOR THE TIME STEP              313:        0.65252E+02

===============================================================


 INSTANT    0.314000000E+03   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        -0.243037477E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40352E+02 0.62435E+01
   Friction velocity        uet   :  0.14351E-01 0.48578E+01
   Friction velocity        uk    :  0.14349E-01 0.46354E+01
   Dimensionless distance   yplus :  0.95109E-04 0.13183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7588
   Nb of faces within the viscous sub-layer     :      17517
   Total number of wall faces                   :      41000
--------------Smooth wall               5       41000        -0.123596764E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60102E+02 0.62459E+01
   Friction velocity        uet   :  0.15812E-01 0.48756E+01
   Friction velocity        uk    :  0.15810E-01 0.46401E+01
   Dimensionless distance   yplus :  0.90836E-04 0.14874E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7515
   Nb of faces within the viscous sub-layer     :      17761
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31974E+01     127   0.17721E+00   0.23724E+03 0.59684E+03 
c  Velocity[X]                                      0.63436E+02 
c  Velocity[Y]                                      0.84025E+02 
c  Velocity[Z]                                      0.89779E+02 
c  Pressure     0.12330E+00     824   0.12873E-01   0.46367E+00 0.20535E+04 
c  k            0.88458E-01      74   0.77898E-02   0.22520E+00 0.37536E+04 
c  epsilon      0.32220E+04      49   0.13050E-01   0.61400E+10 0.93369E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012013                             6
a  epsilon        -0.55436                             7


  ** Computed fieldBoundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.202508419E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45302E+02 0.63012E+01
   Friction velocity        uet   :  0.23414E-01 0.49094E+01
   Friction velocity        uk    :  0.23404E-01 0.46802E+01
   Dimensionless distance   yplus :  0.99182E-04 0.13736E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7699
   Nb of faces within the viscous sub-layer     :      17302
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32228E+01     123   0.17782E+00   0.20230E+03 0.53900E+03 
c  Velocity[X]                                      0.57672E+02 
c  Velocity[YSmooth wall               5       41000        -0.123596764E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60102E+02 0.62459E+01
   Friction velocity        uet   :  0.15812E-01 0.48756E+01
   Friction velocity        uk    :  0.15810E-01 0.46401E+01
   Dimensionless distance   yplus :  0.90836E-04 0.14874E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7515
   Nb of faces within the viscous sub-layer     :      17761
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31974E+01     127   0.17721E+00   0.23724E+03 0.59684E+03 
c  Velocity[X]                                      0.63436E+02 
c  Velocity[Y]                                      0.84025E+02 
c  Velocity[Z]                                      0.89779E+02 
c  Pressure     0.12330E+00     824   0.12873E-01   0.46367E+00 0.20535E+04 
c  k            0.88458E-01      74   0.77898E-02   0.22520E+00 0.37536E+04 
c  epsilon      0.32220E+04      49   0.13050E-01   0.61400E+10 0.93369E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012013                             6
a  epsilon        -0.55436                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -8.1772          25.193          1.3044         0.17266
v  Velocity[Y]            -19.052          20.799         0.57582         0.41701
v  Velocity[Z]            -37.714          33.248        -0.50849     -0.00015429
v  ǁVelocityǁ          7.0568e-05          45.356          3.6551          3.6059
v  Pressure           -1.6567e+05      1.2732e+05           75372           65830
v  k                   1.4869e-08           7.033        0.034632        0.022122
v  epsilon             1.4273e-05      2.9772e+06          966.14          22.612
v  TurbVisc            2.2472e-12          0.2163      0.00Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.202508419E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45302E+02 0.63012E+01
   Friction velocity        uet   :  0.23414E-01 0.49094E+01
   Friction velocity        uk    :  0.23404E-01 0.46802E+01
   Dimensionless distance   yplus :  0.99182E-04 0.13736E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7699
   Nb of faces within the viscous sub-layer     :      17302
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32228E+01     123   0.17782E+00   0.20230E+03 0.53900E+03 
c  Velocity[X]                                      0.57672E+02 
c  Velocity[Y]                                      0.66314E+02 
c  Velocity[Z]                                      0.78319E+02 
c  Pressure     0.12059E+00     770   0.12255E-01   0.44652E+00 0.23046E+04 
c  k            0.88031E-01      72   0.50632E-02   0.23022E+00 0.35686E+04 
c  epsilon      0.34083E+04      50   0.11764E-01   0.50709E+10 0.63044E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  --------
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.275197410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50678E+02 0.63476E+01
   Friction velocity        uet   :  0.31851E-01 0.49693E+01
   Friction velocity        uk    :  0.31832E-01 0.47126E+01
   Dimensionless distance   yplus :  0.10785E-03 0.14175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7833
   Nb of faces within the viscous sub-layer     :      16952
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32518E+01     123   0.18174E+00   0.17733E+03 0.50252E+03 
c  Velocity[X]                                      0.49814E+02 
c  Velocity[Y]                                      0.57128E+02 
c  Velocity[Z]                                      0.70392E+02 
c  Pressure     0.11984E+00     969   0.11095E-01   0.43766E+00 0.35943E+04 
c  k            0.91510E-01      70   0.70453E-02   0.31715E+00 0.29541E+04 
c  epsilon      0.36040E+04      53   0.78064E-02   0.16700E+10 0.72643E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.7089e-05                             2
a  epsilon        -0.02525                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.198           24.47          1.3567         0.17201
v  Velocity[Y]            -19.254          20.706         0.59189         0.41762
v  Velocity[Z]            -40.463          35.165        -0.53435     -0.00051006
v  ǁVelocityǁ          0.00010079          45.622          3.8264          3.6397
v  Pressure           -1.8283e+05      1.2913e+05           74806           65625
v  k                   8.0969e-08          5.9542        0.039332        0.022575
v  epsilon              5.157e-05      2.3768e+06          1203.2          24.599
v  TurbVisc            2.8224e-12          0.2163      0.00093788        0.013725
v  total_pressure      3.1717e+05      6.2913e+05      5.7481e+05      5.6562e+05


 TIME FOR THE TIME STEP              317:        0.87766E+02

===============================================================


 INSTANT    0.318000000E+03   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.241089728E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54215E+02 0.63528E+01
   Friction velocity        uet   :  0.27101E-01 0.49193E+01
   Friction velocity        uk    :  0.27079E-01 
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.275197410E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50678E+02 0.63476E+01
   Friction velocity        uet   :  0.31851E-01 0.49693E+01
   Friction velocity        uk    :  0.31832E-01 0.47126E+01
   Dimensionless distance   yplus :  0.10785E-03 0.14175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7833
   Nb of faces within the viscous sub-layer     :      16952
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32518E+01     123   0.18174E+00   0.17733E+03 0.50252E+03 
c  Velocity[X]                                      0.49814E+02 
c  Velocity[Y]                                      0.57128E+02 
c  Velocity[Z]                                      0.70392E+02 
c  Pressure     0.11984E+00     969   0.11095E-01   0.43766E+00 0.35943E+04 
c  k            0.91510E-01      70   0.70453E-02   0.31715E+00 0.29541E+04 
c  epsilon      0.36040E+04      53   0.78064E-02   0.16700E+10 0.72643E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippin===============================================================


 INSTANT    0.319000000E+03   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         0.399558129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49239E+02 0.63465E+01
   Friction velocity        uet   :  0.14126E-01 0.48914E+01
   Friction velocity        uk    :  0.16585E-01 0.47107E+01
   Dimensionless distance   yplus :  0.11721E-03 0.14059E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7933
   Nb of faces within the viscous sub-layer     :      16683
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32706E+01     122   0.18222E+00   0.17976E+03 0.49492E+03 
c  Velocity[X]                                      0.51460E+02 
c  Velocity[Y]                                      0.51953E+02 
c  Velocity[Z]                                      0.76345E+02 
c  Pressure     0.12581E+00     804   0.93581E-02   0.45220E+00 0.42527E+04 
c  k            0.11057E+00      71   0.14097E-01   0.12590E+01 0.30622E+04 
c  epsilon      0.38008E+04      50   0.12695E-01   0.24926E+10 0.35789E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.2582e-05                             2
a  epsilon       -0.029888                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.703          24.701          1.3841         0.17217
v  Velocity[Y]            -19.949          20.436          0.5935         0.41679
v  Velocity[Z]            -39.925          36.912        -0.55065     -0.00091198
v  ǁVelocityǁ          0.00011303          46.757           3.889          3.6526
v  Pressure           -1.8881e+05      1.2909e+05           74420           65474
v  k                   9.5508e-08          10.899        0.041483        0.022943
v  epsilon             5.9978e-05      2.3729e+06          1323.7          25.774
v  TurbVisc            3.1361e-12          0.2163      0.00095607        0.013751
v  total_pressure      3.1119e+05      6.2909e+05      5.7442e+05      5.6547e+05


 TIME FOR THE TIME STEP              319:        0.82422E+02

===============================================================


 INSTANT    0.320000000E+03   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.155153529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------===============================================================


 INSTANT    0.319000000E+03   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         0.399558129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49239E+02 0.63465E+01
   Friction velocity        uet   :  0.14126E-01 0.48914E+01
   Friction velocity        uk    :  0.16585E-01 0.47107E+01
   Dimensionless distance   yplus :  0.11721E-03 0.14059E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7933
   Nb of faces within the viscous sub-layer     :      16683
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32706E+01     122   0.18222E+00   0.17976E+03 0.49492E+03 
c  Velocity[X]                                      0.51460E+02 
c  Velocity[Y]                                      0.51953E+02 
c  Velocity[Z]                                      0.76345E+02 
c  Pressure     0.12581E+00     804   0.93581E-02   0.45220E+00 0.42527E+04 
c  k            0.11057E+00      71   0.14097E-01   0.12590E+01 0.30622E+04 
c  epsilon      0.38008E+04 v  total_pressure      3.0792e+05      6.2917e+05      5.7427e+05      5.6541e+05


 TIME FOR THE TIME STEP              320:        0.71429E+02

===============================================================


 INSTANT    0.321000000E+03   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        -0.123813550E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58341E+02 0.63696E+01
   Friction velocity        uet   :  0.16333E-01 0.49193E+01
   Friction velocity        uk    :  0.16037E-01 0.47279E+01
   Dimensionless distance   yplus :  0.12362E-03 0.16635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8026
   Nb of faces within the viscous sub-layer     :      16498
   Total number of wall faces                   :      4===============================================================


 INSTANT    0.319000000E+03   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         0.399558129E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49239E+02 0.63465E+01
   Friction velocity        uet   :  0.14126E-01 0.48914E+01
   Friction velocity        uk    :  0.16585E-01 0.47107E+01
   Dimensionless distance   yplus :  0.11721E-03 0.14059E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7933
   Nb of faces within the viscous sub-layer     :      16683
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32706E+01     122   0.18222E+00   0.17976E+03 0.49492E+03 
c  Velocity[X]                                      0.51460E+02 
c  Velocity[Y]                                      0.51953E+02 
c  Velocity[Z]                                      0.76345E+02 
c  Pressure     0.12581E+00     804   0.93581E-02   0.45220E+00 0.42527E+04 
c  k            0.11057E+00      71   0.14097E-01   0.12590E+01 0.30622E+04 
c  epsilon      0.38008E+04      50   0.12695E-01   0.24926E+10 0.35789E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.2582e-05                             2
a  epsilon       -0.029888                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.703          24.701          1.3841         0.17217
v  Velocity[Y]            -19.949          20.436          0.5935      v  total_pressure      3.0792e+05      6.2917e+05      5.7427e+05      5.6541e+05


 TIME FOR THE TIME STEP              320:        0.73507E+02

===============================================================


 INSTANT    0.321000000E+03   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        -0.123813550E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58341E+02 0.63696E+01
   Friction velocity        uet   :  0.16333E-01 0.49193E+01
   Friction velocity        uk    :  0.16037E-01 0.47279E+01
   Dimensionless distance   yplus :  0.12362E-03 0.16635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8026
   Nb of faces within the viscous sub-layer     :      16498
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32896E+01     121   0.18174E+00   0.18816E+03 0.49690E+03 
c  Velocity[X]                                      0.52822E+02 
c  Velocity[Y]                                      0.52449E+02 
c  Velocity[Z]                                      0.82889E+02 
c  Pressure     0.v  epsilon              8.086e-05      2.3952e+06          1428.3          27.414
v  TurbVisc            3.7988e-12         0.32756      0.00098693        0.013816
v  total_pressure      3.0296e+05      6.2897e+05      5.7411e+05      5.6538e+05


 TIME FOR THE TIME STEP              322:        0.75897E+02

===============================================================


 INSTANT    0.323000000E+03   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        -0.214768325E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46044E+02 0.64061E+01
   Friction velocity        uet   :  0.23959E-01 0.50100E+01
   Friction velocity        uk    :  0.27267E-01 0.47538E+01
   Dimensionless distance   yplus :  0.13086E-03 0.16850E+02
   ------------------------------------------------------
   Nb of reversal of the velocitv  total_pressure      3.0792e+05      6.2917e+05      5.7427e+05      5.6541e+05


 TIME FOR THE TIME STEP              320:        0.74646E+02

===============================================================


 INSTANT    0.321000000E+03   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        -0.123813550E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58341E+02 0.63696E+01
   Friction velocity        uet   :  0.16333E-01 0.49193E+01
   Friction velocity        uk    :  0.16037E-01 0.47279E+01
   Dimensionless distance   yplus :  0.12362E-03 0.16635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8026
   Nb of faces within the viscous sub-layer     :      16498
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32896E+01     121   0.18174E+00   0.18816E+03 0.49690E+03 
c  Velocity[X]                                      0.52822E+02 
c  Velocity[Y]                                      0.52449E+02 
c  Velocity[Z]                                      0.82889E+02 
c  Pressure     0.11827E+00     716   0.78072E-02   0.42337E+00 0.24275E+04 
c  k            0.15310E+00      73   0.12171E-01   0.78404E+00 0.20165E+04 
c  epsilon      0.39728E+04      51   0.77952E-02   0.17845E+10 0.40528E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.4156e-05                             2
a  epsilon       -0.040628                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  ----v  epsilon              8.086e-05      2.3952e+06          1428.3          27.414
v  TurbVisc            3.7988e-12         0.32756      0.00098693        0.013816
v  total_pressure      3.0296e+05      6.2897e+05      5.7411e+05      5.6538e+05


 TIME FOR THE TIME STEP              322:        0.77304E+02

===============================================================


 INSTANT    0.323000000E+03   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        -0.214768325E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46044E+02 0.64061E+01
   Friction velocity        uet   :  0.23959E-01 0.50100E+01
   Friction velocity        uk    :  0.27267E-01 0.47538E+01
   Dimensionless distance   yplus :  0.13086E-03 0.16850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8089
   Nb of faces within the viscous sub-layer     :      16345
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33085E+01     120   0.18490E+00   0.17715E+03 0.48690E+03 
c  Velocity[X]                                   v  Pressure           -2.0168e+05      1.2879e+05           73974           65358
v  k                   1.4294e-07            8.83        0.044476        0.023536
v  epsilon               1.91e-05       2.384e+06          1488.2          27.516
v  TurbVisc            4.1899e-12         0.23723       0.0010045        0.013838
v  total_pressure      2.9832e+05      6.2879e+05      5.7397e+05      5.6536e+05


 TIME FOR THE TIME STEP              324:        0.61088E+02

===============================================================


 INSTANT    0.325000000E+03   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.364615654E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444439E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49053E+02 0.63986E+01
   Friction velocity        uet   :  0.30566E-01 0.49442E+01
   Friction velocity        uk    :  0.30317E-01v  epsilon              8.086e-05      2.3952e+06          1428.3          27.414
v  TurbVisc            3.7988e-12         0.32756      0.00098693        0.013816
v  total_pressure      3.0296e+05      6.2897e+05      5.7411e+05      5.6538e+05


 TIME FOR THE TIME STEP              322:        0.67993E+02

===============================================================


 INSTANT    0.323000000E+03   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        -0.214768325E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46044E+02 0.64061E+01
   Friction velocity        uet   :  0.23959E-01 0.50100E+01
   Friction velocity        uk    :  0.27267E-01 0.47538E+01
   Dimensionless distance   yplus :  0.13086E-03 0.16850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8089
   Nb of faces within the viscous sub-layer     :      16345
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33085E+01     120   0.18490E+00   0.17715E+03 0.48690E+03 
c  Velocity[X]                                      0.50062E+02 
c  Velocity[Y]                                      0.49552E+02 
c  Velocity[Z]                                      0.77540E+02 
c  Pressure     0.10997E+00     746   0.80119E-02   0.39401E+00 0.13711E+04 
c  k            0.15270E+00      70   0.97913E-02   0.50728E+00 0.19251E+04 
c  epsilon      0.41212E+04      48   0.60172E-02   0.10988E+10 0.37946E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2169e-05                             4
a  epsilon        -0.71075                             5


  ** Computed fields on cells
     ---------------v  Pressure           -2.0168e+05      1.2879e+05           73974           65358
v  k                   1.4294e-07            8.83        0.044476        0.023536
v  epsilon               1.91e-05       2.384e+06          1488.2          27.516
v  TurbVisc            4.1899e-12         0.23723       0.0010045        0.013838
v  total_pressure      2.9832e+05      6.2879e+05      5.7397e+05      5.6536e+05


 TIME FOR THE TIME STEP              324:        0.73004E+02

===============================================================


 INSTANT    0.325000000E+03   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.364615654E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444439E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49053E+02 0.63986E+01
   Friction velocity        uet   :  0.30566E-01 0.49442E+01
   Friction velocity        uk    :  0.30317E-01 0.47492E+01
   Dimensionless distance   yplus :  0.13205E-03 0.14460E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8140
   Nb of faces within the viscous sub-layer     :      16200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------v  Velocity[Z]            -36.657          37.251        -0.59481     -0.00015868
v  ǁVelocityǁ          0.00013282          43.122          4.0104          3.6779
v  Pressure           -2.0646e+05      1.2893e+05           73901           65359
v  k                   7.0587e-08          8.9422        0.045266        0.023518
v  epsilon             0.00012508      2.4166e+06          1544.1          27.629
v  TurbVisc             4.491e-12          0.2163       0.0010178        0.013843
v  total_pressure      2.9354e+05      6.2893e+05       5.739e+05      5.6536e+05


 TIME FOR THE TIME STEP              326:        0.75489E+02

===============================================================


 INSTANT    0.327000000E+03   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.413068649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Relv  Pressure           -2.0168e+05      1.2879e+05           73974           65358
v  k                   1.4294e-07            8.83        0.044476        0.023536
v  epsilon               1.91e-05       2.384e+06          1488.2          27.516
v  TurbVisc            4.1899e-12         0.23723       0.0010045        0.013838
v  total_pressure      2.9832e+05      6.2879e+05      5.7397e+05      5.6536e+05


 TIME FOR THE TIME STEP              324:        0.60685E+02

===============================================================


 INSTANT    0.325000000E+03   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.364615654E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444439E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49053E+02 0.63986E+01
   Friction velocity        uet   :  0.30566E-01 0.49442E+01
   Friction velocity        uk    :  0.30317E-01 0.47492E+01
   Dimensionless distance   yplus :  0.13205E-03 0.14460E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8140
   Nb of faces within the viscous sub-layer     :      16200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33186E+01     120   0.18088E+00   0.16751E+03 0.47102E+03 
c  Velocity[X]                                      0.51284E+02 
c  Velocity[Y]                                      0.47650E+02 
c  Velocity[Z]                                      0.68576E+02 
c  Pressure     0.10708E+00     530   0.78375E-02   0.38588E+00 0.12188E+04 
c  k            0.13188E+00      70   0.66899E-02   0.27651E+00 0.16966E+04 
c  epsilon      0.41684E+04      46   0.56224E-02   0.99324E+09 0.20815E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
v  Velocity[Z]            -36.657          37.251        -0.59481     -0.00015868
v  ǁVelocityǁ          0.00013282          43.122          4.0104          3.6779
v  Pressure           -2.0646e+05      1.2893e+05           73901           65359
v  k                   7.0587e-08          8.9422        0.045266        0.023518
v  epsilon             0.00012508      2.4166e+06          1544.1          27.629
v  TurbVisc             4.491e-12          0.2163       0.0010178        0.013843
v  total_pressure      2.9354e+05      6.2893e+05       5.739e+05      5.6536e+05


 TIME FOR THE TIME STEP              326:        0.72717E+02

===============================================================


 INSTANT    0.327000000E+03   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.413068649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48266E+02 0.64303E+01
   Friction velocity        uet   :  0.29248E-01 0.49859E+01
   Friction velocity        uk    :  0.28895E-01 0.47717E+01
   Dimensionless distance   yplus :  0.13229E-03 0.13970E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8203
   Nb of faces within the viscous sub-layer     :      16073
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------v  Velocity[X]            -9.8113          24.873          1.4507         0.17156
v  Velocity[Y]            -17.704          20.429         0.58157         0.41554
v  Velocity[Z]             -33.65          42.734        -0.60587     -0.00027956
v  ǁVelocityǁ           0.0001281          43.835          4.0328          3.6817
v  Pressure           -2.0894e+05      1.2924e+05           73884           65418
v  k                   2.8143e-08          9.5709        0.045617        0.023519
v  epsilon               0.000153       2.429e+06          1557.9          27.773
v  TurbVisc              6.48e-14         0.21802       0.0010272        0.013845
v  total_pressure      2.9106e+05      6.2924e+05      5.7388e+05      5.6542e+05


 TIME FOR THE TIME STEP              328:        0.69823E+02

===============================================================


 INSTANT    0.329000000E+03   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        -0.152077535E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Z]            -36.657          37.251        -0.59481     -0.00015868
v  ǁVelocityǁ          0.00013282          43.122          4.0104          3.6779
v  Pressure           -2.0646e+05      1.2893e+05           73901           65359
v  k                   7.0587e-08          8.9422        0.045266        0.023518
v  epsilon             0.00012508      2.4166e+06          1544.1          27.629
v  TurbVisc             4.491e-12          0.2163       0.0010178        0.013843
v  total_pressure      2.9354e+05      6.2893e+05       5.739e+05      5.6536e+05


 TIME FOR THE TIME STEP              326:        0.71177E+02

===============================================================


 INSTANT    0.327000000E+03   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.413068649E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48266E+02 0.64303E+01
   Friction velocity        uet   :  0.29248E-01 0.49859E+01
   Friction velocity        uk    :  0.28895E-01 0.47717E+01
   Dimensionless distance   yplus :  0.13229E-03 0.13970E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8203
   Nb of faces within the viscous sub-layer     :      16073
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33334E+01     119   0.18344E+00   0.16531E+03 0.46161E+03 
c  Velocity[X]                                      0.49101E+02 
c  Velocity[Y]                                      0.45457E+02 
c  Velocity[Z]                                      0.70750E+02 
c  Pressure     0.10689E+00     589   0.80654E-02   0.38899E+00 0.11760E+04 
c  k            0.12873E+00      68   0.43504E-02   0.11384E+00 0.11412E+04 
c  epsilon      0.42521E+04      44   0.46757E-02   0.35053E+09 0.11185E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     ---------v  Velocity[X]            -9.8113          24.873          1.4507         0.17156
v  Velocity[Y]            -17.704          20.429         0.58157         0.41554
v  Velocity[Z]             -33.65          42.734        -0.60587     -0.00027956
v  ǁVelocityǁ           0.0001281          43.835          4.0328          3.6817
v  Pressure           -2.0894e+05      1.2924e+05           73884           65418
v  k                   2.8143e-08          9.5709        0.045617        0.023519
v  epsilon               0.000153       2.429e+06          1557.9          27.773
v  TurbVisc              6.48e-14         0.21802       0.0010272        0.013845
v  total_pressure      2.9106e+05      6.2924e+05      5.7388e+05      5.6542e+05


 TIME FOR THE TIME STEP              328:        0.67581E+02

===============================================================


 INSTANT    0.329000000E+03   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        -0.152077535E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61214E+02 0.64325E+01
   Friction velocity        uet   :  0.31681E-01 0.45870E+01
   Friction velocity        uk    :  0.31349E-01 0.47721E+01
   Dimensionless distance   yplus :  0.13038E-03 0.14978E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8259
   Nb of faces within the viscous sub-layer     :      15977
   Total number of wall faces                   :      4
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.21          25.318          1.4537         0.17188
v  Velocity[Y]            -17.605          20.619         0.58415         0.41528
v  Velocity[Z]            -33.354          32.909        -0.61589     -0.00071409
v  ǁVelocityǁ          0.00012729          39.665          4.0545          3.6857
v  Pressure           -2.1175e+05      1.2985e+05           73999           65571
v  k                   2.1942e-07          11.026        0.046034        0.023539
v  epsilon             0.00018323      3.8047e+06          1588.1          27.992
v  TurbVisc            4.7125e-12         0.23535       0.0010337        0.013844
v  total_pressure      2.8825e+05      6.2985e+05        5.74e+05      5.6557e+05


 TIME FOR THE TIME STEP              330:        0.64014E+02

===============================================================


 INSTANT    0.331000000E+03   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        -0.516178460E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           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]            -9.8113          24.873          1.4507         0.17156
v  Velocity[Y]            -17.704          20.429         0.58157         0.41554
v  Velocity[Z]             -33.65          42.734        -0.60587     -0.00027956
v  ǁVelocityǁ           0.0001281          43.835          4.0328          3.6817
v  Pressure           -2.0894e+05      1.2924e+05           73884           65418
v  k                   2.8143e-08          9.5709        0.045617        0.023519
v  epsilon               0.000153       2.429e+06          1557.9          27.773
v  TurbVisc              6.48e-14         0.21802       0.0010272        0.013845
v  total_pressure      2.9106e+05      6.2924e+05      5.7388e+05      5.6542e+05


 TIME FOR THE TIME STEP              328:        0.69617E+02

===============================================================


 INSTANT    0.329000000E+03   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        -0.152077535E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61214E+02 0.64325E+01
   Friction velocity        uet   :  0.31681E-01 0.45870E+01
   Friction velocity        uk    :  0.31349E-01 0.47721E+01
   Dimensionless distance   yplus :  0.13038E-03 0.14978E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8259
   Nb of faces within the viscous sub-layer     :      15977
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33394E+01     119   0.18729E+00   0.16612E+03 0.45741E+03 
c  Velocity[X]                                      0.46707E+02 
c  Velocity[Y]                                      0.43236E+02 
c  Velocity[Z]                                      0.76178E+02 
c  Pressure     0.10135E+00     735   0.79914E-02   0.37081E+00 0.12158E+04 
c  k            0.12914E+00      68   0.40096E-02   0.98088E-01 0.19617E+04 
c  epsilon      0.43315E+04      45   0.83862E
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.21          25.318          1.4537         0.17188
v  Velocity[Y]            -17.605          20.619         0.58415         0.41528
v  Velocity[Z]            -33.354          32.909        -0.61589     -0.00071409
v  ǁVelocityǁ          0.00012729          39.665          4.0545          3.6857
v  Pressure           -2.1175e+05      1.2985e+05           73999           65571
v  k                   2.1942e-07          11.026        0.046034        0.023539
v  epsilon             0.00018323      3.8047e+06          1588.1          27.992
v  TurbVisc            4.7125e-12         0.23535       0.0010337        0.013844
v  total_pressure      2.8825e+05      6.2985e+05        5.74e+05      5.6557e+05


 TIME FOR THE TIME STEP              330:        0.73775E+02

===============================================================


 INSTANT    0.331000000E+03   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        -0.516178460E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39408E+02 0.65274E+01
   Friction velocity        uet   :  0.31938E-01 0.46109E+01
   Friction velocity        uk    :  0.31268E-01 0.47968E+01
   Dimensionless distance   yplus :  0.13069E-03 0.14715E+02
   ------------------------------------------------------
  a  k           -3.9558e-05                             2
a  epsilon          -1.504                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.118          25.067          1.4572         0.17173
v  Velocity[Y]            -18.704          20.531         0.58775          0.4153
v  Velocity[Z]            -36.025          35.596        -0.62465     -0.00085829
v  ǁVelocityǁ          0.00012073          42.409          4.0771          3.6892
v  Pressure           -2.1266e+05      1.3056e+05           74260           65848
v  k                   2.4664e-07          12.691        0.046515        0.023581
v  epsilon             0.00021533      3.9929e+06          1620.1          28.337
v  TurbVisc            4.7266e-12         0.26523       0.0010391        0.013841
v  total_pressure      2.8734e+05      6.3056e+05      5.7426e+05      5.6585e+05


 TIME FOR THE TIME STEP              332:        0.73681E+02

===============================================================


 INSTANT    0.333000000E+03   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        -0.560195389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.21          25.318          1.4537         0.17188
v  Velocity[Y]            -17.605          20.619         0.58415         0.41528
v  Velocity[Z]            -33.354          32.909        -0.61589     -0.00071409
v  ǁVelocityǁ          0.00012729          39.665          4.0545          3.6857
v  Pressure           -2.1175e+05      1.2985e+05           73999           65571
v  k                   2.1942e-07          11.026        0.046034        0.023539
v  epsilon             0.00018323      3.8047e+06          1588.1          27.992
v  TurbVisc            4.7125e-12         0.23535       0.0010337        0.013844
v  total_pressure      2.8825e+05      6.2985e+05        5.74e+05      5.6557e+05


 TIME FOR THE TIME STEP              330:        0.74088E+02

===============================================================


 INSTANT    0.331000000E+03   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        -0.516178460E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39408E+02 0.65274E+01
   Friction velocity        uet   :  0.31938E-01 0.46109E+01
   Friction velocity        uk    :  0.31268E-01 0.47968E+01
   Dimensionless distance   yplus :  0.13069E-03 0.14715E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8332
   Nb of faces within the viscous sub-layer     :      15888
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33389E+01     121   0.17715E+00   0.16297E+03 0.45081E+03 
c  Velocity[X]                                      0.45811E+02 
c  Velocity[Y]                                      0.46754E+02 
c  Velocity[Z]                                      0.70404E+02 
c  Pressure     0.98818Ea  k           -3.9558e-05                             2
a  epsilon          -1.504                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.118          25.067          1.4572         0.17173
v  Velocity[Y]            -18.704          20.531         0.58775          0.4153
v  Velocity[Z]            -36.025          35.596        -0.62465     -0.00085829
v  ǁVelocityǁ          0.00012073          42.409          4.0771          3.6892
v  Pressure           -2.1266e+05      1.3056e+05           74260           65848
v  k                   2.4664e-07          12.691        0.046515        0.023581
v  epsilon             0.00021533      3.9929e+06          1620.1          28.337
v  TurbVisc            4.7266e-12         0.26523       0.0010391        0.013841
v  total_pressure      2.8734e+05      6.3056e+05      5.7426e+05      5.6585e+05


 TIME FOR THE TIME STEP              332:        0.68640E+02

===============================================================


 INSTANT    0.333000000E+03   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        -0.560195389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45687E+02 0.66078E+01
   Friction velocity        uet   :  0.30496E-01 0.46107E+01
   Friction velocity        uk    :  0.
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3927e-05                             3
a  epsilon         -0.9029                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          26.458          1.4613         0.17173
v  Velocity[Y]            -16.889           20.97         0.59279         0.41517
v  Velocity[Z]            -35.681          31.225        -0.63095     -0.00068097
v  ǁVelocityǁ          0.00011685           42.44          4.0998          3.6927
v  Pressure           -2.1771e+05      1.3174e+05           74510           66102
v  k                   2.7397e-07          14.665        0.046922        0.023651
v  epsilon             0.00025018      3.9956e+06          1619.9          28.762
v  TurbVisc            4.7077e-12         0.29637       0.0010446        0.013837
v  total_pressure      2.8229e+05      6.3174e+05      5.7451e+05       5.661e+05


 TIME FOR THE TIME STEP              334:        0.82113E+02

===============================================================


 INSTANT    0.335000000E+03   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.151820798E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.0000a  k           -3.9558e-05                             2
a  epsilon          -1.504                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.118          25.067          1.4572         0.17173
v  Velocity[Y]            -18.704          20.531         0.58775          0.4153
v  Velocity[Z]            -36.025          35.596        -0.62465     -0.00085829
v  ǁVelocityǁ          0.00012073          42.409          4.0771          3.6892
v  Pressure           -2.1266e+05      1.3056e+05           74260           65848
v  k                   2.4664e-07          12.691        0.046515        0.023581
v  epsilon             0.00021533      3.9929e+06          1620.1          28.337
v  TurbVisc            4.7266e-12         0.26523       0.0010391        0.013841
v  total_pressure      2.8734e+05      6.3056e+05      5.7426e+05      5.6585e+05


 TIME FOR THE TIME STEP              332:        0.67155E+02

===============================================================


 INSTANT    0.333000000E+03   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        -0.560195389E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45687E+02 0.66078E+01
   Friction velocity        uet   :  0.30496E-01 0.46107E+01
   Friction velocity        uk    :  0.29524E-01 0.48853E+01
   Dimensionless distance   yplus :  0.12739E-03 0.15892E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8371
   Nb of faces within the viscous sub-layer     :      15745
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33396E+01     122   0.17968E+00   0.16885E+03 0.45430E+03 
c  Velocity[X]                                      0.47946E+02 
c  Velocity
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3927e-05                             3
a  epsilon         -0.9029                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          26.458          1.4613         0.17173
v  Velocity[Y]            -16.889           20.97         0.59279         0.41517
v  Velocity[Z]            -35.681          31.225        -0.63095     -0.00068097
v  ǁVelocityǁ          0.00011685           42.44          4.0998          3.6927
v  Pressure           -2.1771e+05      1.3174e+05           74510           66102
v  k                   2.7397e-07          14.665        0.046922        0.023651
v  epsilon             0.00025018      3.9956e+06          1619.9          28.762
v  TurbVisc            4.7077e-12         0.29637       0.0010446        0.013837
v  total_pressure      2.8229e+05      6.3174e+05      5.7451e+05       5.661e+05


 TIME FOR THE TIME STEP              334:        0.83093E+02

===============================================================


 INSTANT    0.335000000E+03   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.151820798E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -1.603e-05                             1
a  epsilon          -1.037                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.496          25.318          1.4635         0.17204
v  Velocity[Y]            -16.719          20.779          0.5987         0.41563
v  Velocity[Z]            -37.512          35.788        -0.63684     -0.00056102
v  ǁVelocityǁ          0.00011765          44.542          4.1221          3.6961
v  Pressure           -2.2282e+05      1.3363e+05           74867           66426
v  k                   3.0089e-07          14.701        0.047289        0.023706
v  epsilon             0.00029066      3.9711e+06            1617          29.159
v  TurbVisc            4.6868e-12         0.31355       0.0010496        0.013833
v  total_pressure      2.7718e+05      6.3363e+05      5.7487e+05      5.6643e+05


 TIME FOR THE TIME STEP              336:        0.74956E+02

===============================================================


 INSTANT    0.337000000E+03   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3927e-05                             3
a  epsilon         -0.9029                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          26.458          1.4613         0.17173
v  Velocity[Y]            -16.889           20.97         0.59279         0.41517
v  Velocity[Z]            -35.681          31.225        -0.63095     -0.00068097
v  ǁVelocityǁ          0.00011685           42.44          4.0998          3.6927
v  Pressure           -2.1771e+05      1.3174e+05           74510           66102
v  k                   2.7397e-07          14.665        0.046922        0.023651
v  epsilon             0.00025018      3.9956e+06          1619.9          28.762
v  TurbVisc            4.7077e-12         0.29637       0.0010446        0.013837
v  total_pressure      2.8229e+05      6.3174e+05      5.7451e+05       5.661e+05


 TIME FOR THE TIME STEP              334:        0.81952E+02

===============================================================


 INSTANT    0.335000000E+03   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.151820798E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39882E+02 0.65960E+01
   Friction velocity        uet   :  0.34738E-01 0.46392E+01
   Friction velocity        uk    :  0.34663E-01 0.48629E+01
   Dimensionless distance   yplus :  0.12547E-03 0.16538E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8438
   Nb of faces within the viscous sub-layer     :      15648
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
---------------------------------------------------------------------------------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -1.603e-05                             1
a  epsilon          -1.037                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.496          25.318          1.4635         0.17204
v  Velocity[Y]            -16.719          20.779          0.5987         0.41563
v  Velocity[Z]            -37.512          35.788        -0.63684     -0.00056102
v  ǁVelocityǁ          0.00011765          44.542          4.1221          3.6961
v  Pressure           -2.2282e+05      1.3363e+05           74867           66426
v  k                   3.0089e-07          14.701        0.047289        0.023706
v  epsilon             0.00029066      3.9711e+06            1617          29.159
v  TurbVisc            4.6868e-12         0.31355       0.0010496        0.013833
v  total_pressure      2.7718e+05      6.3363e+05      5.7487e+05      5.6643e+05


 TIME FOR THE TIME STEP              336:        0.72823E+02

===============================================================


 INSTANT    0.337000000E+03   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.177642229E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------c  k            0.18445E+00      64   0.60381E-02   0.37254E+00 0.11498E+04 
c  epsilon      0.45124E+04      42   0.37751E-02   0.36976E+09 0.20344E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.9953e-06                             2
a  epsilon         -1.0274                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.822          26.082           1.465         0.17277
v  Velocity[Y]             -18.95           20.73         0.60277         0.41563
v  Velocity[Z]            -35.962          31.297        -0.64199     -0.00067664
v  ǁVelocityǁ          0.00012117          42.576          4.1433          3.6993
v  Pressure           -2.2791e+05      1.3422e+05           75112           66657
v  k                   3.2752e-07          14.117        0.047644        0.023739
v  epsilon             0.00034052      3.9957e+06            1628          29.432
v  TurbVisc             4.703e-12         0.29982       0.0010536         0.01383
v  total_pressure      2.7209e+05      6.3422e+05      5.7511e+05      5.6666e+05


 TIME FOR THE TIME STEP              338:        0.71580E+02

===============================================================


 INSTANT    0.339000000E+03   TIME STEP NUMBER             339
 ============================================================= 




   ** 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            -1.603e-05                             1
a  epsilon          -1.037                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.496          25.318          1.4635         0.17204
v  Velocity[Y]            -16.719          20.779          0.5987         0.41563
v  Velocity[Z]            -37.512          35.788        -0.63684     -0.00056102
v  ǁVelocityǁ          0.00011765          44.542          4.1221          3.6961
v  Pressure           -2.2282e+05      1.3363e+05           74867           66426
v  k                   3.0089e-07          14.701        0.047289        0.023706
v  epsilon             0.00029066      3.9711e+06            1617          29.159
v  TurbVisc            4.6868e-12         0.31355       0.0010496        0.013833
v  total_pressure      2.7718e+05      6.3363e+05      5.7487e+05      5.6643e+05


 TIME FOR THE TIME STEP              336:        0.80989E+02

===============================================================


 INSTANT    0.337000000E+03   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.177642229E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46235E+02 0.65757E+01
   Friction velocity        uet   :  0.20001E-01 0.46008E+01
   Friction velocity        uk    :  0.19954E-01 0.47926E+01
   Dimensionless distance   yplus :  0.12565E-03 0.17962E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8525
   Nb of faces within the viscous sub-layer     :      15556
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
c  k            0.18445E+00      64   0.60381E-02   0.37254E+00 0.11498E+04 
c  epsilon      0.45124E+04      42   0.37751E-02   0.36976E+09 0.20344E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.9953e-06                             2
a  epsilon         -1.0274                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.822          26.082           1.465         0.17277
v  Velocity[Y]             -18.95           20.73         0.60277         0.41563
v  Velocity[Z]            -35.962          31.297        -0.64199     -0.00067664
v  ǁVelocityǁ          0.00012117          42.576          4.1433          3.6993
v  Pressure           -2.2791e+05      1.3422e+05           75112           66657
v  k                   3.2752e-07          14.117        0.047644        0.023739
v  epsilon             0.00034052      3.9957e+06            1628          29.432
v  TurbVisc             4.703e-12         0.29982       0.0010536         0.01383
v  total_pressure      2.7209e+05      6.3422e+05      5.7511e+05      5.6666e+05


 TIME FOR THE TIME STEP              338:        0.72646E+02

===============================================================


 INSTANT    0.339000000E+03   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.278795990E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           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[Z]                                      0.71242E+02 
c  Pressure     0.96588E-01     773   0.74007E-02   0.35165E+00 0.75242E+03 
c  k            0.18719E+00      69   0.69588E-02   0.53997E+00 0.14079E+04 
c  epsilon      0.45156E+04      44   0.54995E-02   0.17944E+10 0.27485E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2583e-05                             1
a  epsilon        -0.38814                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.939           26.02          1.4653          0.1731
v  Velocity[Y]            -19.593           20.74         0.60576         0.41568
v  Velocity[Z]            -37.197          35.997        -0.64619     -0.00070442
v  ǁVelocityǁ          0.00012256          44.128          4.1645          3.7031
v  Pressure           -2.3167e+05      1.3457e+05           75474           66958
v  k                   3.5506e-07          16.022        0.048001        0.023776
v  epsilon             0.00039115      3.9922e+06          1641.1          29.692
v  TurbVisc            4.7358e-12         0.33498       0.0010558        0.013827
v  total_pressure      2.6833e+05      6.3457e+05      5.7547e+05      5.6696e+05


 TIME FOR THE TIME STEP              340:        0.64881E+02

===============================================================


 INSTANT    0.341000000E+03   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      --------------c  k            0.18445E+00      64   0.60381E-02   0.37254E+00 0.11498E+04 
c  epsilon      0.45124E+04      42   0.37751E-02   0.36976E+09 0.20344E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.9953e-06                             2
a  epsilon         -1.0274                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.822          26.082           1.465         0.17277
v  Velocity[Y]             -18.95           20.73         0.60277         0.41563
v  Velocity[Z]            -35.962          31.297        -0.64199     -0.00067664
v  ǁVelocityǁ          0.00012117          42.576          4.1433          3.6993
v  Pressure           -2.2791e+05      1.3422e+05           75112           66657
v  k                   3.2752e-07          14.117        0.047644        0.023739
v  epsilon             0.00034052      3.9957e+06            1628          29.432
v  TurbVisc             4.703e-12         0.29982       0.0010536         0.01383
v  total_pressure      2.7209e+05      6.3422e+05      5.7511e+05      5.6666e+05


 TIME FOR THE TIME STEP              338:        0.72720E+02

===============================================================


 INSTANT    0.339000000E+03   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.278795990E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35088E+02 0.65799E+01
   Friction velocity        uet   :  0.19040E-01 0.46090E+01
   Friction velocity        uk    :  0.18660E-01 0.47743E+01
   Dimensionless distance   yplus :  0.12726E-03 0.18008E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8572
   Nb of faces within the viscous sub-layer     :      15471
   Total number of wall faces                   :      41000
------------------------------------------------------------



  c  Velocity[Z]                                      0.71242E+02 
c  Pressure     0.96588E-01     773   0.74007E-02   0.35165E+00 0.75242E+03 
c  k            0.18719E+00      69   0.69588E-02   0.53997E+00 0.14079E+04 
c  epsilon      0.45156E+04      44   0.54995E-02   0.17944E+10 0.27485E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2583e-05                             1
a  epsilon        -0.38814                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.939           26.02          1.4653          0.1731
v  Velocity[Y]            -19.593           20.74         0.60576         0.41568
v  Velocity[Z]            -37.197          35.997        -0.64619     -0.00070442
v  ǁVelocityǁ          0.00012256          44.128          4.1645          3.7031
v  Pressure           -2.3167e+05      1.3457e+05           75474           66958
v  k                   3.5506e-07          16.022        0.048001        0.023776
v  epsilon             0.00039115      3.9922e+06          1641.1          29.692
v  TurbVisc            4.7358e-12         0.33498       0.0010558        0.013827
v  total_pressure      2.6833e+05      6.3457e+05      5.7547e+05      5.6696e+05


 TIME FOR THE TIME STEP              340:        0.72555E+02

===============================================================


 INSTANT    0.341000000E+03   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         0.461891291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15   c  Velocity     0.33548E+01     118   0.17902E+00   0.15176E+03 0.44042E+03 
c  Velocity[X]                                      0.47241E+02 
c  Velocity[Y]                                      0.43344E+02 
c  Velocity[Z]                                      0.61172E+02 
c  Pressure     0.98158E-01     701   0.83983E-02   0.35519E+00 0.12685E+04 
c  k            0.19714E+00      72   0.45172E-02   0.29191E+00 0.13344E+04 
c  epsilon      0.45650E+04      49   0.52077E-02   0.18243E+10 0.24976E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7389e-06                             2
a  epsilon         -1.4335                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.013          26.406          1.4667         0.17348
v  Velocity[Y]            -18.083           20.92         0.60765         0.41528
v  Velocity[Z]            -39.665          30.547        -0.64953      -0.0010646
v  ǁVelocityǁ          0.00012727          46.999           4.185          3.7077
v  Pressure           -2.3491e+05      1.3502e+05           75699           67138
v  k                   3.8501e-07          16.595        0.048486        0.023843
v  epsilon              0.0004411      3.9665e+06          1661.9           30.04
v  TurbVisc            4.7819e-12         0.43132       0.0010587        0.013826
v  total_pressure      2.6509e+05      6.3502e+05       5.757e+05      5.6714e+05


 TIME FOR THE TIME STEP              342:        0.60021E+02

===============================================================


 INSTANT    0.343000000E+03   TIME STEP NUMBERc  Velocity[Z]                                      0.71242E+02 
c  Pressure     0.96588E-01     773   0.74007E-02   0.35165E+00 0.75242E+03 
c  k            0.18719E+00      69   0.69588E-02   0.53997E+00 0.14079E+04 
c  epsilon      0.45156E+04      44   0.54995E-02   0.17944E+10 0.27485E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.2583e-05                             1
a  epsilon        -0.38814                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.939           26.02          1.4653          0.1731
v  Velocity[Y]            -19.593           20.74         0.60576         0.41568
v  Velocity[Z]            -37.197          35.997        -0.64619     -0.00070442
v  ǁVelocityǁ          0.00012256          44.128          4.1645          3.7031
v  Pressure           -2.3167e+05      1.3457e+05           75474           66958
v  k                   3.5506e-07          16.022        0.048001        0.023776
v  epsilon             0.00039115      3.9922e+06          1641.1          29.692
v  TurbVisc            4.7358e-12         0.33498       0.0010558        0.013827
v  total_pressure      2.6833e+05      6.3457e+05      5.7547e+05      5.6696e+05


 TIME FOR THE TIME STEP              340:        0.78669E+02

===============================================================


 INSTANT    0.341000000E+03   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         0.461891291E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46823E+02 0.65884E+01
   Friction velocity        uet   :  0.20106E-01 0.46273E+01
   Friction velocity        uk    :  0.19690E-01 0.47723E+01
   Dimensionless distance   yplus :  0.12793E-03 0.18683E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wc  Velocity     0.33548E+01     118   0.17902E+00   0.15176E+03 0.44042E+03 
c  Velocity[X]                                      0.47241E+02 
c  Velocity[Y]                                      0.43344E+02 
c  Velocity[Z]                                      0.61172E+02 
c  Pressure     0.98158E-01     701   0.83983E-02   0.35519E+00 0.12685E+04 
c  k            0.19714E+00      72   0.45172E-02   0.29191E+00 0.13344E+04 
c  epsilon      0.45650E+04      49   0.52077E-02   0.18243E+10 0.24976E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7389e-06                             2
a  epsilon         -1.4335                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.013          26.406          1.4667         0.17348
v  Velocity[Y]            -18.083           20.92         0.60765         0.41528
v  Velocity[Z]            -39.665          30.547        -0.64953      -0.0010646
v  ǁVelocityǁ          0.00012727          46.999           4.185          3.7077
v  Pressure           -2.3491e+05      1.3502e+05           75699           67138
v  k                   3.8501e-07          16.595        0.048486        0.023843
v  epsilon              0.0004411      3.9665e+06          1661.9           30.04
v  TurbVisc            4.7819e-12         0.43132       0.0010587        0.013826
v  total_pressure      2.6509e+05      6.3502e+05       5.757e+05      5.6714e+05


 TIME FOR THE TIME STEP              342:        0.77120E+02

===============================================================


 INSTANT    0.343000000E+03   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         0.187652612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33585E+01     116   0.18171E+00   0.15789E+03 0.43960E+03 
c  Velocity[X]                                      0.47392E+02 
c  Velocity[Y]                                      0.44836E+02 
c  Velocity[Z]                                      0.65663E+02 
c  Pressure     0.96115E-01     809   0.66143E-02   0.34635E+00 0.39062E+03 
c  k            0.19549E+00      70   0.53789E-02   0.18008E+00 0.89763E+03 
c  epsilon      0.45824E+04      48   0.56830E-02   0.33139E+09 0.17160E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1061e-06                             1
a  epsilon         -1.8642                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.115          27.675          1.4696         0.17355
v  Velocity[Y]            -18.713          20.522         0.60815         0.41533
v  Velocity[Z]             -40.79          33.362        -0.65362      -0.0011175
v  ǁVelocityǁ          0.00012638          48.435          4.2043          3.7113
v  Pressure           -2.3761e+05      1.3513e+05           75765           67209
v  k                   4.1832e-07          18.537        0.048799        0.023851
v  epsilon             0.00049667      3.9816e+06          1670.8          30.124
v  TurbVisc            4.8184e-12         0.41167       0.0010608        0.013827
v  total_pressure      2.6239e+05      6.3513e+05  c  Velocity     0.33548E+01     118   0.17902E+00   0.15176E+03 0.44042E+03 
c  Velocity[X]                                      0.47241E+02 
c  Velocity[Y]                                      0.43344E+02 
c  Velocity[Z]                                      0.61172E+02 
c  Pressure     0.98158E-01     701   0.83983E-02   0.35519E+00 0.12685E+04 
c  k            0.19714E+00      72   0.45172E-02   0.29191E+00 0.13344E+04 
c  epsilon      0.45650E+04      49   0.52077E-02   0.18243E+10 0.24976E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.7389e-06                             2
a  epsilon         -1.4335                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.013          26.406          1.4667         0.17348
v  Velocity[Y]            -18.083           20.92         0.60765         0.41528
v  Velocity[Z]            -39.665          30.547        -0.64953      -0.0010646
v  ǁVelocityǁ          0.00012727          46.999           4.185          3.7077
v  Pressure           -2.3491e+05      1.3502e+05           75699           67138
v  k                   3.8501e-07          16.595        0.048486        0.023843
v  epsilon              0.0004411      3.9665e+06          1661.9           30.04
v  TurbVisc            4.7819e-12         0.43132       0.0010587        0.013826
v  total_pressure      2.6509e+05      6.3502e+05       5.757e+05      5.6714e+05


 TIME FOR THE TIME STEP              342:        0.74352E+02

===============================================================


 INSTANT    0.343000000E+03   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         0.187652612E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41122E+02 0.65828E+01
   Friction velocity        uet   :  0.11780E-01 0.46176E+01
   Friction velocity        uk    :  0.11680E-01 0.47787E+01
   Di   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33585E+01     116   0.18171E+00   0.15789E+03 0.43960E+03 
c  Velocity[X]                                      0.47392E+02 
c  Velocity[Y]                                      0.44836E+02 
c  Velocity[Z]                                      0.65663E+02 
c  Pressure     0.96115E-01     809   0.66143E-02   0.34635E+00 0.39062E+03 
c  k            0.19549E+00      70   0.53789E-02   0.18008E+00 0.89763E+03 
c  epsilon      0.45824E+04      48   0.56830E-02   0.33139E+09 0.17160E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1061e-06                             1
a  epsilon         -1.8642                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.115          27.675          1.4696         0.17355
v  Velocity[Y]            -18.713          20.522         0.60815         0.41533
v  Velocity[Z]             -40.79          33.362        -0.65362      -0.0011175
v  ǁVelocityǁ          0.00012638          48.435          4.2043          3.7113
v  Pressure           -2.3761e+05      1.3513e+05           75765           67209
v  k                   4.1832e-07          18.537        0.048799        0.023851
v  epsilon             0.00049667      3.9816e+06          1670.8          30.124
v  TurbVisc            4.8184e-12         0.41167       0.0010608        0.013827
v  total_pressure      2.6239e+05      6.3513e+05      5.7577e+05      5.6721e+05


 TIME FOR THE TIME STEP              344:        0.73672E+02

===============================================================


 INSTANT    0.345000000E+03   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         0.411631781E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45940E+02 0.68175E+01
   Friction velocity        uet   :  0.26714E-01 0.46463E+01
   Friction velocity        uk    :  0.26056E-01 0.47665E+01
   Dimensionless distance   yplus :  0.13007E-03 0.19021E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8686
   Nb of faces within the viscous sub-layer     :      15225
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33600E+01     116   0.18295E+00   0.15441E+03 0.43661E+03 
c  Velocity[X]                                      0.46070E+02 
c  Velocity[Y]                                      0.43965E+02 
c  Velocity[Z]                                      0.64372E+02 
c  Pressure     0.97163E-01     742   0.69485E-02   0.35430E+00 0.88729E+03 
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33585E+01     116   0.18171E+00   0.15789E+03 0.43960E+03 
c  Velocity[X]                                      0.47392E+02 
c  Velocity[Y]                                      0.44836E+02 
c  Velocity[Z]                                      0.65663E+02 
c  Pressure     0.96115E-01     809   0.66143E-02   0.34635E+00 0.39062E+03 
c  k            0.19549E+00      70   0.53789E-02   0.18008E+00 0.89763E+03 
c  epsilon      0.45824E+04      48   0.56830E-02   0.33139E+09 0.17160E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1061e-06                             1
a  epsilon         -1.8642                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.115          27.675          1.4696         0.17355
v  Velocity[Y]            -18.713          20.522         0.60815         0.41533
v  Velocity[Z]             -40.79          33.362        -0.65362      -0.0011175
v  ǁVelocityǁ          0.00012638          48.435          4.2043          3.7113
v  Pressure           -2.3761e+05      1.3513e+05           75765           67209
v  k                   4.1832e-07          18.537        0.048799        0.023851
v  epsilon             0.00049667      3.9816e+06          1670.8          30.124
v  TurbVisc            4.8184e-12         0.41167       0.0010608        0.013827
v  total_pressure      2.6239e+05      6.3513e+05      5.7577e+05      5.6721e+05


 TIME FOR THE TIME STEP              344:        0.73875E+02

===============================================================


 INSTANT    0.345000000E+03   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         0.411631781E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45940E+02 0.68175E+01
   Friction velocity        uet   :  0.26714E-01 0.46463E+01
   Friction velocity        uk    :  0.26056E-01 0.47665E+01
   Dimensionless distance   yplus :  0.13007E-03 0.19021E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8686
   Nb of faces within the viscous sub-layer     :      15225
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33600E+01     116   0.18295E+00   0.15441E+03 0.43661E+03 
c  Velocity[X]                                      0.46070E+02 
c  Velocity[Y]                                      0.43965E+02 
c  Velocity[Z]                                      0.64372E+02 
c  Pressure     0.97163E-01     742   0.69485E-02   0.35430E+00 0.88729E+03 
c  k            0.18307E+00      67   0.67241E-02   0.30610E+00 0.10376E+04 
c  epsilon      0.45694E+04      46   0.38936E-02   0.24193E+09 0.12333E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.0421e-05                             2
a  epsilon         -2.0569                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.208          26.352          1.4711         0.17329
v  Velocity[Y]            -18.651          20.401         0.60757          0.4154
v  Velocity[Z]            -36.539          33.718        -0.65578      -0.0012495
v  ǁVelocityǁ          0.00012662          43.962          4.2137           3.713
v  Pressure           -2.3782e+05      1.3559e+05           75861           67292
v  k                   4.3616e-07           16.28        0.048955        0.023828
v  epsilon             0.00052356      3.9609e+06          1678.5          30.074
v  TurbVisc            4.8314e-12         0.40875       0.0010621        0.013828
v  total_pressure      2.6218   Nb of faces within the viscous sub-layer     :      15172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33625E+01     113   0.17912E+00   0.14534E+03 0.42789E+03 
c  Velocity[X]                                      0.43925E+02 
c  Velocity[Y]                                      0.44972E+02 
c  Velocity[Z]                                      0.56447E+02 
c  Pressure     0.89222E-01     679   0.55721E-02   0.32285E+00 0.83903E+03 
c  k            0.17093E+00      67   0.50187E-02   0.17172E+00 0.10787E+04 
c  epsilon      0.46137E+04      45   0.48172E-02   0.50097E+09 0.18551E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6923e-05                             1
a  epsilon         -4.0842                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          27.502          1.4759           0.173
v  Velocity[Y]            -17.613          20.818         0.60926         0.41546
v  Velocity[Z]            -41.966          35.123        -0.66242      -0.0010055
v  ǁVelocityǁ          0.00012496          48.732          4.2404          3.7187
v  Pressure           -2.3736e+05      1.3607e+05           76114           675   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33592E+01     115   0.17897E+00   0.15546E+03 0.44120E+03 
c  Velocity[X]                                      0.47198E+02 
c  Velocity[Y]                                      0.45239E+02 
c  Velocity[Z]                                      0.63023E+02 
c  Pressure     0.93030E-01     658   0.60587E-02   0.33613E+00 0.83345E+03 
c  k            0.17638E+00      66   0.48925E-02   0.11770E+00 0.84851E+03 
c  epsilon      0.45762E+04      45   0.32081E-02   0.25336E+09 0.12399E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0981e-05                             2
a  epsilon         -1.6572                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -13.087          26.562           1.473         0.17345
v  Velocity[Y]            -21.071          20.602         0.60782         0.41533
v  Velocity[Z]            -39.289            36.7        -0.65792       -0.001158
v  ǁVelocityǁ          0.00012617           46.62          4.2229           3.715
v  Pressure           -2.3846e+05      1.3589e+05           75906           67330
v  k                    4.546e-07          15.842        0.049015        0.023812
v  epsilon             0.00055114      3.9697e+06          1685.4          29.998
v  TurbVisc            4.8541e-12         0.34721       0.0010629        0.013828
v  total_pressure      2.6154e+05      6.3589e+05      5.7591e+05      5.6733e+05


 TIME FOR THE TIME STEP              346:        0.69953E+02

===============================================================


 INSTANT    0.347000000E+03   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.172008152E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------------   Nb of faces within the viscous sub-layer     :      15172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33625E+01     113   0.17912E+00   0.14534E+03 0.42789E+03 
c  Velocity[X]                                      0.43925E+02 
c  Velocity[Y]                                      0.44972E+02 
c  Velocity[Z]                                      0.56447E+02 
c  Pressure     0.89222E-01     679   0.55721E-02   0.32285E+00 0.83903E+03 
c  k            0.17093E+00      67   0.50187E-02   0.17172E+00 0.10787E+04 
c  epsilon      0.46137E+04      45   0.48172E-02   0.50097E+09 0.18551E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6923e-05                             1
a  epsilon         -4.0842                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          27.502          1.4759           0.173
v  Velocity[Y]            -17.613          20.818         0.60926         0.41546
v  Velocity[Z]            -41.966          35.123        -0.66242      -0.0010055
v  ǁVelocityǁ          0.00012496          48.732          4.2404          3.7187
v  Pressure           -2.3736e+05      1.3607e+05           76114           67510
v  k                   1.0262e-07          14.906        0.049355        0.023815
v  epsilon             0.00021826      3.9601e+06          1706.6          30.052
v  TurbVisc            4.8786e-12         0.35011       0.0010655         0.01383
v  total_pressure      2.6264e+05      6.3607e+05      5.7611e+05      5.6751e+05


 TIME FOR THE TIME STEP              348:        0.69520E+02

===============================================================


 INSTANT    0.349000000E+03   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.12947E-03 0.17276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8732
   Nb of faces within the viscous sub-layer     :      15105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33581E+01     115   0.18023E+00   0.14314E+03 0.42992E+03 
c  Velocity[X]                                      0.44823E+02 
c  Velocity[Y]                                      0.43678E+02 
c  Velocity[Z]                                      0.54641E+02 
c  Pressure     0.87524E-01     718   0.52166E-02   0.31723E+00 0.61697E+03 
c  k            0.17444E+00      65   0.63021E-02   0.26425E+00 0.10936E+04 
c  epsilon      0.46378E+04      43   0.43025E-02   0.31116E+09 0.93383E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5327e-05                             1
a  epsilon         -1.6741                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.327          25.947          1.4793         0.17305
v  Velocity[Y]            -17.452          20.993         0.61269          0.4156
v  Velocity[Z]            -37.438          31.245        -0   Nb of faces within the viscous sub-layer     :      15172
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33625E+01     113   0.17912E+00   0.14534E+03 0.42789E+03 
c  Velocity[X]                                      0.43925E+02 
c  Velocity[Y]                                      0.44972E+02 
c  Velocity[Z]                                      0.56447E+02 
c  Pressure     0.89222E-01     679   0.55721E-02   0.32285E+00 0.83903E+03 
c  k            0.17093E+00      67   0.50187E-02   0.17172E+00 0.10787E+04 
c  epsilon      0.46137E+04      45   0.48172E-02   0.50097E+09 0.18551E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.6923e-05                             1
a  epsilon         -4.0842                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.553          27.502          1.4759           0.173
v  Velocity[Y]            -17.613          20.818         0.60926         0.41546
v  Velocity[Z]            -41.966          35.123        -0.66242      -0.0010055
v  ǁVelocityǁ          0.00012496          48.732          4.2404          3.7187
v  Pressure           -2.3736e+05      1.3607e+05           76114           67510
v  k                   1.0262e-07          14.906        0.049355        0.023815
v  epsilon             0.00021826      3.9601e+06          1706.6          30.052
v  TurbVisc            4.8786e-12         0.35011       0.0010655         0.01383
v  total_pressure      2.6264e+05      6.3607e+05      5.7611e+05      5.6751e+05


 TIME FOR THE TIME STEP              348:        0.80348E+02

===============================================================


 INSTANT    0.349000000E+03   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.922650605E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
-------------   Dimensionless distance   yplus :  0.12947E-03 0.17276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8732
   Nb of faces within the viscous sub-layer     :      15105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33581E+01     115   0.18023E+00   0.14314E+03 0.42992E+03 
c  Velocity[X]                                      0.44823E+02 
c  Velocity[Y]                                      0.43678E+02 
c  Velocity[Z]                                      0.54641E+02 
c  Pressure     0.87524E-01     718   0.52166E-02   0.31723E+00 0.61697E+03 
c  k            0.17444E+00      65   0.63021E-02   0.26425E+00 0.10936E+04 
c  epsilon      0.46378E+04      43   0.43025E-02   0.31116E+09 0.93383E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5327e-05                             1
a  epsilon         -1.6741                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.327          25.947          1.4793         0.17305
v  Velocity[Y]            -17.452          20.993         0.61269          0.4156
v  Velocity[Z]            -37.438          31.245        -0.66679     -0.00088302
v  ǁVelocityǁ          0.00012414           43.59          4.2561          3.7224
v  Pressure           -2.3648e+05      1.3647e+05           76343           67682
v  k                   5.2864e-07          14.634        0.049663        0.023848
v  epsilon             0.00065115      3.9855e+06          1722.4          30.194
v  TurbVisc            4.8874e-12         0.30605       0.0010678        0.013832
v  total_pressure      2.6352e+05      6.3647e+05      5.7634e+05      5.6768e+05


 TIME FOR THE TIME STEP              350:        0.68089E+02

=========================   Rel velocity at the wall uiptn : -0.34314E+02 0.11124E+02
   Friction velocity        uet   :  0.22132E-01 0.46495E+01
   Friction velocity        uk    :  0.22077E-01 0.48056E+01
   Dimensionless distance   yplus :  0.12870E-03 0.19512E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8759
   Nb of faces within the viscous sub-layer     :      15069
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33641E+01     115   0.18158E+00   0.14053E+03 0.42418E+03 
c  Velocity[X]                                      0.41715E+02 
c  Velocity[Y]                                      0.45710E+02 
c  Velocity[Z]                                      0.53105E+02 
c  Pressure     0.90436E-01     688   0.53369E-02   0.32593E+00 0.13861E+04 
c  k            0.19561E+00      63   0.86126E-02   0.50381E+00 0.15354E+04 
c  epsilon      0.46892E+04      44   0.63585E-02   0.28926E+10 0.39429E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5687e-05                             3
a  epsilon         -1.9051                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.63             Dimensionless distance   yplus :  0.12947E-03 0.17276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8732
   Nb of faces within the viscous sub-layer     :      15105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33581E+01     115   0.18023E+00   0.14314E+03 0.42992E+03 
c  Velocity[X]                                      0.44823E+02 
c  Velocity[Y]                                      0.43678E+02 
c  Velocity[Z]                                      0.54641E+02 
c  Pressure     0.87524E-01     718   0.52166E-02   0.31723E+00 0.61697E+03 
c  k            0.17444E+00      65   0.63021E-02   0.26425E+00 0.10936E+04 
c  epsilon      0.46378E+04      43   0.43025E-02   0.31116E+09 0.93383E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5327e-05                             1
a  epsilon         -1.6741                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.327          25.947          1.4793         0.17305
v  Velocity[Y]            -17.452          20.993         0.61269          0.4156
v  Velocity[Z]            -37.438          31.245        -0.66679     -0.00088302
v  ǁVelocityǁ          0.00012414           43.59          4.2561          3.7224
v  Pressure           -2.3648e+05      1.3647e+05           76343           67682
v  k                   5.2864e-07          14.634        0.049663        0.023848
v  epsilon             0.00065115      3.9855e+06          1722.4          30.194
v  TurbVisc            4.8874e-12         0.30605       0.0010678        0.013832
v  total_pressure      2.6352e+05      6.3647e+05      5.7634e+05      5.6768e+05


 TIME FOR THE TIME STEP              350:        0.74870E+02

===============================================================


 INSTANT    0.351000000E+03   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        -0.289435422E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         Rel velocity at the wall uiptn : -0.34314E+02 0.11124E+02
   Friction velocity        uet   :  0.22132E-01 0.46495E+01
   Friction velocity        uk    :  0.22077E-01 0.48056E+01
   Dimensionless distance   yplus :  0.12870E-03 0.19512E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8759
   Nb of faces within the viscous sub-layer     :      15069
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33641E+01     115   0.18158E+00   0.14053E+03 0.42418E+03 
c  Velocity[X]                                      0.41715E+02 
c  Velocity[Y]                                      0.45710E+02 
c  Velocity[Z]                                      0.53105E+02 
c  Pressure     0.90436E-01     688   0.53369E-02   0.32593E+00 0.13861E+04 
c  k            0.19561E+00      63   0.86126E-02   0.50381E+00 0.15354E+04 
c  epsilon      0.46892E+04      44   0.63585E-02   0.28926E+10 0.39429E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5687e-05                             3
a  epsilon         -1.9051                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.63          27.418          1.4811         0.17298
v  Velocity[Y]            -18.413          20.946         0.61665         0.41581
v  Velocity[Z]            -47.049           37.53        -0.67163      -0.0009788
v  ǁVelocityǁ          0.00012228          52.934          4.2708          3.7265
v  Pressure           -2.3412e+05      1.3716e+05           76987           68182
v  k                   5.6211e-07          18.001        0.049905        0.023919
v  epsilon             0.00010368      3.9988e+06          1740.8          30.449
v  TurbVisc            4.8312e-12          0.3356       0.0010708     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44768E+02 0.12084E+02
   Friction velocity        uet   :  0.21484E-01 0.46748E+01
   Friction velocity        uk    :  0.20991E-01 0.48949E+01
   Dimensionless distance   yplus :  0.12757E-03 0.20017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8792
   Nb of faces within the viscous sub-layer     :      15042
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33646E+01     115   0.18110E+00   0.14635E+03 0.43485E+03 
c  Velocity[X]                                      0.45358E+02 
c  Velocity[Y]                                      0.44788E+02 
c  Velocity[Z]                                      0.56209E+02 
c  Pressure     0.82302E-01     662   0.52484E-02   0.29538E+00 0.15273E+04 
c  k            0.19728E+00      66   0.89139E-02   0.72311E+00 0.12672E+04 
c  epsilon      0.47357E+04      46   0.38622E-02   0.15816E+09 0.74105E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -4.447e-06                             2
a  epsilon         -43.735                             7


  ** Computed fields on cells
     ------------------------

   field                   Rel velocity at the wall uiptn : -0.34314E+02 0.11124E+02
   Friction velocity        uet   :  0.22132E-01 0.46495E+01
   Friction velocity        uk    :  0.22077E-01 0.48056E+01
   Dimensionless distance   yplus :  0.12870E-03 0.19512E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8759
   Nb of faces within the viscous sub-layer     :      15069
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33641E+01     115   0.18158E+00   0.14053E+03 0.42418E+03 
c  Velocity[X]                                      0.41715E+02 
c  Velocity[Y]                                      0.45710E+02 
c  Velocity[Z]                                      0.53105E+02 
c  Pressure     0.90436E-01     688   0.53369E-02   0.32593E+00 0.13861E+04 
c  k            0.19561E+00      63   0.86126E-02   0.50381E+00 0.15354E+04 
c  epsilon      0.46892E+04      44   0.63585E-02   0.28926E+10 0.39429E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5687e-05                             3
a  epsilon         -1.9051                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.63          27.418          1.4811         0.17298
v  Velocity[Y]            -18.413          20.946         0.61665         0.41581
v  Velocity[Z]            -47.049           37.53        -0.67163      -0.0009788
v  ǁVelocityǁ          0.00012228          52.934          4.2708          3.7265
v  Pressure           -2.3412e+05      1.3716e+05           76987           68182
v  k                   5.6211e-07          18.001        0.049905        0.023919
v  epsilon             0.00010368      3.9988e+06          1740.8          30.449
v  TurbVisc            4.8312e-12          0.3356       0.0010708        0.013835
v  total_pressure      2.6588e+05      6.3716e+05      5.7699e+05      5.6818e+05


 TIME FOR THE TIME STEP              352:        0.70994E+02

===============================================================


 INSTANT    0.353000000E+03   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        -0.966694072E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4    ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44768E+02 0.12084E+02
   Friction velocity        uet   :  0.21484E-01 0.46748E+01
   Friction velocity        uk    :  0.20991E-01 0.48949E+01
   Dimensionless distance   yplus :  0.12757E-03 0.20017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8792
   Nb of faces within the viscous sub-layer     :      15042
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33646E+01     115   0.18110E+00   0.14635E+03 0.43485E+03 
c  Velocity[X]                                      0.45358E+02 
c  Velocity[Y]                                      0.44788E+02 
c  Velocity[Z]                                      0.56209E+02 
c  Pressure     0.82302E-01     662   0.52484E-02   0.29538E+00 0.15273E+04 
c  k            0.19728E+00      66   0.89139E-02   0.72311E+00 0.12672E+04 
c  epsilon      0.47357E+04      46   0.38622E-02   0.15816E+09 0.74105E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -4.447e-06                             2
a  epsilon         -43.735                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.28           26.54          1.4819         0.17306
v  Velocity[Y]             -18.51          21.103         0.62036         0.41599
v  Velocity[Z]            -37.702          34.039        -0.67564     -0.00089591
v  ǁVelocityǁ          0.00012143          43.012          4.2826          3.7292
v  Pressure            -2.334e+05      1.3792e+05           77322           68444
v  k                   5.9143e-07          15.381        0.050123        0.023951
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36458E+02 0.92257E+01
   Friction velocity        uet   :  0.24910E-01 0.46691E+01
   Friction velocity        uk    :  0.24843E-01 0.48345E+01
   Dimensionless distance   yplus :  0.12752E-03 0.17916E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8825
   Nb of faces within the viscous sub-layer     :      15013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33697E+01     115   0.18110E+00   0.13715E+03 0.41742E+03 
c  Velocity[X]                                      0.42663E+02 
c  Velocity[Y]                                      0.42621E+02 
c  Velocity[Z]                                      0.51870E+02 
c  Pressure     0.84015E-01     533   0.55177E-02   0.30041E+00 0.63990E+03 
c  k            0.17075E+00      72   0.70982E-02   0.34937E+00 0.11680E+04 
c  epsilon      0.46844E+04      48   0.43059E-02   0.22515E+09 0.16298E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44768E+02 0.12084E+02
   Friction velocity        uet   :  0.21484E-01 0.46748E+01
   Friction velocity        uk    :  0.20991E-01 0.48949E+01
   Dimensionless distance   yplus :  0.12757E-03 0.20017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8792
   Nb of faces within the viscous sub-layer     :      15042
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33646E+01     115   0.18110E+00   0.14635E+03 0.43485E+03 
c  Velocity[X]                                      0.45358E+02 
c  Velocity[Y]                                      0.44788E+02 
c  Velocity[Z]                                      0.56209E+02 
c  Pressure     0.82302E-01     662   0.52484E-02   0.29538E+00 0.15273E+04 
c  k            0.19728E+00      66   0.89139E-02   0.72311E+00 0.12672E+04 
c  epsilon      0.47357E+04      46   0.38622E-02   0.15816E+09 0.74105E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -4.447e-06                             2
a  epsilon         -43.735                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.28           26.54          1.4819         0.17306
v  Velocity[Y]             -18.51          21.103         0.62036         0.41599
v  Velocity[Z]            -37.702          34.039        -0.67564     -0.00089591
v  ǁVelocityǁ          0.00012143          43.012          4.2826          3.7292
v  Pressure            -2.334e+05      1.3792e+05           77322           68444
v  k                   5.9143e-07          15.381        0.050123        0.023951
v  epsilon             0.00021912      3.9849e+06          1746.5          30.628
v  TurbVisc            4.8034e-12          0.3615       0.0010747        0.013838
v  total_pressure       2.666e+05      6.3792e+05      5.7732e+05      5.6844e+05


 TIME FOR THE TIME STEP              354:        0.71048E+02

===============================================================


 INSTANT    0.355000000E+03   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         0.374705338E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41618E+02 0.93259E+01
   Friction velocity        uet   :  0.18592E-01 0.46788E+01
   Friction velocity        uk    :  0.18553E-01 0.48683E+01
   Dimensionless distance   yplus :  0.12754E-03 0.18116E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8799
   Nb of faces within the viscous sub-layer     :      15039
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33698E+01     116   0.18261E+00   0.14760E+03 0.43068E+03 
c  Velocity[X]                                      0.44259E+02 
c  Velocity[Y]                                      0.43843E+02 
c  Velocity[Z]                                      0.59500E+02 
c  Pressure     0.83739E-01    1112   0.59841E-02   0.30082E+00 0.20988E+04 
c  k            0.18216E+00      70   0.86995E-02   0.53219E+00 0.13761E+04 
c  epsilon      0.46828E+04      47   0.77018E-02   0.11318E+10 0.24648E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -9.421e-06                             2
a  epsilon         -1.3263                             6


  ** Computed fields oConvective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36640E+02 0.11521E+02
   Friction velocity        uet   :  0.23411E-01 0.46777E+01
   Friction velocity        uk    :  0.23351E-01 0.47966E+01
   Dimensionless distance   yplus :  0.12779E-03 0.18238E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8846
   Nb of faces within the viscous sub-layer     :      14955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33757E+01     115   0.17877E+00   0.13511E+03 0.42049E+03 
c  Velocity[X]                                      0.40828E+02 
c  Velocity[Y]                                      0.43507E+02 
c  Velocity[Z]                                      0.50780E+02 
c  Pressure     0.88937E-01     836   0.50702E-02   0.31737E+00 0.56382E+03 
c  k            0.17562E+00      70   0.71254E-02   0.24646E+00 0.14576E+04 
c  epsilon      0.46713E+04      48   0.80384E-02   0.25020E+10 0.36016E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36458E+02 0.92257E+01
   Friction velocity        uet   :  0.24910E-01 0.46691E+01
   Friction velocity        uk    :  0.24843E-01 0.48345E+01
   Dimensionless distance   yplus :  0.12752E-03 0.17916E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8825
   Nb of faces within the viscous sub-layer     :      15013
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33697E+01     115   0.18110E+00   0.13715E+03 0.41742E+03 
c  Velocity[X]                                      0.42663E+02 
c  Velocity[Y]                                      0.42621E+02 
c  Velocity[Z]                                      0.51870E+02 
c  Pressure     0.84015E-01     533   0.55177E-02   0.30041E+00 0.63990E+03 
c  k            0.17075E+00      72   0.70982E-02   0.34937E+00 0.11680E+04 
c  epsilon      0.46844E+04      48   0.43059E-02   0.22515E+09 0.16298E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8106e-05                             2
a  epsilon         -22.644                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.311          25.414          1.4814         0.17295
v  Velocity[Y]            -19.747          21.005         0.62486         0.41622
v  Velocity[Z]            -37.618          39.715        -0.67768     -0.00052991
v  ǁVelocityǁ          0.00012421          43.005          4.2935          3.7325
v  Pressure           -2.3268e+05       1.383e+05           77716           68765
v  k                   6.1589e-07          11.568        0.050244        0.023908
v  epsilon             0.00017214      4.0515e+06            1744          30.453
v  TurbVisc            4.8197e-12         0.25291       0.0010765        0.013839
v  total_pressure      2.6732e+05       6.383e+05      5.7772e+05      5.6877e+05


 TIME FOR THE TIME STEP              356:        0.67779E+02

===============================================================


 INSTANT    0.357000000E+03   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.146088503E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444441E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54731E+02 0.10149E+02
   Friction velocity        uet   :  0.26567E-01 0.46786E+01
   Friction velocity        uk    :  0.26493E-01 0.48155E+01
   Dimensionless distance   yplus :  0.12932E-03 0.17928E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8827
   Nb of faces within the viscous sub-layer     :      14990
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33736E+01     115   0.18053E+00   0.14064E+03 0.41876E+03 
c  Velocity[X]                                      0.41643E+02 
c  Velocity[Y]                                      0.42676E+02 
c  Velocity[Z]                                      0.56319E+02 
c  Pressure     0.87354E-01     982   0.58828E-02   0.31328E+00 0.93914E+03 
c  k            0.16825E+00      71   0.39047E-02   0.13509E+00 0.10214E+04 
c  epsilon      0.46664E+04      49   0.34774E-02   0.24392E+09 0.13084E+05 
-----------------------------------------------------------------------------
  
  

  ** 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         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39937E+02 0.11060E+02
   Friction velocity        uet   :  0.14869E-01 0.46723E+01
   Friction velocity        uk    :  0.14646E-01 0.49235E+01
   Dimensionless distance   yplus :  0.12625E-03 0.20123E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8893
   Nb of faces within the viscous sub-layer     :      14907
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33852E+01     115   0.18400E+00   0.14658E+03 0.42736E+03 
c  Velocity[X]                                      0.43883E+02 
c  Velocity[Y]                                      0.47646E+02 
c  Velocity[Z]                                      0.55050E+02 
c  Pressure     0.94850E-01     634   0.51312E-02   0.33781E+00 0.54230E+03 
c  k            0.19831E+00      65   0.60370E-02   0.19890E+00 0.99431E+03 
c  epsilon      0.47326E+04      44   0.42910E-02Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36640E+02 0.11521E+02
   Friction velocity        uet   :  0.23411E-01 0.46777E+01
   Friction velocity        uk    :  0.23351E-01 0.47966E+01
   Dimensionless distance   yplus :  0.12779E-03 0.18238E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8846
   Nb of faces within the viscous sub-layer     :      14955
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33757E+01     115   0.17877E+00   0.13511E+03 0.42049E+03 
c  Velocity[X]                                      0.40828E+02 
c  Velocity[Y]                                      0.43507E+02 
c  Velocity[Z]                                      0.50780E+02 
c  Pressure     0.88937E-01     836   0.50702E-02   0.31737E+00 0.56382E+03 
c  k            0.17562E+00      70   0.71254E-02   0.24646E+00 0.14576E+04 
c  epsilon      0.46713E+04      48   0.80384E-02   0.25020E+10 0.36016E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.2414e-06                             2
a  epsilon       -0.086907                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.457          26.121          1.4819         0.17306
v  Velocity[Y]                -19           20.89         0.62954         0.41611
v  Velocity[Z]            -40.434          36.139        -0.67608     -0.00054745
v  ǁVelocityǁ          0.00012033          45.216          4.3026           3.735
v  Pressure           -2.3335e+05      1.3919e+05           78068           69063
v  k                   6.3538e-07          12.411        0.050418        0.023926
v  epsilon             3.2058e-05      4.0113e+06          1755.7          30.559
v  TurbVisc            4.8333e-12         0.24428       0.0010775        0.013839
v  total_pressure      2.6665e+05      6.3919e+05      5.7807e+05      5.6906e+05


 TIME FOR THE TIME STEP              358:        0.72062E+02

===============================================================


 INSTANT    0.359000000E+03   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.172361529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46415E+02 0.11911E+02
   Friction velocity        uet   :  0.23338E-01 0.46844E+01
   Friction velocity        uk    :  0.23278E-01 0.48969E+01
   Dimensionless distance   yplus :  0.12693E-03 0.20492E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8868
   Nb of faces within the viscous sub-layer     :      14934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33852E+01     116   0.18691E+00   0.13816E+03 0.41866E+03 
c  Velocity[X]                                      0.41590E+02 
c  Velocity[Y]                                      0.41925E+02 
c  Velocity[Z]                                      0.54648E+02 
c  Pressure     0.93631E-01     745   0.58552E-02   0.33582E+00 0.90661E+03 
c  k            0.18920E+00      68   0.61934E-02   0.22786E+00 0.96937E+03 
c  epsilon      0.47148E+04      46   0.46822E-02   0.29870E+09 0.11849E+05 
----------------------------------------------------Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.340106213E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35931E+02 0.93555E+01
   Friction velocity        uet   :  0.22086E-01 0.46679E+01
   Friction velocity        uk    :  0.21557E-01 0.48530E+01
   Dimensionless distance   yplus :  0.12545E-03 0.19886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8923
   Nb of faces within the viscous sub-layer     :      14858
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33900E+01     114   0.17993E+00   0.14154E+03 0.42199E+03 
c  Velocity[X]                                      0.43301E+02 
c  Velocity[Y]                                      0.43288E+02 
c  Velocity[Z]                                      0.54947E+02 
c  PressureSymmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39937E+02 0.11060E+02
   Friction velocity        uet   :  0.14869E-01 0.46723E+01
   Friction velocity        uk    :  0.14646E-01 0.49235E+01
   Dimensionless distance   yplus :  0.12625E-03 0.20123E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8893
   Nb of faces within the viscous sub-layer     :      14907
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33852E+01     115   0.18400E+00   0.14658E+03 0.42736E+03 
c  Velocity[X]                                      0.43883E+02 
c  Velocity[Y]                                      0.47646E+02 
c  Velocity[Z]                                      0.55050E+02 
c  Pressure     0.94850E-01     634   0.51312E-02   0.33781E+00 0.54230E+03 
c  k            0.19831E+00      65   0.60370E-02   0.19890E+00 0.99431E+03 
c  epsilon      0.47326E+04      44   0.42910E-02   0.36043E+09 0.12766E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -8.9241e-07                             2
a  epsilon       -0.056844                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.371          26.043          1.4832         0.17314
v  Velocity[Y]            -17.355          22.792         0.63463         0.41625
v  Velocity[Z]            -40.377          56.131        -0.67258     -0.00033176
v  ǁVelocityǁ          0.00011747          58.256          4.3113           3.738
v  Pressure           -2.3551e+05      1.4006e+05           78411           69359
v  k                   6.5042e-07           13.87        0.050663        0.024004
v  epsilon             0.00013247      4.0288e+06          1759.2          30.956
v  TurbVisc             4.818e-12         0.28316       0.0010785         0.01384
v  total_pressure      2.6449e+05      6.4006e+05      5.7841e+05      5.6936e+05


 TIME FOR THE TIME STEP              360:        0.63908E+02

===============================================================


 INSTANT    0.361000000E+03   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         0.653282056E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444439E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78590E+02 0.10273E+02
   Friction velocity        uet   :  0.23700E-01 0.46969E+01
   Friction velocity        uk    :  0.23125E-01 0.49090E+01
   Dimensionless distance   yplus :  0.12534E-03 0.21227E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8900
   Nb of faces within the viscous sub-layer     :      14876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33928E+01     116   0.18453E+00   0.16929E+03 0.44047E+03 
c  Velocity[X]                                      0.44263E+02 
c  Velocity[Y]                                      0.45364E+02 
c  Velocity[Z]                                      0.79662E+02 
c  Pressure     0.86827E-01     678   0.58781E-02   0.30975E+00 0.12486E+04 
c  k            0.20291E+00      63   0.46806E-02 ---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.249000104E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444449E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35157E+02 0.11311E+02
   Friction velocity        uet   :  0.88493E-02 0.46846E+01
   Friction velocity        uk    :  0.88430E-02 0.49598E+01
   Dimensionless distance   yplus :  0.12625E-03 0.18777E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8975
   Nb of faces within the viscous sub-layer     :      14807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33995E+01     115   0.18330E+00   0.14961E+03 0.42500E+03 
c  Velocity[X]                                      0.43338E+02 
c  Velocity[Y]                           Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.340106213E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35931E+02 0.93555E+01
   Friction velocity        uet   :  0.22086E-01 0.46679E+01
   Friction velocity        uk    :  0.21557E-01 0.48530E+01
   Dimensionless distance   yplus :  0.12545E-03 0.19886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8923
   Nb of faces within the viscous sub-layer     :      14858
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33900E+01     114   0.17993E+00   0.14154E+03 0.42199E+03 
c  Velocity[X]                                      0.43301E+02 
c  Velocity[Y]                                      0.43288E+02 
c  Velocity[Z]                                      0.54947E+02 
c  Pressure     0.86559E-01     736   0.47457E-02   0.30711E+00 0.12206E+04 
c  k            0.20099E+00      64   0.46341E-02   0.11696E+00 0.91265E+03 
c  epsilon      0.47421E+04      40   0.66137E-02   0.93675E+09 0.21991E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.27887                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.428          25.529          1.4847         0.17317
v  Velocity[Y]             -18.79          20.579         0.63895         0.41623
v  Velocity[Z]            -43.359          37.495         -0.6687     -0.00036055
v  ǁVelocityǁ          0.00012141          48.534           4.318          3.7402
v  Pressure           -2.3747e+05      1.4051e+05           78675           69557
v  k                   4.7577e-07          14.272        0.050813        0.024045
v  epsilon             0.00012051      4.0593e+06          1759.5          31.186
v  TurbVisc            4.8345e-12         0.30797       0.0010792        ---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.249000104E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444449E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35157E+02 0.11311E+02
   Friction velocity        uet   :  0.88493E-02 0.46846E+01
   Friction velocity        uk    :  0.88430E-02 0.49598E+01
   Dimensionless distance   yplus :  0.12625E-03 0.18777E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8975
   Nb of faces within the viscous sub-layer     :      14807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33995E+01     115   0.18330E+00   0.14961E+03 0.42500E+03 
c  Velocity[X]                                      0.43338E+02 
c  Velocity[Y]                                      0.45866E+02 
c  Velocity[Z]                                      0.60402E+02 
c  Pressure     0.91164E-01     643   0.47771E-02   0.32063E+00 0.89143E+03 
c  k            0.20534E+00      67   0.70625E-02   0.35141E+00 0.11273E+04 
c  epsilon      0.48039E+04      44   0.43240E-02   0.98750E+09 0.20607E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.220471326E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38516E+02 0.94395E+01
   Friction velocity        uet   :  0.29725E-01 0.46585E+01
   Friction velocity        uk    :  0.28928E-01 0.48938E+01
   Dimensionless distance   yplus :  0.12526E-03 0.19269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8994
   Nb of faces within the viscous sub-layer     :      14759
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34036E+01     115   0.18784E+00   0.14420E+03 0.42376E+---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.249000104E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444449E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35157E+02 0.11311E+02
   Friction velocity        uet   :  0.88493E-02 0.46846E+01
   Friction velocity        uk    :  0.88430E-02 0.49598E+01
   Dimensionless distance   yplus :  0.12625E-03 0.18777E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8975
   Nb of faces within the viscous sub-layer     :      14807
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33995E+01     115   0.18330E+00   0.14961E+03 0.42500E+03 
c  Velocity[X]                                      0.43338E+02 
c  Velocity[Y]                                      0.45866E+02 
c  Velocity[Z]                                      0.60402E+02 
c  Pressure     0.91164E-01     643   0.47771E-02   0.32063E+00 0.89143E+03 
c  k            0.20534E+00      67   0.70625E-02   0.35141E+00 0.11273E+04 
c  epsilon      0.48039E+04      44   0.43240E-02   0.98750E+09 0.20607E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -2.9187                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.408          26.062          1.4856         0.17301
v  Velocity[Y]            -17.811          22.842         0.64189         0.41631
v  Velocity[Z]            -44.987          51.077        -0.66493     -0.00025081
v  ǁVelocityǁ          0.00011697          53.477          4.3244          3.7425
v  Pressure           -2.3984e+05      1.4093e+05           78954           69758
v  k                   1.5853e-07          16.567        0.051073         0.02409
v  epsilon             0.00018396      4.3263e+06            1788          31---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.220471326E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38516E+02 0.94395E+01
   Friction velocity        uet   :  0.29725E-01 0.46585E+01
   Friction velocity        uk    :  0.28928E-01 0.48938E+01
   Dimensionless distance   yplus :  0.12526E-03 0.19269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8994
   Nb of faces within the viscous sub-layer     :      14759
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34036E+01     115   0.18784E+00   0.14420E+03 0.42376E+03 
c  Velocity[X]                                      0.43366E+02 
c  Velocity[Y]                                      0.45737E+02 
c  Velocity[Z]                                      0.55102E+02 
c  Pressure     0.87466E-01     756   0.50072E-02   0.30750E+00 0.38268E+03 
c  k            0.21339E+00      68   0.47004E-02   0.18067E+00 0.93939E+03 
c  epsilon      0.47962E+04      46   0.52708E-02   0.55407E+09 0.14787E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.196603748E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444440E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40156E+02 0.91402E+01
   Friction velocity        uet   :  0.28449E-01 0.46486E+01
   Friction velocity        uk    :  0.27766E-01 0.49441E+01
   Dimensionless distance   yplus :  0.12594E-03 0.19313E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9026
   Nb of faces within the viscous sub-layer     :      14740
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      de---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.220471326E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38516E+02 0.94395E+01
   Friction velocity        uet   :  0.29725E-01 0.46585E+01
   Friction velocity        uk    :  0.28928E-01 0.48938E+01
   Dimensionless distance   yplus :  0.12526E-03 0.19269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8994
   Nb of faces within the viscous sub-layer     :      14759
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34036E+01     115   0.18784E+00   0.14420E+03 0.42376E+03 
c  Velocity[X]                                      0.43366E+02 
c  Velocity[Y]                                      0.45737E+02 
c  Velocity[Z]                                      0.55102E+02 
c  Pressure     0.87466E-01     756   0.50072E-02   0.30750E+00 0.38268E+03 
c  k            0.21339E+00      68   0.47004E-02   0.18067E+00 0.93939E+03 
c  epsilon      0.47962E+04      46   0.52708E-02   0.55407E+09 0.14787E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -6.625e-06                             2
a  epsilon        -0.51729                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.408          24.726           1.487         0.17317
v  Velocity[Y]            -18.071          20.506         0.64437         0.41629
v  Velocity[Z]            -44.642          43.986        -0.66312     -0.00037222
v  ǁVelocityǁ          0.00011803          49.461          4.3312           3.744
v  Pressure           -2.4142e+05      1.4137e+05           79166           69893
v  k                   4.5409e-09          18.188        0.051247        0.024124
v  epsilon             8.7642e-06      4.3895e+06          1786.9          31.591
v  TurbVisc            4.8483e-12         0.36248       0.0010799        0.013843
v  total_pressure      2.5858e+05      6.4137e+05      5.7917e+05      5.6989e+05


 TIME FOR THE TIME STEP              366:        0.74468E+02

===============================================================


 INSTANT    0.367000000E+03   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.278288319E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.65055E+02 0.10075E+02
   Friction velocity        uet   :  0.22071E-01 0.46859E+01
   Friction velocity        uk    :  0.21560E-01 0.48873E+01
   Dimensionless distance   yplus :  0.12542E-03 0.19133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9007
   Nb of faces within the viscous sub-layer     :      14745
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34094E+01     1 TIME FOR THE TIME STEP              369:        0.68828E+02

===============================================================


 INSTANT    0.370000000E+03   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.387290106E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444441E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33729E+02 0.92781E+01
   Friction velocity        uet   :  0.20173E-01 0.46846E+01
   Friction velocity        uk    :  0.20165E-01 0.49308E+01
   Dimensionless distance   yplus :  0.12709E-03 0.18909E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9035
   Nb of faces within the viscous sub-layer     :      14737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.196603748E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444440E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40156E+02 0.91402E+01
   Friction velocity        uet   :  0.28449E-01 0.46486E+01
   Friction velocity        uk    :  0.27766E-01 0.49441E+01
   Dimensionless distance   yplus :  0.12594E-03 0.19313E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9026
   Nb of faces within the viscous sub-layer     :      14740
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34072E+01     116   0.18417E+00   0.14658E+03 0.42647E+03 
c  Velocity[X]                                      0.41235E+02 
c  Velocity[Y]                                      0.48200E+02 
c  Velocity[Z]                                      0.57145E+02 
c  Pressure     0.83332E-01     689   0.51695E-02   0.29268E+00 0.38235E+03 
c  k            0.21838E+00      66   0.31435E-02   0.93473E-01 0.71858E+03 
c  epsilon      0.48723E+04      46   0.36184E-02   0.24065E+09 0.10354E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.2271e-06                             4
a  epsilon        -0.51945                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.371          25.297          1.4885         0.17283
v  Velocity[Y]            -18.598          20.677         0.64504         0.41628
v  Velocity[Z]            -45.074           34.76        -0.66444     -0.00064015
v  ǁVelocityǁ          0.00012215          49.995          4.3371          3.7451
v  Pressure           -2.4215e+05      1.4097e+05           79115           69843
v  k                   1.2466e-07          18.415        0.051466        0.024127
v  epsilon             6.1983e-07      4.3795e+06          1808.9          31.713
v  TurbVisc            4.8669e-12         0.36331       0.0010794        0.013843
v  total_pressure      2.5785e+05      6.4097e+05      5.7911e+05      5.6984e+05


 TIME FOR THE TIME STEP              368:        0.64719E+02

===============================================================


 INSTANT    0.369000000E+03   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        -0.128888025E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444439E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44044E+02 0.93428E+01
   Friction velocity        uet   :  0.30351E-01 0.46541E+01
   Friction velocity        uk    :  0.30342E-01 0.49461E+01
   Dimensionless distance   yplus :  0.12796E-03 0.19234E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9017
   Nb of faces within the viscous sub-layer     :      14729
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs normv  TurbVisc            4.8661e-12         0.33064       0.0010779        0.013841
v  total_pressure      2.5937e+05      6.4147e+05      5.7952e+05      5.7017e+05


 TIME FOR THE TIME STEP              371:        0.63454E+02

===============================================================


 INSTANT    0.372000000E+03   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        -0.147739778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46543E+02 0.12280E+02
   Friction velocity        uet   :  0.24183E-01 0.46747E+01
   Friction velocity        uk    :  0.26284E-01 0.48974E+01
   Dimensionless distance   yplus :  0.12606E-03 0.21112E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9063
   Nb of faces within the viscous sub-layer     :       TIME FOR THE TIME STEP              369:        0.67550E+02

===============================================================


 INSTANT    0.370000000E+03   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.387290106E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444441E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33729E+02 0.92781E+01
   Friction velocity        uet   :  0.20173E-01 0.46846E+01
   Friction velocity        uk    :  0.20165E-01 0.49308E+01
   Dimensionless distance   yplus :  0.12709E-03 0.18909E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9035
   Nb of faces within the viscous sub-layer     :      14737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34067E+01     115   0.18034E+00   0.13621E+03 0.41306E+03 
c  Velocity[X]                                      0.40948E+02 
c  Velocity[Y]                                      0.45095E+02 
c  Velocity[Z]                                      0.50164E+02 
c  Pressure     0.86982E-01     496   0.51920E-02   0.30450E+00 0.69669E+03 
c  k            0.21008E+00      63   0.48663E-02   0.12492E+00 0.11618E+04 
c  epsilon      0.48408E+04      43   0.76985E-02   0.14906E+10 0.26234E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.9902e-05                             4
a  epsilon        -0.40217                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.426           25.84          1.4901      v  TurbVisc            4.8661e-12         0.33064       0.0010779        0.013841
v  total_pressure      2.5937e+05      6.4147e+05      5.7952e+05      5.7017e+05


 TIME FOR THE TIME STEP              371:        0.68084E+02

===============================================================


 INSTANT    0.372000000E+03   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        -0.147739778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46543E+02 0.12280E+02
   Friction velocity        uet   :  0.24183E-01 0.46747E+01
   Friction velocity        uk    :  0.26284E-01 0.48974E+01
   Dimensionless distance   yplus :  0.12606E-03 0.21112E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9063
   Nb of faces within the viscous sub-layer     :      14709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34099E+01     113   0.18488E+00   0.14730E+03 0.43028E+03 
c  Velocity[X]                                      0.43581E+02 
c  Velocity[Y]                                      0.48083E+02 
cv  k                   2.5163e-07          18.051         0.05173        0.024138
v  epsilon             0.00041124      4.3744e+06          1821.5          31.778
v  TurbVisc            4.8777e-12         0.33234       0.0010793        0.013842
v  total_pressure      2.6214e+05       6.417e+05      5.7959e+05      5.7024e+05


 TIME FOR THE TIME STEP              373:        0.75157E+02

===============================================================


 INSTANT    0.374000000E+03   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         0.202175675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39464E+02 0.14084E+02
   Friction velocity        uet   :  0.27796E-01 0.46815E+01
   Friction velocity        uk    :  0.29377E-01 0.49681E+01
   Dimensionless distance   yplus :  0.12568E-03 0.22827E+02
   -----v  TurbVisc            4.8661e-12         0.33064       0.0010779        0.013841
v  total_pressure      2.5937e+05      6.4147e+05      5.7952e+05      5.7017e+05


 TIME FOR THE TIME STEP              371:        0.64270E+02

===============================================================


 INSTANT    0.372000000E+03   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        -0.147739778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46543E+02 0.12280E+02
   Friction velocity        uet   :  0.24183E-01 0.46747E+01
   Friction velocity        uk    :  0.26284E-01 0.48974E+01
   Dimensionless distance   yplus :  0.12606E-03 0.21112E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9063
   Nb of faces within the viscous sub-layer     :      14709
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34099E+01     113   0.18488E+00   0.14730E+03 0.43028E+03 
c  Velocity[X]                                      0.43581E+02 
c  Velocity[Y]                                      0.48083E+02 
c  Velocity[Z]                                      0.55635E+02 
c  Pressure     0.80371E-01     656   0.43213E-02   0.28106E+00 0.72445E+03 
c  k            0.20902E+00      59   0.36427E-02   0.88282E-01 0.10552E+04 
c  epsilon      0.48612E+04      40   0.69923E-02   0.17348E+10 0.29418E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.2327e-05                             3
a  epsilon         -1.7961                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spv  k                   2.5163e-07          18.051         0.05173        0.024138
v  epsilon             0.00041124      4.3744e+06          1821.5          31.778
v  TurbVisc            4.8777e-12         0.33234       0.0010793        0.013842
v  total_pressure      2.6214e+05       6.417e+05      5.7959e+05      5.7024e+05


 TIME FOR THE TIME STEP              373:        0.77411E+02

===============================================================


 INSTANT    0.374000000E+03   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         0.202175675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39464E+02 0.14084E+02
   Friction velocity        uet   :  0.27796E-01 0.46815E+01
   Friction velocity        uk    :  0.29377E-01 0.49681E+01
   Dimensionless distance   yplus :  0.12568E-03 0.22827E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9082
   Nb of faces within the viscous sub-layer     :      14697
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34111E+01     114   0.18v  ǁVelocityǁ          0.00011806          43.632          4.3536          3.7498
v  Pressure           -2.3568e+05      1.4212e+05           79683           70321
v  k                    9.202e-07          18.199        0.051862        0.024164
v  epsilon              0.0010803      4.3758e+06            1827          31.906
v  TurbVisc            4.8758e-12         0.34328       0.0010807        0.013844
v  total_pressure      2.6432e+05      6.4212e+05      5.7968e+05      5.7032e+05


 TIME FOR THE TIME STEP              375:        0.69778E+02

===============================================================


 INSTANT    0.376000000E+03   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.281693664E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55509E+02 0.10194E+02
   Friction velocity       v  k                   2.5163e-07          18.051         0.05173        0.024138
v  epsilon             0.00041124      4.3744e+06          1821.5          31.778
v  TurbVisc            4.8777e-12         0.33234       0.0010793        0.013842
v  total_pressure      2.6214e+05       6.417e+05      5.7959e+05      5.7024e+05


 TIME FOR THE TIME STEP              373:        0.70565E+02

===============================================================


 INSTANT    0.374000000E+03   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         0.202175675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444455E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39464E+02 0.14084E+02
   Friction velocity        uet   :  0.27796E-01 0.46815E+01
   Friction velocity        uk    :  0.29377E-01 0.49681E+01
   Dimensionless distance   yplus :  0.12568E-03 0.22827E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9082
   Nb of faces within the viscous sub-layer     :      14697
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34111E+01     114   0.18429E+00   0.13332E+03 0.40963E+03 
c  Velocity[X]                                      0.40765E+02 
c  Velocity[Y]                                      0.43421E+02 
c  Velocity[Z]                                      0.49136E+02 
c  Pressure     0.92120E-01     623   0.43895E-02   0.32179E+00 0.79003E+03 
c  k            0.21338E+00      58   0.58001E-02   0.17425E+00 0.89149E+03 
c  epsilon      0.49118E+04      43   0.39220E-02   0.28367E+09 0.92212E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.1276e-05                             3
a  epsilon        -0.22161                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.212          24.633          1.4959         0.17252
v  Velocity[Y]            -18.563          27.288         0.64028         0.41708
v  Velocity[Z]            -38.172          51.139        -0.66853     -0.00050041
v  ǁVelocityǁ          0.00012078          53.129          4.3533          3.7496
v  Pressure           -2.3717e+05       1.419e+05           79603           70249
v  k                   8.8677e-07          18.081        0.051813        0.024144
v  epsilon              0.0005346      4.4143e+06          1827.9          31.833
v  TurbVisc            4.8695e-12         0.34377       0.0010802        0.013843
v  total_pressure      2.6283e+05       6.419e+05       5.796e+05      5.7025e+05


 TIME FOR THE TIME STEP              374:        0.67245E+02

===============================================================


 INSTANT    0.375000000E+03   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        -0.145886606E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76014E+02 0.10653E+02
   Friction velocity        uet   :  0.32367E-01 0.46913E+01
   Friction velocity        uk    :  0.41120E-01 0.49209E+01
   Dimensionless distance   yplus :  0.v  Velocity[Y]            -18.913          21.756         0.63841         0.41735
v  Velocity[Z]            -36.813          33.804        -0.66802     -0.00067187
v  ǁVelocityǁ          0.00011741          43.196          4.3552          3.7514
v  Pressure           -2.3425e+05      1.4253e+05           79887           70492
v  k                   9.7876e-07          15.748        0.051895        0.024161
v  epsilon             0.00081882      4.3783e+06          1835.6          31.877
v  TurbVisc            4.8476e-12         0.34635        0.001083        0.013845
v  total_pressure      2.6575e+05      6.4253e+05      5.7989e+05      5.7049e+05


 TIME FOR THE TIME STEP              377:        0.63850E+02

===============================================================


 INSTANT    0.378000000E+03   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        -0.225916506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minv  ǁVelocityǁ          0.00011806          43.632          4.3536          3.7498
v  Pressure           -2.3568e+05      1.4212e+05           79683           70321
v  k                    9.202e-07          18.199        0.051862        0.024164
v  epsilon              0.0010803      4.3758e+06            1827          31.906
v  TurbVisc            4.8758e-12         0.34328       0.0010807        0.013844
v  total_pressure      2.6432e+05      6.4212e+05      5.7968e+05      5.7032e+05


 TIME FOR THE TIME STEP              375:        0.73824E+02

===============================================================


 INSTANT    0.376000000E+03   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.281693664E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55509E+02 0.10194E+02
   Friction velocity        uet   :  0.20481E-01 0.46843E+01
   Friction velocity        uk    :  0.20450E-01 0.49555E+01
   Dimensionless distance   yplus :  0.12629E-03 0.21477E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9097
   Nb of faces within the viscous sub-layer     :      14663
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34106E+01     114   0.18282E+00   0.14878E+03 0.42458E+03 
c  Velocity[X]                                      0.43004E+02 
c  Velocity[Y]                                      0.45249E+02 
c  Velocity[Z]                                      0.60523E+02 
c  Pressure     0.83695E-01     602   0.52275E-02   0.29234E+00 0.95405E+02 
c  k            0.21384E+00      59   0.70509E-02   0.19856E+00 0.76574E+03 
c  epsilon      0.49021E+04      40   0.45420E-02   0.19945E+09 0.70044E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clv  Velocity[Y]            -18.913          21.756         0.63841         0.41735
v  Velocity[Z]            -36.813          33.804        -0.66802     -0.00067187
v  ǁVelocityǁ          0.00011741          43.196          4.3552          3.7514
v  Pressure           -2.3425e+05      1.4253e+05           79887           70492
v  k                   9.7876e-07          15.748        0.051895        0.024161
v  epsilon             0.00081882      4.3783e+06          1835.6          31.877
v  TurbVisc            4.8476e-12         0.34635        0.001083        0.013845
v  total_pressure      2.6575e+05      6.4253e+05      5.7989e+05      5.7049e+05


 TIME FOR THE TIME STEP              377:        0.68094E+02

===============================================================


 INSTANT    0.378000000E+03   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        -0.225916506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34431E+02 0.92494E+01
   Friction velocity        uet   :  0.32907E-01 0.46941E+01
   Friction velocity        uk    :  0.31942E-01 0.49496E+01
   Dimensionless distance   yplus :  0.12559E-03 0.19001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9094
   Nb of faces within the viscous sub-layer     :      14654
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMAT-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.331          25.339          1.5018         0.17207
v  Velocity[Y]            -21.447          21.962         0.63811         0.41721
v  Velocity[Z]            -41.647           35.42        -0.66852     -0.00042118
v  ǁVelocityǁ          0.00011612          45.883          4.3566          3.7529
v  Pressure           -2.3502e+05      1.4323e+05           80070           70657
v  k                   1.0298e-06          12.339        0.051793        0.024105
v  epsilon             0.00094936      4.3908e+06          1819.3           31.62
v  TurbVisc            4.8392e-12         0.26197       0.0010836        0.013844
v  total_pressure      2.6498e+05      6.4323e+05      5.8007e+05      5.7066e+05


 TIME FOR THE TIME STEP              379:        0.67173E+02

===============================================================


 INSTANT    0.380000000E+03   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        -0.110606259E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS Fv  Velocity[Y]            -18.913          21.756         0.63841         0.41735
v  Velocity[Z]            -36.813          33.804        -0.66802     -0.00067187
v  ǁVelocityǁ          0.00011741          43.196          4.3552          3.7514
v  Pressure           -2.3425e+05      1.4253e+05           79887           70492
v  k                   9.7876e-07          15.748        0.051895        0.024161
v  epsilon             0.00081882      4.3783e+06          1835.6          31.877
v  TurbVisc            4.8476e-12         0.34635        0.001083        0.013845
v  total_pressure      2.6575e+05      6.4253e+05      5.7989e+05      5.7049e+05


 TIME FOR THE TIME STEP              377:        0.70031E+02

===============================================================


 INSTANT    0.378000000E+03   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        -0.225916506E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444450E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34431E+02 0.92494E+01
   Friction velocity        uet   :  0.32907E-01 0.46941E+01
   Friction velocity        uk    :  0.31942E-01 0.49496E+01
   Dimensionless distance   yplus :  0.12559E-03 0.19001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9094
   Nb of faces within the viscous sub-layer     :      14654
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34137E+01     111   0.18342E+00   0.13651E+03 0.41365E+03 
c  Velocity[X]                                      0.40971E+02 
c  Velocity[Y]                                      0.44717E+02 
c  Velocity[Z]                                      0.50822E+02 
c  Pressure     0.82928E-01     771   0.50067E-02   0.28680E+00 0.28478E+03 
c  k            0.19072E+00      66   0.79133E-02   0.37427E+00 0.12736E+04 
c  epsilon      0.48670E+04      42   0.79538E-02   0.13495E+10 0.25435E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.9983e-05                             3
a  epsilon        -0.31734                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.231          26.539          1.5012         0.17202
v  Velocity[Y]            -19.115           20.86         0.63806         0.41726
v  Velocity[Z]            -37.654          44.667        -0.66794     -0.00036917
v  ǁVelocityǁ          0.00011702          46.564          4.3564          3.7524
v  Pressure           -2.3507e+05      1.4292e+05           79965           70556
v  k                   1.0047e-06          13.476        0.051817        0.024122
v  epsilon             8.9571e-05      4.4119e+06          1824.9          31.714
v  TurbVisc            4.8448e-12         0.29964       0.0010837        0.013845
v  total_pressure      2.6493e+05      6.4292e+05      5.7997e+05      5.7056e+05


 TIME FOR THE TIME STEP              378:        0.70306E+02

===============================================================


 INSTANT    0.379000000E+03   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         0.214578262E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                    
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.201          25.065          1.5034         0.17209
v  Velocity[Y]             -19.22          20.578         0.63767         0.41714
v  Velocity[Z]            -36.121          33.791        -0.67034     -0.00047997
v  ǁVelocityǁ          0.00011926          43.064          4.3589          3.7546
v  Pressure           -2.3795e+05      1.4343e+05           80134           70732
v  k                    1.073e-06          12.072        0.051838          0.0241
v  epsilon             0.00093044       4.383e+06          1827.7          31.577
v  TurbVisc            4.8686e-12         0.24312       0.0010842        0.013843
v  total_pressure      2.6205e+05      6.4343e+05      5.8013e+05      5.7073e+05


 TIME FOR THE TIME STEP              381:        0.73133E+02

===============================================================


 INSTANT    0.382000000E+03   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         0.226067584E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.0000000-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.331          25.339          1.5018         0.17207
v  Velocity[Y]            -21.447          21.962         0.63811         0.41721
v  Velocity[Z]            -41.647           35.42        -0.66852     -0.00042118
v  ǁVelocityǁ          0.00011612          45.883          4.3566          3.7529
v  Pressure           -2.3502e+05      1.4323e+05           80070           70657
v  k                   1.0298e-06          12.339        0.051793        0.024105
v  epsilon             0.00094936      4.3908e+06          1819.3           31.62
v  TurbVisc            4.8392e-12         0.26197       0.0010836        0.013844
v  total_pressure      2.6498e+05      6.4323e+05      5.8007e+05      5.7066e+05


 TIME FOR THE TIME STEP              379:        0.76076E+02

===============================================================


 INSTANT    0.380000000E+03   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        -0.110606259E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36585E+02 0.10457E+02
   Friction velocity        uet   :  0.34108E-01 0.46936E+01
   Friction velocity        uk    :  0.34908E-01 0.48913E+01
   Dimensionless distance   yplus :  0.12480E-03 0.18366E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9086
   Nb of faces within the viscous sub-layer     :      14617
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34153E+01     114   0.18359E+00   0.14302E+03 0.42464E+03 
c  Velocity[X]                                      0.43393E+02 
c  Velocity[Y]                                      0.44917E+02 
c  Velocity[Z]                                      0.54705E+02 
c  Pressure     0.81338E-01     767   0.47741E-02   0.28253E+00 0.30163E+03 
c  k            0.17393E+00      69   0.60900E-02   0.17271E+00 0.11599E+04 
c  epsilon      0.48332E+04      47   0.64974E-02   0.13963E+10 0.26928E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.3945e-05                             3
a  epsilon        -0.38648                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.17           25.42          1.5025         0.17216
v  Velocity[Y]            -18.828           20.63         0.63794         0.41706
v  Velocity[Z]            -40.779          40.547        -0.66966     -0.00064862
v  ǁVelocityǁ          0.00012074          45.939          4.3578           3.754
v  Pressure           -2.3721e+05      1.4341e+05           80060           70661
v  k                   1.0538e-06          11.796        0.051822        0.024086
v  epsilon              0.0010878      4.3615e+06          1828.3          31.548
v  TurbVisc             4.853e-12         0.24687       0.0010841        0.013844
v  total_pressure      2.6279e+05      6.4341e+05      5.8006e+05      5.7066e+05


 TIME FOR THE TIME STEP              380:        0.76489E+02

===============================================================


 INSTANT    0.381000000E+03   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.496527262E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------------------------------------------  -------  --------------  --------------  ------------  ------------
a  k           -5.1417e-05                             3
a  epsilon        -0.41512                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.651          25.453          1.5045         0.17211
v  Velocity[Y]            -18.125           20.34         0.63672         0.41717
v  Velocity[Z]            -37.765          33.776         -0.6717     -0.00056508
v  ǁVelocityǁ          0.00011738          42.812          4.3603           3.756
v  Pressure           -2.4206e+05      1.4372e+05           80069           70696
v  k                   1.0974e-06           13.08        0.051909        0.024152
v  epsilon             0.00068817      4.3847e+06          1826.7          31.805
v  TurbVisc            4.8389e-12         0.27306       0.0010849        0.013844
v  total_pressure      2.5794e+05      6.4372e+05      5.8007e+05       5.707e+05


 TIME FOR THE TIME STEP              383:        0.72507E+02

===============================================================


 INSTANT    0.384000000E+03   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         0.709112692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0  
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.201          25.065          1.5034         0.17209
v  Velocity[Y]             -19.22          20.578         0.63767         0.41714
v  Velocity[Z]            -36.121          33.791        -0.67034     -0.00047997
v  ǁVelocityǁ          0.00011926          43.064          4.3589          3.7546
v  Pressure           -2.3795e+05      1.4343e+05           80134           70732
v  k                    1.073e-06          12.072        0.051838          0.0241
v  epsilon             0.00093044       4.383e+06          1827.7          31.577
v  TurbVisc            4.8686e-12         0.24312       0.0010842        0.013843
v  total_pressure      2.6205e+05      6.4343e+05      5.8013e+05      5.7073e+05


 TIME FOR THE TIME STEP              381:        0.71128E+02

===============================================================


 INSTANT    0.382000000E+03   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         0.226067584E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32300E+02 0.97842E+01
   Friction velocity        uet   :  0.17451E-01 0.46802E+01
   Friction velocity        uk    :  0.17118E-01 0.49679E+01
   Dimensionless distance   yplus :  0.12675E-03 0.18108E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9107
   Nb of faces within the viscous sub-layer     :      14598
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34103E+01     113   0.17879E+00   0.14027E+03 0.41615E+03 
c  Velocity[X]                                      0.43900E+02 
c  Velocity[Y]                                      0.44029E+02 
c  Velocity[Z]                                      0.52341E+02 
c  Pressure     0.82890E-01     609   0.52750E-02   0.28871E+00 0.91845E+03 
c  k            0.18213E+00      66   0.56325E-02   0.17593E+00 0.78621E+03 
c  epsilon      0.48574E+04      45   0.27887E-02   0.11311E+09 0.74860E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010478                             3
a  epsilon        -0.38024                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.54          26.346          1.5041         0.17213
v  Velocity[Y]            -18.863          20.768         0.63714         0.41705
v  Velocity[Z]            -45.104          35.254        -0.67112     -0.00054205
v  ǁVelocityǁ           0.0001187          51.859          4.3601           3.755
v  Pressure           -2.4046e+05      1.4356e+05           79985           70630
v  k                   1.0864e-06          12.719        0.051892        0.024124
v  epsilon             0.00096376      4.4028e+06          1828.6          31.688
v  TurbVisc            4.8495e-12         0.25513       0.0010846        0.013843
v  total_pressure      2.5954e+05      6.4356e+05      5.7999e+05      5.7063e+05


 TIME FOR THE TIME STEP              382:        0.67012E+02

===============================================================


 INSTANT    0.383000000E+03   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        -0.248725797E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444451E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.0105e-05                             2
a  epsilon         -0.3893                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.579          25.068          1.5047         0.17208
v  Velocity[Y]            -17.772          20.737          0.6349         0.41672
v  Velocity[Z]            -37.892          33.924        -0.67217     -0.00032549
v  ǁVelocityǁ          0.00011909          43.326          4.3613           3.757
v  Pressure           -2.4751e+05      1.4344e+05           79836           70564
v  k                   5.8344e-07          13.257        0.051978        0.024196
v  epsilon             0.00020107      4.3717e+06          1828.5          32.027
v  TurbVisc            4.8506e-12          0.2844       0.0010842        0.013844
v  total_pressure      2.5249e+05      6.4344e+05      5.7984e+05      5.7056e+05


 TIME FOR THE TIME STEP              385:        0.67784E+02

===============================================================


 INSTANT    0.386000000E+03   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.196738275E-17
Rough wall                6           0        -  -------  --------------  --------------  ------------  ------------
a  k           -5.1417e-05                             3
a  epsilon        -0.41512                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.651          25.453          1.5045         0.17211
v  Velocity[Y]            -18.125           20.34         0.63672         0.41717
v  Velocity[Z]            -37.765          33.776         -0.6717     -0.00056508
v  ǁVelocityǁ          0.00011738          42.812          4.3603           3.756
v  Pressure           -2.4206e+05      1.4372e+05           80069           70696
v  k                   1.0974e-06           13.08        0.051909        0.024152
v  epsilon             0.00068817      4.3847e+06          1826.7          31.805
v  TurbVisc            4.8389e-12         0.27306       0.0010849        0.013844
v  total_pressure      2.5794e+05      6.4372e+05      5.8007e+05       5.707e+05


 TIME FOR THE TIME STEP              383:        0.69400E+02

===============================================================


 INSTANT    0.384000000E+03   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         0.709112692E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444453E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36147E+02 0.11083E+02
   Friction velocity        uet   :  0.17074E-01 0.46937E+01
   Friction velocity        uk    :  0.21982E-01 0.49386E+01
   Dimensionless distance   yplus :  0.12560E-03 0.17987E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9109
   Nb of faces within the viscous sub-layer     :      14596
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34162E+01     112   0.18810E+00   0.13777E+03 0.41671E+03 
c  Velocity[X]                                      0.43036E+02 
c  Velocity[Y]                                      0.43937E+02 
c  Velocity[Z]                                      0.50794E+02 
c  Pressure     0.89073E-01     715   0.47680E-02   0.30771E+00 0.14416E+04 
c  k            0.20101E+00      61   0.58921E-02   0.20189E+00 0.79146E+03 
c  epsilon      0.48732E+04      43   0.33592E-02   0.17729E+09 0.73688E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.0646e-05                             3
a  epsilon        -0.46606                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.216          26.095          1.5049         0.17229
v  Velocity[Y]            -18.528           20.78          0.6359         0.41688
v  Velocity[Z]            -47.413          34.102        -0.67218      -0.0005241
v  ǁVelocityǁ          0.00011765          54.415          4.3611          3.7565
v  Pressure           -2.4569e+05      1.4365e+05           79964           70640
v  k                   1.1068e-06          13.246        0.051934        0.024176
v  epsilon             0.00054606      4.3852e+06          1827.1          31.914
v  TurbVisc            4.8452e-12         0.28186       0.0010847        0.013844
v  total_pressure      2.5431e+05      6.4365e+05      5.7996e+05      5.7064e+05


 TIME FOR THE TIME STEP              384:        0.66888E+02

===============================================================


 INSTANT    0.385000000E+03   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        -0.536748826E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet     c  epsilon      0.48525E+04      41   0.34342E-02   0.10325E+09 0.67345E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6171e-05                             2
a  epsilon        -0.56988                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.771          25.068          1.5038         0.17245
v  Velocity[Y]            -17.743          22.709         0.63309         0.41682
v  Velocity[Z]            -34.597          34.073        -0.67226     -0.00054386
v  ǁVelocityǁ          0.00011991          43.422          4.3617          3.7583
v  Pressure           -2.5215e+05      1.4338e+05           79807           70544
v  k                   6.9412e-07          13.078        0.051841        0.024177
v  epsilon             6.4689e-05       4.371e+06          1812.1          31.941
v  TurbVisc            4.8768e-12         0.27896       0.0010826        0.013845
v  total_pressure      2.4785e+05      6.4338e+05      5.7981e+05      5.7054e+05


 TIME FOR THE TIME STEP              387:        0.67020E+02

===============================================================


 INSTANT    0.388000000E+03   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2     
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.0105e-05                             2
a  epsilon         -0.3893                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.579          25.068          1.5047         0.17208
v  Velocity[Y]            -17.772          20.737          0.6349         0.41672
v  Velocity[Z]            -37.892          33.924        -0.67217     -0.00032549
v  ǁVelocityǁ          0.00011909          43.326          4.3613           3.757
v  Pressure           -2.4751e+05      1.4344e+05           79836           70564
v  k                   5.8344e-07          13.257        0.051978        0.024196
v  epsilon             0.00020107      4.3717e+06          1828.5          32.027
v  TurbVisc            4.8506e-12          0.2844       0.0010842        0.013844
v  total_pressure      2.5249e+05      6.4344e+05      5.7984e+05      5.7056e+05


 TIME FOR THE TIME STEP              385:        0.59188E+02

===============================================================


 INSTANT    0.386000000E+03   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.196738275E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444452E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32455E+02 0.10964E+02
   Friction velocity        uet   :  0.28907E-01 0.46862E+01
   Friction velocity        uk    :  0.28061E-01 0.49259E+01
   Dimensionless distance   yplus :  0.12624E-03 0.20238E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9117
   Nb of faces within the viscous sub-layer     :      14602
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34118E+01     114   0.18189E+00   0.14747E+03 0.42359E+03 
c  Velocity[X]                                      0.43450E+02 
c  Velocity[Y]                                      0.46878E+02 
c  Velocity[Z]                                      0.57145E+02 
c  Pressure     0.95196E-01     554   0.54777E-02   0.32868E+00 0.29236E+03 
c  k            0.20464E+00      59   0.44551E-02   0.13716E+00 0.10600E+04 
c  epsilon      0.48625E+04      39   0.71166E-02   0.12658E+10 0.24780E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011166                             2
a  epsilon         -0.5865                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.908          25.234          1.5043         0.17239
v  Velocity[Y]            -19.066          20.456         0.63405         0.41684
v  Velocity[Z]            -42.347          33.841        -0.67227     -0.00049369
v  ǁVelocityǁ           0.0001226          47.883          4.3617          3.7583
v  Pressure           -2.5085e+05      1.4344e+05           79823           70549
v  k                   1.7771e-07          13.068        0.051925        0.024193
v  epsilon              0.0001352      4.3863e+06          1820.1          31.998
v  TurbVisc            4.8544e-12         0.28344       0.0010837        0.013845
v  total_pressure      2.4915e+05      6.4344e+05      5.7982e+05      5.7055e+05


 TIME FOR THE TIME STEP              386:        0.65524E+02

===============================================================


 INSTANT    0.387000000E+03   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         0.329461970E-17
Rough wall                6           0         0.000c  Pressure     0.10247E+00     627   0.48905E-02   0.35156E+00 0.11528E+04 
c  k            0.19610E+00      60   0.50987E-02   0.11108E+00 0.64638E+03 
c  epsilon      0.48546E+04      40   0.27503E-02   0.14557E+09 0.88092E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6993e-05                             2
a  epsilon        -0.48008                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.419          25.257          1.5034         0.17246
v  Velocity[Y]            -18.326           20.59         0.63148         0.41631
v  Velocity[Z]            -37.864          34.076         -0.6728     -0.00067783
v  ǁVelocityǁ          0.00011937          43.163          4.3636          3.7597
v  Pressure           -2.5624e+05      1.4347e+05           79586           70418
v  k                   1.1655e-06          13.922        0.051844        0.024153
v  epsilon              0.0012935      4.3579e+06          1822.5          31.828
v  TurbVisc            4.8819e-12         0.28972       0.0010801        0.013845
v  total_pressure      2.4376e+05      6.4347e+05      5.7959e+05      5.7042e+05


 TIME FOR THE TIME STEP              389:        0.64595E+02

===============================================================


 INSTANT    0.390000000E+03   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-----------------------------------------------------------c  epsilon      0.48525E+04      41   0.34342E-02   0.10325E+09 0.67345E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.6171e-05                             2
a  epsilon        -0.56988                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.771          25.068          1.5038         0.17245
v  Velocity[Y]            -17.743          22.709         0.63309         0.41682
v  Velocity[Z]            -34.597          34.073        -0.67226     -0.00054386
v  ǁVelocityǁ          0.00011991          43.422          4.3617          3.7583
v  Pressure           -2.5215e+05      1.4338e+05           79807           70544
v  k                   6.9412e-07          13.078        0.051841        0.024177
v  epsilon             6.4689e-05       4.371e+06          1812.1          31.941
v  TurbVisc            4.8768e-12         0.27896       0.0010826        0.013845
v  total_pressure      2.4785e+05      6.4338e+05      5.7981e+05      5.7054e+05


 TIME FOR THE TIME STEP              387:        0.70091E+02

===============================================================


 INSTANT    0.388000000E+03   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        -0.697434440E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34251E+02 0.84548E+01
   Friction velocity        uet   :  0.29026E-01 0.46779E+01
   Friction velocity        uk    :  0.28760E-01 0.48900E+01
   Dimensionless distance   yplus :  0.12716E-03 0.18739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9114
   Nb of faces within the viscous sub-layer     :      14572
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34080E+01     116   0.17873E+00   0.14494E+03 0.42177E+03 
c  Velocity[X]                                      0.45551E+02 
c  Velocity[Y]                                      0.46665E+02 
c  Velocity[Z]                                      0.52721E+02 
c  Pressure     0.95392E-01     678   0.51879E-02   0.32803E+00 0.11210E+04 
c  k            0.19571E+00      60   0.41954E-02   0.13308E+00 0.11032E+04 
c  epsilon      0.48498E+04      40   0.66196E-02   0.13939E+10 0.26537E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.0066e-05                             2
a  epsilon        -0.48868                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -10.31          25.976          1.5035         0.17248
v  Velocity[Y]            -19.224          20.602         0.63231         0.41637
v  Velocity[Z]            -36.733          33.035         -0.6728     -0.00073459
v  ǁVelocityǁ          0.00012007          40.525          4.3626           3.759
v  Pressure           -2.5508e+05      1.4353e+05           79685           70465
v  k                   1.1501e-06          13.499        0.051863        0.024169
v  epsilon              0.0012669      4.3619e+06          1820.5           31.89
v  TurbVisc            4.8779e-12         0.27977       0.0010812        0.013845
v  total_pressure      2.4492e+05      6.4353e+05      5.7968e+05      5.7047e+05


 TIME FOR THE TIME STEP              388:        0.75436E+02

===============================================================


 INSTANT    0.389000000E+03   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
--------------------------------------------------c  Velocity[X]                                      0.47156E+02 
c  Velocity[Y]                                      0.47872E+02 
c  Velocity[Z]                                      0.65311E+02 
c  Pressure     0.93883E-01     793   0.49692E-02   0.32198E+00 0.27171E+03 
c  k            0.19909E+00      62   0.37692E-02   0.93321E-01 0.10304E+04 
c  epsilon      0.48274E+04      40   0.73145E-02   0.12339E+10 0.24916E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.5843e-05                             3
a  epsilon        -0.58859                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.129          25.303          1.5028         0.17224
v  Velocity[Y]            -18.354          20.959         0.63006         0.41626
v  Velocity[Z]            -34.942          34.274         -0.6739     -0.00060027
v  ǁVelocityǁ           0.0001173          43.218          4.3662          3.7596
v  Pressure           -2.6065e+05      1.4322e+05           79362           70300
v  k                   1.2024e-06          14.641        0.051755        0.024144
v  epsilon             0.00039416      4.3877e+06          1810.7          31.806
v  TurbVisc            4.8743e-12         0.30632       0.0010773        0.013844
v  total_pressure      2.3935e+05      6.4322e+05      5.7936e+05       5.703e+05


 TIME FOR THE TIME STEP              391:        0.72912E+02

===============================================================


 INSTANT    0.392000000E+03   TIME STEP NUMBER             392
 ===============================================c  Pressure     0.10247E+00     627   0.48905E-02   0.35156E+00 0.11528E+04 
c  k            0.19610E+00      60   0.50987E-02   0.11108E+00 0.64638E+03 
c  epsilon      0.48546E+04      40   0.27503E-02   0.14557E+09 0.88092E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.6993e-05                             2
a  epsilon        -0.48008                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.419          25.257          1.5034         0.17246
v  Velocity[Y]            -18.326           20.59         0.63148         0.41631
v  Velocity[Z]            -37.864          34.076         -0.6728     -0.00067783
v  ǁVelocityǁ          0.00011937          43.163          4.3636          3.7597
v  Pressure           -2.5624e+05      1.4347e+05           79586           70418
v  k                   1.1655e-06          13.922        0.051844        0.024153
v  epsilon              0.0012935      4.3579e+06          1822.5          31.828
v  TurbVisc            4.8819e-12         0.28972       0.0010801        0.013845
v  total_pressure      2.4376e+05      6.4347e+05      5.7959e+05      5.7042e+05


 TIME FOR THE TIME STEP              389:        0.64757E+02

===============================================================


 INSTANT    0.390000000E+03   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         0.304843645E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39221E+02 0.78344E+01
   Friction velocity        uet   :  0.36053E-01 0.46792E+01
   Friction velocity        uk    :  0.37792E-01 0.49553E+01
   Dimensionless distance   yplus :  0.12658E-03 0.17927E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9127
   Nb of faces within the viscous sub-layer     :      14549
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34133E+01     117   0.18336E+00   0.14530E+03 0.42133E+03 
c  Velocity[X]                                      0.46096E+02 
c  Velocity[Y]                                      0.44772E+02 
c  Velocity[Z]                                      0.54431E+02 
c  Pressure     0.96565E-01     661   0.53091E-02   0.32933E+00 0.17437E+04 
c  k            0.19737E+00      61   0.40788E-02   0.10135E+00 0.74104E+03 
c  epsilon      0.48673E+04      40   0.27241E-02   0.16757E+09 0.81171E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.1621e-05                             2
a  epsilon        -0.41793                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.666          25.881          1.5031         0.17234
v  Velocity[Y]            -18.053          20.771          0.6307         0.41628
v  Velocity[Z]            -34.617          35.314        -0.67295     -0.00042716
v  ǁVelocityǁ           0.0001178          39.725           4.365          3.7599
v  Pressure           -2.5933e+05      1.4335e+05           79365           70278
v  k                    1.183e-06          14.319        0.051865        0.024149
v  epsilon              0.0014185      4.3905e+06          1824.2          31.837
v  TurbVisc            4.8808e-12         0.29874       0.0010785        0.013845
v  total_pressure      2.4067e+05      6.4335e+05      5.7937e+05      5.7028e+05


 TIME FOR THE TIME STEP              390:        0.71954E+02

===============================================================


 INSTANT    0.391000000E+03   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

------------------------------------------------------------------------------------------------
c  Velocity     0.34062E+01     118   0.18811E+00   0.15123E+03 0.42988E+03 
c  Velocity[X]                                      0.48278E+02 
c  Velocity[Y]                                      0.46442E+02 
c  Velocity[Z]                                      0.56508E+02 
c  Pressure     0.95603E-01     593   0.51172E-02   0.32836E+00 0.55347E+03 
c  k            0.20424E+00      65   0.54274E-02   0.29038E+00 0.11811E+04 
c  epsilon      0.48393E+04      41   0.67539E-02   0.15683E+10 0.28136E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1939e-05                             2
a  epsilon       -0.093729                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.622          24.684          1.5037         0.17209
v  Velocity[Y]            -17.898          20.424         0.62988         0.41588
v  Velocity[Z]            -35.764          34.113        -0.67632     -0.00064078
v  ǁVelocityǁ          0.00012118          42.873          4.3716            3.76
v  Pressure           -2.6443e+05       1.431e+05           79074           70101
v  k                   1.2447e-06          16.385        0.051828        0.024138
v  epsilon              0.0013032      4.3546e+06          1821.9          31.811
v  TurbVisc             4.905e-12         0.31442       0.0010747        0.013843
v  total_pressure      2.3557e+05       6.431e+05      5.7907e+05       5.701e+05


 TIME FOR THE TIME STEP              393:   c  Velocity[X]                                      0.47156E+02 
c  Velocity[Y]                                      0.47872E+02 
c  Velocity[Z]                                      0.65311E+02 
c  Pressure     0.93883E-01     793   0.49692E-02   0.32198E+00 0.27171E+03 
c  k            0.19909E+00      62   0.37692E-02   0.93321E-01 0.10304E+04 
c  epsilon      0.48274E+04      40   0.73145E-02   0.12339E+10 0.24916E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.5843e-05                             3
a  epsilon        -0.58859                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.129          25.303          1.5028         0.17224
v  Velocity[Y]            -18.354          20.959         0.63006         0.41626
v  Velocity[Z]            -34.942          34.274         -0.6739     -0.00060027
v  ǁVelocityǁ           0.0001173          43.218          4.3662          3.7596
v  Pressure           -2.6065e+05      1.4322e+05           79362           70300
v  k                   1.2024e-06          14.641        0.051755        0.024144
v  epsilon             0.00039416      4.3877e+06          1810.7          31.806
v  TurbVisc            4.8743e-12         0.30632       0.0010773        0.013844
v  total_pressure      2.3935e+05      6.4322e+05      5.7936e+05       5.703e+05


 TIME FOR THE TIME STEP              391:        0.73947E+02

===============================================================


 INSTANT    0.392000000E+03   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        -0.100409571E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444432E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34890E+02 0.78142E+01
   Friction velocity        uet   :  0.19629E-01 0.46805E+01
   Friction velocity        uk    :  0.19614E-01 0.48848E+01
   Dimensionless distance   yplus :  0.12548E-03 0.18222E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9139
   Nb of faces within the viscous sub-layer     :      14555
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34061E+01     118   0.18454E+00   0.14764E+03 0.42637E+03 
c  Velocity[X]                                      0.46945E+02 
c  Velocity[Y]                                      0.47095E+02 
c  Velocity[Z]                                      0.53605E+02 
c  Pressure     0.97623E-01     696   0.51178E-02   0.33416E+00 0.15546E+04 
c  k            0.19890E+00      62   0.42664E-02   0.12068E+00 0.93823E+03 
c  epsilon      0.48365E+04      44   0.35132E-02   0.33153E+09 0.11760E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.5681e-05                             3
a  epsilon        -0.36035                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.391          25.222          1.5031         0.17216
v  Velocity[Y]            -18.338          20.623         0.62984         0.41577
v  Velocity[Z]            -33.889          32.721        -0.67428     -0.00039481
v  ǁVelocityǁ          0.00012304          39.281          4.3687          3.7596
v  Pressure           -2.6333e+05      1.4316e+05           79144           70145
v  k                   1.2231e-06          14.857        0.051811         0.02413
v  epsilon             0.00096738       4.352e+06          1814.6          31.795
v  TurbVisc            4.8877e-12         0.31179       0.0010761        0.013844
v  total_pressure      2.3667e+05      6.4316e+05      5.7914e+05      5.7014e+05


 TIME FOR THE TIME STEP              392:        0.69004E+02

===============================================================


 INSTANT    0.393000000E+03   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.277910758E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36975E+02 0.67625E+01
   Friction velocity        uet   :  0.25921E-01 0.47015E+01
   Friction velocity        uk    :  0.25902E-01 0.48812E+01
   Dimensionless distance   yplus :  0.12870E-03 0.18050E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9142
   Nb of faces within the viscous sub-layer     :      14542
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34062E+01     118   0.18811E+00   0.15123E+03 0.42988E+03 
c  Velocity[X]                                      0.48278E+02 
c  Velocity[Y]                                      0.46442E+02 
c  Velocity[Z]                                      0.56508E+02 
c  Pressure     0.95603E-01     593   0.51172E-02   0.32836E+00 0.55347E+03 
c  k            0.20424E+00      65   0.54274E-02   0.29038E+00 0.11811E+04 
c  epsilon      0.48393E+04      41   0.67539E-02   0.15683E+10 0.28136E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.1939e-05                             2
a  epsilon       -0.093729                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.622          24.684          1.5037         0.17209
v  Velocity[Y]            -17.898          20.424         0.62988         0.41588
v  Velocity[Z]            -35.764          34.113        -0.67632     -0.00064078
v  ǁVelocityǁ          0.00012118          42.873          4.3716            3.76
v  Pressure           -2.6443e+05       1.431e+05           79074           70101
v  k                   1.2447e-06          16.385        0.051828        0.024138
v  epsilon              0.0013032      4.3546e+06          1821.9          31.811
v  TurbVisc             4.905e-12         0.31442       0.0010747        0.013843
v  total_pressure      2.3557e+05       6.431e+05      5.7907e+05       5.701e+05


 TIME FOR THE TIME STEP              393:        0.65627E+02

===============================================================


 INSTANT    0.394000000E+03   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000        -0.931498906E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444438E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34673E+02 0.71190E+01
   Friction velocity        uet   :  0.26396E-01 0.47017E+01
   Friction velocity        uk    :  0.26219E-01 0.49052E+01
   Dimensionless distance   yplus :  0.12784E-03 0.17905E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9140
   Nb of faces within the viscous sub-layer     :      14532
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34031E+01     117   0.18090E+00   0.15169E+03 0.42489E+03 
c  Velocity[X]                                      0.47609E+02 
c  Velocity[Y]                                      0.45399E+02 
c  Velocity[Z]                                      0.58684E+02 
c  Pressure     0.94968E-01     754   0.53188E-02   0.32517E+00 0.80941E+03 
c  k            0.21315E+00      68   0.45782E-02   0.23484E+00 0.84261E+03 
c  epsilon      0.48660E+04      45   0.34200E-02   0.20072E+09 0.87586E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -3.3093e-05                             2
a  epsilon        -0.19966                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.989          25.628          1.5051         0.17205
v  Velocity[Y]            -19.797          20.359         0.63009         0.41539
v  Velocity[Z]            -37.146          37.458        -0.67817      -0.0005481
v  ǁVelocityǁ           0.0001201          42.504          4.3748          3.7597
v  Pressure           -2.6719e+05      1.4294e+05           79050           70102
v  k                   1.2665e-06          17.711        0.051821        0.024161
v  epsilon             0.00087348      4.3502e+06          1819.6          31.897
v  TurbVisc             4.899e-12         0.34106        0.001074        0.013842
v  total_pressure      2.3281e+05      6.4294e+05      5.7905e+05       5.701e+05


 TIME FOR THE TIME STEP              394:        0.65978E+02

===============================================================


 INSTANT    0.395000000E+03   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         0.226072275E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444434E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49876E+02 0.75983E+01
   Friction velocity        uet   :  0.36462E-01 0.47001E+01
   Friction velocity        uk    :  0.37357E-01 0.49313E+01
   Dimensionless distance   yplus :  0.12705E-03 0.18665E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9111
   Nb of faces within the viscous sub-layer     :      14547
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34050E+01     119   0.18478E+00   0.15567E+03 0.42924E+03 
c  Velocity[X]                                      0.44853E+02 
c  Velocity[Y]                                      0.46571E+02 
c  Velocity[Z]                                      0.64246E+02 
c  Pressure     0.93287E-01     862   0.55009E-02   0.32074E+00 0.68761E+03 
c  k            0.22113E+00      69   0.43952E-02   0.22023E+00 0.76919E+03 
c  epsilon      0.48796E+04      47   0.27702E-02   0.12412E+09 0.70349E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.7163e-05                             2
a  epsilon        -0.15163                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.764           25.48          1.5069         0.17212
v  Velocity[Y]            -17.862          21.679         0.63048         0.41582
v  Velocity[Z]            -37.115          33.865        -0.68094     -0.00060745
v  ǁVelocityǁ          0.00011942          43.678          4.3793          3.7606
v  Pressure           -2.6844e+05      1.4282e+05           78995           70090
v  k                   1.2883e-06          18.969        0.051886        0.024181
v  epsilon             0.00092241      4.3339e+06          1824.3          31.996
v  TurbVisc            4.9036e-12         0.35915       0.0010737        0.013842
v  total_pressure      2.3156e+05      6.4282e+05      5.7899e+05      5.7009e+05


 TIME FOR THE TIME STEP              395:        0.81108E+02

===============================================================


 INSTANT    0.396000000E+03   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         0.329389559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444435E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38599E+02 0.79143E+01
   Friction velocity        uet   :  0.21800E-01 0.46926E+01
   Friction velocity        uk    :  0.21611E-01 0.48921E+01
   Dimensionless distance   yplus :  0.12675E-03 0.19490E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9119
   Nb of faces within the viscous sub-layer     :      14539
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34033E+01     117   0.18404E+00   0.15376E+03 0.42728E+03 
c  Velocity[X]                                      0.45373E+02 
c  Velocity[Y]                                      0.47044E+02 
c  Velocity[Z]                                      0.61342E+02 
c  Pressure     0.93084E-01     627   0.54603E-02   0.31863E+00 0.46406E+03 
c  k            0.22190E+00      68   0.35444E-02   0.14521E+00 0.94565E+03 
c  epsilon      0.48758E+04      48   0.69119E-02   0.11306E+10 0.23318E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.8525e-05                             2
a  epsilon        -0.35672                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -11.77          25.609          1.5089         0.17185
v  Velocity[Y]            -18.931          20.767         0.63063         0.41571
v  Velocity[Z]            -37.086          38.728        -0.68376     -0.00064823
v  ǁVelocityǁ          0.00011987          44.542          4.3839          3.7608
v  Pressure            -2.709e+05      1.4292e+05           78926           70056
v  k                   1.3095e-06          18.975        0.051899        0.024182
v  epsilon              0.0013442      4.3325e+06          1819.1            ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9144
   Nb of faces within the viscous sub-layer     :      14548
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34013E+01     118   0.18506E+00   0.15975E+03 0.43405E+03 
c  Velocity[X]                                      0.46073E+02 
c  Velocity[Y]                                      0.45715E+02 
c  Velocity[Z]                                      0.67962E+02 
c  Pressure     0.99038E-01     753   0.55596E-02   0.34255E+00 0.18916E+03 
c  k            0.17716E+00      67   0.61545E-02   0.18681E+00 0.79647E+03 
c  epsilon      0.47941E+04      45   0.45473E-02   0.10424E+09 0.60817E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5034e-05                             2
a  epsilon        -0.40878                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.211          24.423          1.5173         0.17233
v  Velocity[Y]             -19.83          21.513           0.633         0.41564
v  Velocity[Z]            -35.636          34.142        -0.69331     -0.00062528
v  ǁVelocityǁ          0.00012227      Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34027E+01     118   0.18716E+00   0.15752E+03 0.42973E+03 
c  Velocity[X]                                      0.47452E+02 
c  Velocity[Y]                                      0.46873E+02 
c  Velocity[Z]                                      0.63196E+02 
c  Pressure     0.95853E-01     645   0.49961E-02   0.33154E+00 0.15397E+04 
c  k            0.20509E+00      66   0.71447E-02   0.38551E+00 0.86898E+03 
c  epsilon      0.48373E+04      46   0.33298E-02   0.10232E+09 0.61580E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3442e-05                             2
a  epsilon        -0.17304                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.308          27.188          1.5115         0.17216
v  Velocity[Y]            -19.999          20.463         0.63108         0.41569
v  Velocity[Z]            -34.926          37.798        -0.68634     -0.00046082
v  ǁVelocityǁ          0.00012118          44.799          4.3889          3.7614
v  Pressure           -2.7191e+05      1.4254e+05           78731           69944
v  k                   1.3301e-06          16.418        0.051851        0.024133
v  epsilon              0.0010427      4.3283e+06          1815.4          31.862
v  TurbVisc            4.9129e-12         0.36752       0.0010732        0.013842
v  total_pressure      2.2809e+05      6.4254e+05      5.7873e+05      5.6994e+05


 TIME FOR THE TIME STEP              397:        0.71612E+02

===============================================================


 INSTANT    0.398000000E+03   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.156444444E+01
Smooth wall               5       41000         0.236351838E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37934E+02 0.73274E+01
   Friction velocity        uet   :  0.27411E-01 0.46829E+01
   Friction velocity        uk    :  0.35551E-01 0.48732E+01
   Dimensionless distance   yplus :  0.12743E-03 0.18407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9123
   Nb of faces within the viscous sub-layer     :      14513
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33988E+01     118   0.18346E+00   0.15443E+03 0.42592E+03 
c  Velocity[X]                                      0.48336E+02 
c  Velocity[Y]                                      0.47712E+02 
c  Velocity[Z]                                      0.58378E+02 
c  Pressure     0.10386E+00     540   0.63531E-02   0.35698E+00 0.62829E+03 
c  k            0.18969E+00      64   0.73486E-02   0.23490E+00 0.79825E+03 
c  epsilon      0.48261E+04      44   0.36005E-02   0.11719E+09 0.73703E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0655e-05                             2
a  epsilon        -0.22515                             4


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.467          24.855          1.5144         0.17223
v  Velocity[Y]            -18.845          20.133         0.63199         0.41565
v  Velocity[Z]            -39.402          44.597        -0.68985     -0.00061617
v  ǁVelocityǁ          0.00012563          47.948          4.3944          3.7623
v  Pressure           -2.7426e+05      1.4246e+05        Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43537E+02 0.70003E+01
   Friction velocity        uet   :  0.22993E-01 0.47022E+01
   Friction velocity        uk    :  0.22975E-01 0.48677E+01
   Dimensionless distance   yplus :  0.12706E-03 0.16079E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9156
   Nb of faces within the viscous sub-layer     :      14540
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35405E+01     132   0.17971E+00   0.96281E+04 0.18336E+04 
c  Velocity[X]                                      0.11883E+04 
c  Velocity[Y]                                      0.21033E+04 
c  Velocity[Z]                                      0.63365E+04 
c  Pressure     0.10455E+00    1203   0.18241E+00   0.35993E+00 0.27630E+06 
c  k            0.23584E+00     110   0.11582E-01   0.35446E+01 0.20010E+04 
c  epsilon      0.48195E+04      71      ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9144
   Nb of faces within the viscous sub-layer     :      14548
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34013E+01     118   0.18506E+00   0.15975E+03 0.43405E+03 
c  Velocity[X]                                      0.46073E+02 
c  Velocity[Y]                                      0.45715E+02 
c  Velocity[Z]                                      0.67962E+02 
c  Pressure     0.99038E-01     753   0.55596E-02   0.34255E+00 0.18916E+03 
c  k            0.17716E+00      67   0.61545E-02   0.18681E+00 0.79647E+03 
c  epsilon      0.47941E+04      45   0.45473E-02   0.10424E+09 0.60817E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.5034e-05                             2
a  epsilon        -0.40878                             6


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -10.211          24.423          1.5173         0.17233
v  Velocity[Y]             -19.83          21.513           0.633         0.41564
v  Velocity[Z]            -35.636          34.142        -0.69331     -0.00062528
v  ǁVelocityǁ          0.00012227          42.989          4.3997           3.763
v  Pressure           -2.7474e+05      1.4235e+05           78835           70075
v  k                   1.3689e-06          13.886         0.05185        0.024037
v  epsilon              0.0016338      4.3285e+06          1820.5          31.524
v  TurbVisc            4.9402e-12         0.29862        0.001072        0.013838
v  total_pressure      2.2526e+05      6.4235e+05      5.7883e+05      5.7008e+05


 TIME FOR THE TIME STEP              399:        0.73852E+02

===============================================================


 INSTANT    0.400000000E+03   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         0.290751147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444436E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface         Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43537E+02 0.70003E+01
   Friction velocity        uet   :  0.22993E-01 0.47022E+01
   Friction velocity        uk    :  0.22975E-01 0.48677E+01
   Dimensionless distance   yplus :  0.12706E-03 0.16079E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9156
   Nb of faces within the viscous sub-layer     :      14540
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35405E+01     132   0.17971E+00   0.96281E+04 0.18336E+04 
c  Velocity[X]                                      0.11883E+04 
c  Velocity[Y]                                      0.21033E+04 
c  Velocity[Z]                                      0.63365E+04 
c  Pressure     0.10455E+00    1203   0.18241E+00   0.35993E+00 0.27630E+06 
c  k            0.23584E+00     110   0.11582E-01   0.35446E+01 0.20010E+04 
c  epsilon      0.48195E+04      71   0.66920E-02   0.15293E+09 0.70966E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.33719                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25240E+03 0.71021E+01
   Friction velocity        uet   :  0.22884E-01 0.83433E+01
   Friction velocity        uk    :  0.23011E-01 0.52116E+01
   Dimensionless distance   yplus :  0.12767E-03 0.22001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10791
   Nb of faces within the viscous sub-layer     :      13421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57852E+01     141   0.16558E+00   0.27569E+04 0.15703E+04 
c  Velocity[X]                                      0.61924E+03 
c  Velocity[Y]                                      0.10678E+04 
c  Velocity[Z]                                      0.10699E+04 
c  Pressure     0.20611E+00    1433   0.35695E-01   0.59552E+00 0.44429E+05 
c  k            0.24903E+0Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.156444437E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43537E+02 0.70003E+01
   Friction velocity        uet   :  0.22993E-01 0.47022E+01
   Friction velocity        uk    :  0.22975E-01 0.48677E+01
   Dimensionless distance   yplus :  0.12706E-03 0.16079E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9156
   Nb of faces within the viscous sub-layer     :      14540
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.35405E+01     132   0.17971E+00   0.96281E+04 0.18336E+04 
c  Velocity[X]                                      0.11883E+04 
c  Velocity[Y]                                      0.21033E+04 
c  Velocity[Z]                                      0.63365E+04 
c  Pressure     0.10455E+00    1203   0.18241E+00   0.35993E+00 0.27630E+06 
c  k            0.23584E+00     110   0.11582E-01   0.35446E+01 0.20010E+04 
c  epsilon      0.48195E+04      71   0.66920E-02   0.15293E+09 0.70966E+04 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.33719                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -12.079          62.503          1.6845         0.24718
v  Velocity[Y]            -52.172          44.882         0.86226         0.59488
v  Velocity[Z]            -86.482          63.434        -0.70601      -0.0028687
v  ǁVelocityǁ          0.00012045          115.76          4.7519           5.034
v  Pressure           -1.7766e+05      3.8648e+05      2.2866e+05      2.0737e+05
v  k                    1.411e-06          10.802        0.052353         0.02971
v  epsilon              0.0012517      4.2553e+06          1830.3          32.505
v  TurbVisc            4.9185e-12         0.28192       0.0010718        0.013835
v  total_pressure      3.2234e+05      8.8648e+05      7.2866e+05      7.0737e+05


 TIME FOR THE TIME STEP              401:        0.88834E+02

=====================================Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25240E+03 0.71021E+01
   Friction velocity        uet   :  0.22884E-01 0.83433E+01
   Friction velocity        uk    :  0.23011E-01 0.52116E+01
   Dimensionless distance   yplus :  0.12767E-03 0.22001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10791
   Nb of faces within the viscous sub-layer     :      13421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57852E+01     141   0.16558E+00   0.27569E+04 0.15703E+04 
c  Velocity[X]                                      0.61924E+03 
c  Velocity[Y]                                      0.10678E+04 
c  Velocity[Z]                                      0.10699E+04 
c  Pressure     0.20611E+00    1433   0.35695E-01   0.59552E+00 0.44429E+05 
c  k            0.24903E+00     101   0.17732E-01   0.30596E+01 0.27653E+04 
c  epsilon      0.62186E+04      62   0.63385E-01   0.66804E+10 0.50332E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.3079e-05                             7
a  epsilon          -1.489                             2


  ** Computed fields on cells
     ------------------------

   field          ---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.622968018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17103E+03 0.73671E+01
   Friction velocity        uet   :  0.31408E-01 0.70380E+01
   Friction velocity        uk    :  0.31772E-01 0.54704E+01
   Dimensionless distance   yplus :  0.13256E-03 0.20089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10722
   Nb of faces within the viscous sub-layer     :      13444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59843E+01     133   0.16769E+00   0.17120E+04 0.12804E+04 
c  Velocity[X]                                      0.42178E+03 
c  Velocity[Y]                                      0.48890E+03 
c  Velocity[Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245840E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25240E+03 0.71021E+01
   Friction velocity        uet   :  0.22884E-01 0.83433E+01
   Friction velocity        uk    :  0.23011E-01 0.52116E+01
   Dimensionless distance   yplus :  0.12767E-03 0.22001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10791
   Nb of faces within the viscous sub-layer     :      13421
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.57852E+01     141   0.16558E+00   0.27569E+04 0.15703E+04 
c  Velocity[X]                                      0.61924E+03 
c  Velocity[Y]                                      0.10678E+04 
c  Velocity[Z]                                      0.10699E+04 
c  Pressure     0.20611E+00    1433   0.35695E-01   0.59552E+00 0.44429E+05 
c  k            0.24903E+00     101   0.17732E-01   0.30596E+01 0.27653E+04 
c  epsilon      0.62186E+04      62   0.63385E-01   0.66804E+10 0.50332E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.3079e-05                             7
a  epsilon          -1.489                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.008          52.723          1.7863         0.24833
v  Velocity[Y]            -38.017          40.936         0.88598          0.5884
v  Velocity[Z]            -105.23          77.308        -0.76576      -0.0016703
v  ǁVelocityǁ          0.00012453          116.19          4.9919          5.0329
v  Pressure           -3.0984e+05      2.4277e+05      1.5053e+05      1.2952e+05
v  k                   1.4657e-06           11.48         0.05679        0.038426
v  epsilon              0.0018214      4.7558e+06          2061.2          38.709
v  TurbVisc            4.9218e-12         0.32559       0.0012646         0.01921
v  total_pressure      1.9016e+05    ---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.622968018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17103E+03 0.73671E+01
   Friction velocity        uet   :  0.31408E-01 0.70380E+01
   Friction velocity        uk    :  0.31772E-01 0.54704E+01
   Dimensionless distance   yplus :  0.13256E-03 0.20089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10722
   Nb of faces within the viscous sub-layer     :      13444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59843E+01     133   0.16769E+00   0.17120E+04 0.12804E+04 
c  Velocity[X]                                      0.42178E+03 
c  Velocity[Y]                                      0.48890E+03 
c  Velocity[Z]                                      0.80134E+03 
c  Pressure     0.20610E+00     966   0.21992E-01   0.55789E+00 0.60131E+04 
c  k            0.23244E+00      95   0.11996E-01   0.20762E+01 0.36711E+04 
c  epsilon      0.65782E+04      55   0.15186E-01   0.43670E+11 0.11948E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00041312             ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.876187000E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16705E+03 0.83472E+01
   Friction velocity        uet   :  0.16972E-01 0.62312E+01
   Friction velocity        uk    :  0.16966E-01 0.57834E+01
   Dimensionless distance   yplus :  0.13135E-03 0.20176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10761
   Nb of faces within the viscous sub-layer     :      13353
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61758E+01---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.622968018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17103E+03 0.73671E+01
   Friction velocity        uet   :  0.31408E-01 0.70380E+01
   Friction velocity        uk    :  0.31772E-01 0.54704E+01
   Dimensionless distance   yplus :  0.13256E-03 0.20089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10722
   Nb of faces within the viscous sub-layer     :      13444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.59843E+01     133   0.16769E+00   0.17120E+04 0.12804E+04 
c  Velocity[X]                                      0.42178E+03 
c  Velocity[Y]                                      0.48890E+03 
c  Velocity[Z]                                      0.80134E+03 
c  Pressure     0.20610E+00     966   0.21992E-01   0.55789E+00 0.60131E+04 
c  k            0.23244E+00      95   0.11996E-01   0.20762E+01 0.36711E+04 
c  epsilon      0.65782E+04      55   0.15186E-01   0.43670E+11 0.11948E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00041312                             3
a  epsilon         -1.0763                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.023          53.793          1.8549         0.24819
v  Velocity[Y]            -44.537          33.809         0.87774         0.58805
v  Velocity[Z]             -94.44          67.029        -0.80371      -0.0011113
v  ǁVelocityǁ          0.00012865          109.38          5.1641          5.0765
v  Pressure           -3.3385e+05      2.4961e+05      1.5019e+05      1.3094e+05
v  k                   1.0411e-07          13.697        0.058935        0.041821
v  epsilon              0.0018557            ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.876187000E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16705E+03 0.83472E+01
   Friction velocity        uet   :  0.16972E-01 0.62312E+01
   Friction velocity        uk    :  0.16966E-01 0.57834E+01
   Dimensionless distance   yplus :  0.13135E-03 0.20176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10761
   Nb of faces within the viscous sub-layer     :      13353
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61758E+01     129   0.18096E+00   0.13139E+04 0.11247E+04 
c  Velocity[X]                                      0.34177E+03 
c  Velocity[Y]                                      0.35301E+03 
c  Velocity[Z]                                      0.61916E+03 
c  Pressure     0.20243E+00     914   0.18765E-01   0.53123E+00 0.20842E+04 
c  k            0.23260E+00      91   0.96374E-02   0.80991E+00 0.23693E+04 
c  epsilon      0.71661E+04      51   0.79239E-02   0.58917E+10 0.41422E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   fiel INSTANT    0.409000000E+03   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         0.491861366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14262E+03 0.84200E+01
   Friction velocity        uet   :  0.34295E-01 0.59542E+01
   Friction velocity        uk    :  0.36325E-01 0.58501E+01
   Dimensionless distance   yplus :  0.13236E-03 0.18805E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10960
   Nb of faces within the viscous sub-layer     :      13097
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs no      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.876187000E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16705E+03 0.83472E+01
   Friction velocity        uet   :  0.16972E-01 0.62312E+01
   Friction velocity        uk    :  0.16966E-01 0.57834E+01
   Dimensionless distance   yplus :  0.13135E-03 0.20176E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10761
   Nb of faces within the viscous sub-layer     :      13353
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61758E+01     129   0.18096E+00   0.13139E+04 0.11247E+04 
c  Velocity[X]                                      0.34177E+03 
c  Velocity[Y]                                      0.35301E+03 
c  Velocity[Z]                                      0.61916E+03 
c  Pressure     0.20243E+00     914   0.18765E-01   0.53123E+00 0.20842E+04 
c  k            0.23260E+00      91   0.96374E-02   0.80991E+00 0.23693E+04 
c  epsilon      0.71661E+04      51   0.79239E-02   0.58917E+10 0.41422E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -5.5806e-05                             1
a  epsilon       -0.015414                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -11.783          56.181          1.9132         0.24773
v  Velocity[Y]            -35.076           32.78          0.8731         0.58849
v  Velocity[Z]            -80.241          56.311        -0.83321     -0.00018367
v  ǁVelocityǁ          0.00013047           84.57          5.3273          5.1126
v  Pressure           -3.4973e+05   INSTANT    0.409000000E+03   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         0.491861366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14262E+03 0.84200E+01
   Friction velocity        uet   :  0.34295E-01 0.59542E+01
   Friction velocity        uk    :  0.36325E-01 0.58501E+01
   Dimensionless distance   yplus :  0.13236E-03 0.18805E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10960
   Nb of faces within the viscous sub-layer     :      13097
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63116E+01     128   0.17996E+00   0.86057E+03 0.92368E+03 
c  Velocity[X]                                      0.22787E+03 
c  Velocity[Y]                                      0.26650E+03 
c  Velocity[Z]                                      0.36620E+03 
c  Pressure     0.20390E+00     807   0.13831E-01   0.51252E+00 0.14091E+04 
c  k            0.22730E+00      89   0.60582E-02   0.44438E+00 0.20388E+04 
c  epsilon      0.76751E+04 v  total_pressure      1.2016e+05      7.5761e+05      6.4964e+05      6.3186e+05


 TIME FOR THE TIME STEP              410:        0.82653E+02

===============================================================


 INSTANT    0.411000000E+03   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         0.124257463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15579E+03 0.77314E+01
   Friction velocity        uet   :  0.34304E-01 0.59606E+01
   Friction velocity        uk    :  0.34190E-01 0.59227E+01
   Dimensionless distance   yplus :  0.13578E-03 0.19819E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11201
   Nb of faces within the viscous sub-layer     :      12831
   Total number of wall faces                   :      41000
------------------------------------------------------------
 INSTANT    0.409000000E+03   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         0.491861366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14262E+03 0.84200E+01
   Friction velocity        uet   :  0.34295E-01 0.59542E+01
   Friction velocity        uk    :  0.36325E-01 0.58501E+01
   Dimensionless distance   yplus :  0.13236E-03 0.18805E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10960
   Nb of faces within the viscous sub-layer     :      13097
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63116E+01     128   0.17996E+00   0.86057E+03 0.92368E+03 
c  Velocity[X]                                      0.22787E+03 
c  Velocity[Y]                                      0.26650E+03 
c  Velocity[Z]                                      0.36620E+03 
c  Pressure     0.20390E+00     807   0.13831E-01   0.51252E+00 0.14091E+04 
c  k            0.22730E+00      89   0.60582E-02   0.44438E+00 0.20388E+04 
c  epsilon      0.76751E+04      50   0.98046E-02   0.66265E+10 0.32860E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -7.189e-07                             1
a  epsilon      -0.0036253                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.864          47.968          1.9667         0.24711
v  Velocity[Y]            -28.141          31.967          0.8842      v  total_pressure      1.2016e+05      7.5761e+05      6.4964e+05      6.3186e+05


 TIME FOR THE TIME STEP              410:        0.85593E+02

===============================================================


 INSTANT    0.411000000E+03   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         0.124257463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15579E+03 0.77314E+01
   Friction velocity        uet   :  0.34304E-01 0.59606E+01
   Friction velocity        uk    :  0.34190E-01 0.59227E+01
   Dimensionless distance   yplus :  0.13578E-03 0.19819E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11201
   Nb of faces within the viscous sub-layer     :      12831
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64072E+01     127   0.18798E+00   0.84780E+03 0.90075E+03 
c  Velocity[X]                                      0.22163E+03 
c  Velocity[Y]                                      0.24813E+03 
c  Velocity[Z]                       v  epsilon              0.0013883        7.16e+06            3076          43.618
v  TurbVisc            5.7806e-12         0.32658       0.0015182        0.025582
v  total_pressure      1.0125e+05      7.6241e+05      6.4943e+05      6.3188e+05


 TIME FOR THE TIME STEP              412:        0.78795E+02

===============================================================


 INSTANT    0.413000000E+03   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.448765560E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69570E+02 0.77845E+01
   Friction velocity        uet   :  0.37775E-01 0.54509E+01
   Friction velocity        uk    :  0.39092E-01 0.58821E+01
   Dimensionless distance   yplus :  0.13830E-03 0.16031E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11430
   Nb of faces wiv  total_pressure      1.2016e+05      7.5761e+05      6.4964e+05      6.3186e+05


 TIME FOR THE TIME STEP              410:        0.76203E+02

===============================================================


 INSTANT    0.411000000E+03   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         0.124257463E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15579E+03 0.77314E+01
   Friction velocity        uet   :  0.34304E-01 0.59606E+01
   Friction velocity        uk    :  0.34190E-01 0.59227E+01
   Dimensionless distance   yplus :  0.13578E-03 0.19819E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11201
   Nb of faces within the viscous sub-layer     :      12831
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64072E+01     127   0.18798E+00   0.84780E+03 0.90075E+03 
c  Velocity[X]                                      0.22163E+03 
c  Velocity[Y]                                      0.24813E+03 
c  Velocity[Z]                                      0.37803E+03 
c  Pressure     0.18986E+00     858   0.11492E-01   0.47247E+00 0.12962E+04 
c  k            0.22611E+00      87   0.34345E-02   0.31956E+00 0.23145E+04 
c  epsilon      0.81661E+04      48   0.93285E-02   0.77654E+10 0.45487E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.3991e-06                             1
a  epsilon      -0.0030651                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  ------v  epsilon              0.0013883        7.16e+06            3076          43.618
v  TurbVisc            5.7806e-12         0.32658       0.0015182        0.025582
v  total_pressure      1.0125e+05      7.6241e+05      6.4943e+05      6.3188e+05


 TIME FOR THE TIME STEP              412:        0.74202E+02

===============================================================


 INSTANT    0.413000000E+03   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.448765560E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69570E+02 0.77845E+01
   Friction velocity        uet   :  0.37775E-01 0.54509E+01
   Friction velocity        uk    :  0.39092E-01 0.58821E+01
   Dimensionless distance   yplus :  0.13830E-03 0.16031E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11430
   Nb of faces within the viscous sub-layer     :      12570
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64799E+01     126   0.18383E+00   0.60312E+03 0.77576E+03 
c  v  Pressure           -4.1316e+05      2.6604e+05      1.4986e+05      1.3229e+05
v  k                   1.3574e-06          16.251        0.070892        0.046664
v  epsilon                 0.0009      7.1738e+06          3346.8          44.954
v  TurbVisc            5.9866e-12         0.32658       0.0015461        0.025855
v  total_pressure           86835      7.6604e+05      6.4986e+05      6.3229e+05


 TIME FOR THE TIME STEP              414:        0.81291E+02

===============================================================


 INSTANT    0.415000000E+03   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         0.174660997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245839E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92262E+02 0.78033E+01
   Friction velocity        uet   :  0.36322E-01 0.54951E+01
   Friction velocity        uk    :  0.36311E-01 0.58961E+01
   Dimensionless distance   yplusv  epsilon              0.0013883        7.16e+06            3076          43.618
v  TurbVisc            5.7806e-12         0.32658       0.0015182        0.025582
v  total_pressure      1.0125e+05      7.6241e+05      6.4943e+05      6.3188e+05


 TIME FOR THE TIME STEP              412:        0.82550E+02

===============================================================


 INSTANT    0.413000000E+03   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.448765560E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69570E+02 0.77845E+01
   Friction velocity        uet   :  0.37775E-01 0.54509E+01
   Friction velocity        uk    :  0.39092E-01 0.58821E+01
   Dimensionless distance   yplus :  0.13830E-03 0.16031E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11430
   Nb of faces within the viscous sub-layer     :      12570
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.64799E+01     126   0.18383E+00   0.60312E+03 0.77576E+03 
c  Velocity[X]                                      0.17119E+03 
c  Velocity[Y]                                      0.21583E+03 
c  Velocity[Z]                                      0.21610E+03 
c  Pressure     0.18202E+00     880   0.11158E-01   0.44292E+00 0.12840E+04 
c  k            0.22578E+00      85   0.32493E-02   0.30182E+00 0.23444E+04 
c  epsilon      0.86067E+04      47   0.75751E-02   0.82590E+10 0.13269E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon        -0.49939                             1


  ** Computed fields on cells
     ---------------v  Pressure           -4.1316e+05      2.6604e+05      1.4986e+05      1.3229e+05
v  k                   1.3574e-06          16.251        0.070892        0.046664
v  epsilon                 0.0009      7.1738e+06          3346.8          44.954
v  TurbVisc            5.9866e-12         0.32658       0.0015461        0.025855
v  total_pressure           86835      7.6604e+05      6.4986e+05      6.3229e+05


 TIME FOR THE TIME STEP              414:        0.80621E+02

===============================================================


 INSTANT    0.415000000E+03   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         0.174660997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245839E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92262E+02 0.78033E+01
   Friction velocity        uet   :  0.36322E-01 0.54951E+01
   Friction velocity        uk    :  0.36311E-01 0.58961E+01
   Dimensionless distance   yplus :  0.14608E-03 0.16565E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11642
   Nb of faces within the viscous sub-layer     :      12361
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------v  Velocity[Z]            -51.586          55.105        -0.86444     -0.00086956
v  ǁVelocityǁ           0.0001951          61.313          5.8469          5.2169
v  Pressure           -4.2309e+05      2.6876e+05      1.5011e+05      1.3266e+05
v  k                   1.2677e-06          16.308        0.073834        0.047128
v  epsilon              0.0012222      7.2209e+06          3665.9          46.476
v  TurbVisc            6.7113e-12         0.32659       0.0015678        0.026009
v  total_pressure           76907      7.6876e+05      6.5011e+05      6.3266e+05


 TIME FOR THE TIME STEP              416:        0.78323E+02

===============================================================


 INSTANT    0.417000000E+03   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         0.291434170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Relv  Pressure           -4.1316e+05      2.6604e+05      1.4986e+05      1.3229e+05
v  k                   1.3574e-06          16.251        0.070892        0.046664
v  epsilon                 0.0009      7.1738e+06          3346.8          44.954
v  TurbVisc            5.9866e-12         0.32658       0.0015461        0.025855
v  total_pressure           86835      7.6604e+05      6.4986e+05      6.3229e+05


 TIME FOR THE TIME STEP              414:        0.73342E+02

===============================================================


 INSTANT    0.415000000E+03   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         0.174660997E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245839E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92262E+02 0.78033E+01
   Friction velocity        uet   :  0.36322E-01 0.54951E+01
   Friction velocity        uk    :  0.36311E-01 0.58961E+01
   Dimensionless distance   yplus :  0.14608E-03 0.16565E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11642
   Nb of faces within the viscous sub-layer     :      12361
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65428E+01     124   0.18516E+00   0.58661E+03 0.74795E+03 
c  Velocity[X]                                      0.17060E+03 
c  Velocity[Y]                                      0.17897E+03 
c  Velocity[Z]                                      0.23704E+03 
c  Pressure     0.16803E+00     770   0.97166E-02   0.40740E+00 0.18789E+04 
c  k            0.22895E+00      82   0.53230E-02   0.74235E+00 0.35576E+04 
c  epsilon      0.90730E+04      47   0.92678E-02   0.36460E+11 0.13008E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
v  Velocity[Z]            -51.586          55.105        -0.86444     -0.00086956
v  ǁVelocityǁ           0.0001951          61.313          5.8469          5.2169
v  Pressure           -4.2309e+05      2.6876e+05      1.5011e+05      1.3266e+05
v  k                   1.2677e-06          16.308        0.073834        0.047128
v  epsilon              0.0012222      7.2209e+06          3665.9          46.476
v  TurbVisc            6.7113e-12         0.32659       0.0015678        0.026009
v  total_pressure           76907      7.6876e+05      6.5011e+05      6.3266e+05


 TIME FOR THE TIME STEP              416:        0.73103E+02

===============================================================


 INSTANT    0.417000000E+03   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         0.291434170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84147E+02 0.78268E+01
   Friction velocity        uet   :  0.19994E-01 0.54942E+01
   Friction velocity        uk    :  0.19929E-01 0.59303E+01
   Dimensionless distance   yplus :  0.15998E-03 0.16100E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11856
   Nb of faces within the viscous sub-layer     :      12200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      -----------v  Velocity[X]             -13.78          39.093          2.1037         0.24551
v  Velocity[Y]            -27.726          29.353         0.90733         0.58696
v  Velocity[Z]             -60.65          60.237        -0.87557      -0.0011343
v  ǁVelocityǁ          0.00023215          71.845          5.9163          5.2318
v  Pressure           -4.2893e+05      2.6921e+05       1.498e+05      1.3265e+05
v  k                   1.1977e-06          22.503        0.076575        0.047889
v  epsilon              0.0012437      7.2736e+06          3984.1          49.062
v  TurbVisc             6.883e-12         0.34678       0.0015885        0.026104
v  total_pressure           71066      7.6921e+05       6.498e+05      6.3265e+05


 TIME FOR THE TIME STEP              418:        0.69827E+02

===============================================================


 INSTANT    0.419000000E+03   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        -0.158570840E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Z]            -51.586          55.105        -0.86444     -0.00086956
v  ǁVelocityǁ           0.0001951          61.313          5.8469          5.2169
v  Pressure           -4.2309e+05      2.6876e+05      1.5011e+05      1.3266e+05
v  k                   1.2677e-06          16.308        0.073834        0.047128
v  epsilon              0.0012222      7.2209e+06          3665.9          46.476
v  TurbVisc            6.7113e-12         0.32659       0.0015678        0.026009
v  total_pressure           76907      7.6876e+05      6.5011e+05      6.3266e+05


 TIME FOR THE TIME STEP              416:        0.69027E+02

===============================================================


 INSTANT    0.417000000E+03   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         0.291434170E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84147E+02 0.78268E+01
   Friction velocity        uet   :  0.19994E-01 0.54942E+01
   Friction velocity        uk    :  0.19929E-01 0.59303E+01
   Dimensionless distance   yplus :  0.15998E-03 0.16100E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11856
   Nb of faces within the viscous sub-layer     :      12200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.65865E+01     123   0.18048E+00   0.53751E+03 0.71103E+03 
c  Velocity[X]                                      0.15566E+03 
c  Velocity[Y]                                      0.16294E+03 
c  Velocity[Z]                                      0.21890E+03 
c  Pressure     0.16656E+00     683   0.88890E-02   0.39994E+00 0.33120E+04 
c  k            0.25505E+00      79   0.12289E-01   0.37135E+01 0.34954E+04 
c  epsilon      0.95717E+04      55   0.81850E-02   0.28608E+11 0.20928E+06 
-----------------------------------------------------------------------------
  
  

  *v  Velocity[X]             -13.78          39.093          2.1037         0.24551
v  Velocity[Y]            -27.726          29.353         0.90733         0.58696
v  Velocity[Z]             -60.65          60.237        -0.87557      -0.0011343
v  ǁVelocityǁ          0.00023215          71.845          5.9163          5.2318
v  Pressure           -4.2893e+05      2.6921e+05       1.498e+05      1.3265e+05
v  k                   1.1977e-06          22.503        0.076575        0.047889
v  epsilon              0.0012437      7.2736e+06          3984.1          49.062
v  TurbVisc             6.883e-12         0.34678       0.0015885        0.026104
v  total_pressure           71066      7.6921e+05       6.498e+05      6.3265e+05


 TIME FOR THE TIME STEP              418:        0.71779E+02

===============================================================


 INSTANT    0.419000000E+03   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        -0.158570840E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+02 0.79667E+01
   Friction velocity        uet   :  0.31697E-01 0.55425E+01
   Friction velocity        uk    :  0.34550E-01 0.59520E+01
   Dimensionless distance   yplus :  0.17484E-03 0.20044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12045
   Nb of faces within the viscous sub-layer     :      12055
   Total number of wall faces                  -  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.099          38.132          2.1308          0.2455
v  Velocity[Y]            -25.785          29.934         0.89949         0.58604
v  Velocity[Z]            -54.932          55.761         -0.8893      -0.0014409
v  ǁVelocityǁ          0.00026133          64.998          5.9757           5.245
v  Pressure           -4.3443e+05      2.6934e+05      1.4946e+05      1.3265e+05
v  k                   1.1576e-06          37.883        0.079183        0.049091
v  epsilon              0.0013601      7.2446e+06            4196          53.926
v  TurbVisc            6.3805e-12         0.65208       0.0016229        0.026182
v  total_pressure           65573      7.6934e+05      6.4946e+05      6.3265e+05


 TIME FOR THE TIME STEP              420:        0.72908E+02

===============================================================


 INSTANT    0.421000000E+03   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         0.956949663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH v  Velocity[X]             -13.78          39.093          2.1037         0.24551
v  Velocity[Y]            -27.726          29.353         0.90733         0.58696
v  Velocity[Z]             -60.65          60.237        -0.87557      -0.0011343
v  ǁVelocityǁ          0.00023215          71.845          5.9163          5.2318
v  Pressure           -4.2893e+05      2.6921e+05       1.498e+05      1.3265e+05
v  k                   1.1977e-06          22.503        0.076575        0.047889
v  epsilon              0.0012437      7.2736e+06          3984.1          49.062
v  TurbVisc             6.883e-12         0.34678       0.0015885        0.026104
v  total_pressure           71066      7.6921e+05       6.498e+05      6.3265e+05


 TIME FOR THE TIME STEP              418:        0.75123E+02

===============================================================


 INSTANT    0.419000000E+03   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        -0.158570840E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+02 0.79667E+01
   Friction velocity        uet   :  0.31697E-01 0.55425E+01
   Friction velocity        uk    :  0.34550E-01 0.59520E+01
   Dimensionless distance   yplus :  0.17484E-03 0.20044E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12045
   Nb of faces within the viscous sub-layer     :      12055
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66319E+01     121   0.18529E+00   0.51999E+03 0.69521E+03 
c  Velocity[X]                                      0.15789E+03 
c  Velocity[Y]                                      0.14759E+03 
c  Velocity[Z]                                      0.21451E+03 
c  Pressure     0.17175E+00     766   0.85640E-02   0.41629E+00 0.19439E+04 
c  k            0.44319E+00      75   0.22364E-01   0.19320E+02 0.34400E+04 
c  epsilon      0.10125E+05      52  -  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.099          38.132          2.1308          0.2455
v  Velocity[Y]            -25.785          29.934         0.89949         0.58604
v  Velocity[Z]            -54.932          55.761         -0.8893      -0.0014409
v  ǁVelocityǁ          0.00026133          64.998          5.9757           5.245
v  Pressure           -4.3443e+05      2.6934e+05      1.4946e+05      1.3265e+05
v  k                   1.1576e-06          37.883        0.079183        0.049091
v  epsilon              0.0013601      7.2446e+06            4196          53.926
v  TurbVisc            6.3805e-12         0.65208       0.0016229        0.026182
v  total_pressure           65573      7.6934e+05      6.4946e+05      6.3265e+05


 TIME FOR THE TIME STEP              420:        0.70703E+02

===============================================================


 INSTANT    0.421000000E+03   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         0.956949663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83365E+02 0.10328E+02
   Friction velocity        uet   :  0.30870E-01 0.55993E+01
   Friction velocity        uk    :  0.30845E-01 0.59830E+01
   Dimensionless distance   yplus :  0.18426E-03 0.29267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12160
   Nb of faces within the viscous sub-layer     :      1
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.172          38.291          2.1534          0.2462
v  Velocity[Y]            -29.319          30.976         0.88705         0.58498
v  Velocity[Z]            -55.528          56.115        -0.90373      -0.0014131
v  ǁVelocityǁ           0.0002975          65.527          6.0265          5.2566
v  Pressure           -4.4151e+05      2.7041e+05      1.4947e+05      1.3286e+05
v  k                   3.3172e-07          28.854        0.081025        0.049429
v  epsilon             0.00019415      7.4146e+06          4413.7          55.295
v  TurbVisc            6.9321e-12         0.54808       0.0016609        0.026242
v  total_pressure           58491      7.7041e+05      6.4947e+05      6.3286e+05


 TIME FOR THE TIME STEP              422:        0.62427E+02

===============================================================


 INSTANT    0.423000000E+03   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.264245908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.0000000-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.099          38.132          2.1308          0.2455
v  Velocity[Y]            -25.785          29.934         0.89949         0.58604
v  Velocity[Z]            -54.932          55.761         -0.8893      -0.0014409
v  ǁVelocityǁ          0.00026133          64.998          5.9757           5.245
v  Pressure           -4.3443e+05      2.6934e+05      1.4946e+05      1.3265e+05
v  k                   1.1576e-06          37.883        0.079183        0.049091
v  epsilon              0.0013601      7.2446e+06            4196          53.926
v  TurbVisc            6.3805e-12         0.65208       0.0016229        0.026182
v  total_pressure           65573      7.6934e+05      6.4946e+05      6.3265e+05


 TIME FOR THE TIME STEP              420:        0.66468E+02

===============================================================


 INSTANT    0.421000000E+03   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         0.956949663E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83365E+02 0.10328E+02
   Friction velocity        uet   :  0.30870E-01 0.55993E+01
   Friction velocity        uk    :  0.30845E-01 0.59830E+01
   Dimensionless distance   yplus :  0.18426E-03 0.29267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12160
   Nb of faces within the viscous sub-layer     :      11926
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66696E+01     120   0.18447E+00   0.55679E+03 0.69443E+03 
c  Velocity[X]                                      0.15653E+03 
c  Velocity[Y]                                      0.15552E+03 
c  Velocity[Z]                                      0.24473E+03 
c  Pressure     0.16532E+00     718   0.82457E-02   0.40249E+00 0.10414E+04 
c  k            0.65436E+00      74   0.51057E-02   0.36038E+0
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.172          38.291          2.1534          0.2462
v  Velocity[Y]            -29.319          30.976         0.88705         0.58498
v  Velocity[Z]            -55.528          56.115        -0.90373      -0.0014131
v  ǁVelocityǁ           0.0002975          65.527          6.0265          5.2566
v  Pressure           -4.4151e+05      2.7041e+05      1.4947e+05      1.3286e+05
v  k                   3.3172e-07          28.854        0.081025        0.049429
v  epsilon             0.00019415      7.4146e+06          4413.7          55.295
v  TurbVisc            6.9321e-12         0.54808       0.0016609        0.026242
v  total_pressure           58491      7.7041e+05      6.4947e+05      6.3286e+05


 TIME FOR THE TIME STEP              422:        0.67092E+02

===============================================================


 INSTANT    0.423000000E+03   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.264245908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72861E+02 0.11315E+02
   Friction velocity        uet   :  0.38316E-01 0.56203E+01
   Friction velocity        uk    :  0.39316E-01 0.59992E+01
   Dimensionless distance   yplus :  0.19676E-03 0-  -------  --------------  --------------  ------------  ------------
a  k           -2.2156e-05                             3
a  epsilon       -0.037808                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.355          39.969          2.1684         0.24638
v  Velocity[Y]            -25.908          31.252          0.8768         0.58475
v  Velocity[Z]            -58.253          75.368        -0.91839      -0.0012193
v  ǁVelocityǁ          0.00033066          76.831          6.0716          5.2671
v  Pressure           -4.4697e+05      2.7194e+05      1.4981e+05      1.3329e+05
v  k                   4.0806e-07          21.555          0.0822        0.049351
v  epsilon              0.0016871      7.4544e+06          4601.6          54.329
v  TurbVisc            7.4835e-12         0.41045       0.0016922        0.026275
v  total_pressure           53027      7.7194e+05      6.4981e+05      6.3329e+05


 TIME FOR THE TIME STEP              424:        0.69460E+02

===============================================================


 INSTANT    0.425000000E+03   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         0.202067321E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0  
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.172          38.291          2.1534          0.2462
v  Velocity[Y]            -29.319          30.976         0.88705         0.58498
v  Velocity[Z]            -55.528          56.115        -0.90373      -0.0014131
v  ǁVelocityǁ           0.0002975          65.527          6.0265          5.2566
v  Pressure           -4.4151e+05      2.7041e+05      1.4947e+05      1.3286e+05
v  k                   3.3172e-07          28.854        0.081025        0.049429
v  epsilon             0.00019415      7.4146e+06          4413.7          55.295
v  TurbVisc            6.9321e-12         0.54808       0.0016609        0.026242
v  total_pressure           58491      7.7041e+05      6.4947e+05      6.3286e+05


 TIME FOR THE TIME STEP              422:        0.65755E+02

===============================================================


 INSTANT    0.423000000E+03   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.264245908E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72861E+02 0.11315E+02
   Friction velocity        uet   :  0.38316E-01 0.56203E+01
   Friction velocity        uk    :  0.39316E-01 0.59992E+01
   Dimensionless distance   yplus :  0.19676E-03 0.26561E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12269
   Nb of faces within the viscous sub-layer     :      11871
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.66939E+01     119   0.18848E+00   0.52951E+03 0.67916E+03 
c  Velocity[X]                                      0.15081E+03 
c  Velocity[Y]                                      0.14929E+03 
c  Velocity[Z]                                      0.22942E+03 
c  Pressure     0.17098E+00     755   0.82098E-02   0.41255E+00 0.14348E+04 
c  k            0.49633E+00      72   0.16830E-01   0.63364E+01 0.23025E+04 
c  epsilon      0.11149E+05      50   0.11004E-01   0.75094E+10 0.41005E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00028454                             2
a  epsilon       -0.067644                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.959          39.359          2.1618         0.24649
v  Velocity[Y]            -25.058          32.524         0.88178         0.58537
v  Velocity[Z]            -51.808          60.326         -0.9111       -0.001255
v  ǁVelocityǁ          0.00031545          68.562          6.0499          5.2622
v  Pressure           -4.4163e+05      2.7132e+05      1.4969e+05      1.3309e+05
v  k                   1.1763e-06          24.556         0.08145        0.049398
v  epsilon              0.0015814      7.3547e+06          4472.6          54.738
v  TurbVisc            7.4363e-12         0.42976       0.0016769        0.026261
v  total_pressure           58369      7.7132e+05      6.4969e+05      6.3309e+05


 TIME FOR THE TIME STEP              423:        0.77711E+02

===============================================================


 INSTANT    0.424000000E+03   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.237117815E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245868E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021966                             6
a  epsilon       -0.045404                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.462          38.826           2.178         0.24648
v  Velocity[Y]             -26.74          31.219         0.87128         0.58472
v  Velocity[Z]            -53.219          50.786         -0.9332      -0.0011216
v  ǁVelocityǁ          0.00035713          61.799          6.1129          5.2745
v  Pressure             -4.52e+05      2.7373e+05      1.5047e+05      1.3387e+05
v  k                   1.2708e-06          19.884        0.083337        0.049376
v  epsilon              0.0018732      7.4711e+06            4714          54.234
v  TurbVisc            8.1407e-12         0.32659       0.0017218        0.026296
v  total_pressure           48000      7.7373e+05      6.5047e+05      6.3387e+05


 TIME FOR THE TIME STEP              426:        0.60372E+02

===============================================================


 INSTANT    0.427000000E+03   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         0.139612289E-17
Rough wall                6           0        -  -------  --------------  --------------  ------------  ------------
a  k           -2.2156e-05                             3
a  epsilon       -0.037808                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.355          39.969          2.1684         0.24638
v  Velocity[Y]            -25.908          31.252          0.8768         0.58475
v  Velocity[Z]            -58.253          75.368        -0.91839      -0.0012193
v  ǁVelocityǁ          0.00033066          76.831          6.0716          5.2671
v  Pressure           -4.4697e+05      2.7194e+05      1.4981e+05      1.3329e+05
v  k                   4.0806e-07          21.555          0.0822        0.049351
v  epsilon              0.0016871      7.4544e+06          4601.6          54.329
v  TurbVisc            7.4835e-12         0.41045       0.0016922        0.026275
v  total_pressure           53027      7.7194e+05      6.4981e+05      6.3329e+05


 TIME FOR THE TIME STEP              424:        0.76129E+02

===============================================================


 INSTANT    0.425000000E+03   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         0.202067321E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15160E+03 0.13337E+02
   Friction velocity        uet   :  0.24000E-01 0.59161E+01
   Friction velocity        uk    :  0.23752E-01 0.59953E+01
   Dimensionless distance   yplus :  0.20778E-03 0.21784E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12337
   Nb of faces within the viscous sub-layer     :      11788
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67239E+01     119   0.18332E+00   0.53739E+03 0.67468E+03 
c  Ve
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021966                             6
a  epsilon       -0.045404                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.462          38.826           2.178         0.24648
v  Velocity[Y]             -26.74          31.219         0.87128         0.58472
v  Velocity[Z]            -53.219          50.786         -0.9332      -0.0011216
v  ǁVelocityǁ          0.00035713          61.799          6.1129          5.2745
v  Pressure             -4.52e+05      2.7373e+05      1.5047e+05      1.3387e+05
v  k                   1.2708e-06          19.884        0.083337        0.049376
v  epsilon              0.0018732      7.4711e+06            4714          54.234
v  TurbVisc            8.1407e-12         0.32659       0.0017218        0.026296
v  total_pressure           48000      7.7373e+05      6.5047e+05      6.3387e+05


 TIME FOR THE TIME STEP              426:        0.62970E+02

===============================================================


 INSTANT    0.427000000E+03   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         0.139612289E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         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  epsilon      0.11352E+05      45   0.70663E-02   0.25658E+11 0.71623E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00059412                             7
a  epsilon      -0.0061038                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.564          39.974          2.1863         0.24749
v  Velocity[Y]            -32.321          31.503         0.86859         0.58501
v  Velocity[Z]            -57.029          74.775        -0.94897     -0.00063092
v  ǁVelocityǁ          0.00036474          76.879          6.1545          5.2817
v  Pressure           -4.5565e+05      2.7531e+05      1.5092e+05      1.3437e+05
v  k                   3.1332e-07          17.347        0.084674        0.049448
v  epsilon             0.00024685      7.4816e+06          4888.7            54.5
v  TurbVisc            8.4638e-12         0.32659       0.0017522         0.02631
v  total_pressure           44346      7.7531e+05      6.5092e+05      6.3437e+05


 TIME FOR THE TIME STEP              428:        0.77563E+02

===============================================================


 INSTANT    0.429000000E+03   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2     
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021966                             6
a  epsilon       -0.045404                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.462          38.826           2.178         0.24648
v  Velocity[Y]             -26.74          31.219         0.87128         0.58472
v  Velocity[Z]            -53.219          50.786         -0.9332      -0.0011216
v  ǁVelocityǁ          0.00035713          61.799          6.1129          5.2745
v  Pressure             -4.52e+05      2.7373e+05      1.5047e+05      1.3387e+05
v  k                   1.2708e-06          19.884        0.083337        0.049376
v  epsilon              0.0018732      7.4711e+06            4714          54.234
v  TurbVisc            8.1407e-12         0.32659       0.0017218        0.026296
v  total_pressure           48000      7.7373e+05      6.5047e+05      6.3387e+05


 TIME FOR THE TIME STEP              426:        0.72580E+02

===============================================================


 INSTANT    0.427000000E+03   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         0.139612289E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69276E+02 0.12804E+02
   Friction velocity        uet   :  0.33811E-01 0.56211E+01
   Friction velocity        uk    :  0.40662E-01 0.60067E+01
   Dimensionless distance   yplus :  0.21527E-03 0.21299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12439
   Nb of faces within the viscous sub-layer     :      11697
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67287E+01     119   0.18300E+00   0.50648E+03 0.66552E+03 
c  Velocity[X]                                      0.14809E+03 
c  Velocity[Y]                                      0.15372E+03 
c  Velocity[Z]                                      0.20467E+03 
c  Pressure     0.15856E+00     843   0.95587E-02   0.38153E+00 0.19598E+04 
c  k            0.39903E+00      69   0.52120E-02   0.96403E+00 0.17867E+04 
c  epsilon      0.11189E+05      46   0.59269E-02   0.96169E+10 0.11667E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018371                             8
a  epsilon        -0.67978                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.066          39.399          2.1824         0.24716
v  Velocity[Y]            -25.556          31.836         0.87015         0.58506
v  Velocity[Z]             -52.75          69.003        -0.94096     -0.00074153
v  ǁVelocityǁ           0.0003602           75.31          6.1335          5.2772
v  Pressure           -4.5161e+05      2.7482e+05      1.5086e+05      1.3424e+05
v  k                   1.3234e-06          19.183        0.083951        0.049413
v  epsilon              0.0019824        7.48e+06          4781.1          54.333
v  TurbVisc            8.3492e-12         0.32659       0.0017372        0.026304
v  total_pressure           48388      7.7482e+05      6.5086e+05      6.3424e+05


 TIME FOR THE TIME STEP              427:        0.71988E+02

===============================================================


 INSTANT    0.428000000E+03   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.566319600E-18
Rough wall                6           0         0.000c  Pressure     0.15561E+00     659   0.72800E-02   0.37693E+00 0.26090E+03 
c  k            0.39595E+00      70   0.82468E-02   0.17106E+01 0.19235E+04 
c  epsilon      0.11541E+05      49   0.56165E-02   0.89039E+10 0.44361E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001027                             5
a  epsilon       -0.015822                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.617          40.062          2.1926         0.24735
v  Velocity[Y]            -31.018          31.745         0.86689         0.58475
v  Velocity[Z]            -60.999          51.401        -0.96695      -0.0013619
v  ǁVelocityǁ          0.00035316          69.892          6.1929          5.2877
v  Pressure           -4.6023e+05      2.7617e+05      1.5079e+05      1.3439e+05
v  k                    1.547e-06          22.335        0.085829        0.049571
v  epsilon              0.0023536       7.562e+06          4969.3          54.978
v  TurbVisc            8.5971e-12         0.32659       0.0017835         0.02632
v  total_pressure           39769      7.7617e+05      6.5079e+05      6.3439e+05


 TIME FOR THE TIME STEP              430:        0.74148E+02

===============================================================


 INSTANT    0.431000000E+03   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-----------------------------------------------------------c  epsilon      0.11352E+05      45   0.70663E-02   0.25658E+11 0.71623E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00059412                             7
a  epsilon      -0.0061038                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.564          39.974          2.1863         0.24749
v  Velocity[Y]            -32.321          31.503         0.86859         0.58501
v  Velocity[Z]            -57.029          74.775        -0.94897     -0.00063092
v  ǁVelocityǁ          0.00036474          76.879          6.1545          5.2817
v  Pressure           -4.5565e+05      2.7531e+05      1.5092e+05      1.3437e+05
v  k                   3.1332e-07          17.347        0.084674        0.049448
v  epsilon             0.00024685      7.4816e+06          4888.7            54.5
v  TurbVisc            8.4638e-12         0.32659       0.0017522         0.02631
v  total_pressure           44346      7.7531e+05      6.5092e+05      6.3437e+05


 TIME FOR THE TIME STEP              428:        0.75850E+02

===============================================================


 INSTANT    0.429000000E+03   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.298772166E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15336E+03 0.15621E+02
   Friction velocity        uet   :  0.17754E-01 0.59219E+01
   Friction velocity        uk    :  0.17506E-01 0.60068E+01
   Dimensionless distance   yplus :  0.21778E-03 0.21547E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12503
   Nb of faces within the viscous sub-layer     :      11593
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-c  Pressure     0.15561E+00     659   0.72800E-02   0.37693E+00 0.26090E+03 
c  k            0.39595E+00      70   0.82468E-02   0.17106E+01 0.19235E+04 
c  epsilon      0.11541E+05      49   0.56165E-02   0.89039E+10 0.44361E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001027                             5
a  epsilon       -0.015822                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.617          40.062          2.1926         0.24735
v  Velocity[Y]            -31.018          31.745         0.86689         0.58475
v  Velocity[Z]            -60.999          51.401        -0.96695      -0.0013619
v  ǁVelocityǁ          0.00035316          69.892          6.1929          5.2877
v  Pressure           -4.6023e+05      2.7617e+05      1.5079e+05      1.3439e+05
v  k                    1.547e-06          22.335        0.085829        0.049571
v  epsilon              0.0023536       7.562e+06          4969.3          54.978
v  TurbVisc            8.5971e-12         0.32659       0.0017835         0.02632
v  total_pressure           39769      7.7617e+05      6.5079e+05      6.3439e+05


 TIME FOR THE TIME STEP              430:        0.71654E+02

===============================================================


 INSTANT    0.431000000E+03   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.365807501E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0    c  Velocity[X]                                      0.15245E+03 
c  Velocity[Y]                                      0.14399E+03 
c  Velocity[Z]                                      0.20826E+03 
c  Pressure     0.15212E+00     696   0.73871E-02   0.36735E+00 0.66830E+03 
c  k            0.40841E+00      71   0.78270E-02   0.18241E+01 0.21953E+04 
c  epsilon      0.11776E+05      49   0.64983E-02   0.22221E+11 0.64478E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011991                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.896          38.996          2.1992         0.24642
v  Velocity[Y]            -32.781          31.932         0.86921         0.58536
v  Velocity[Z]            -51.809          66.586        -0.98154       -0.001322
v  ǁVelocityǁ          0.00035215          69.023          6.2309          5.2933
v  Pressure           -4.6449e+05      2.7746e+05      1.5121e+05      1.3486e+05
v  k                     1.74e-06          30.615        0.086941        0.049697
v  epsilon              0.0026796      7.5818e+06          5073.3          55.546
v  TurbVisc            8.5919e-12         0.33203       0.0018124        0.026329
v  total_pressure           35512      7.7746e+05      6.5121e+05      6.3486e+05


 TIME FOR THE TIME STEP              432:        0.67648E+02

===============================================================


 INSTANT    0.433000000E+03   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW Ic  Pressure     0.15561E+00     659   0.72800E-02   0.37693E+00 0.26090E+03 
c  k            0.39595E+00      70   0.82468E-02   0.17106E+01 0.19235E+04 
c  epsilon      0.11541E+05      49   0.56165E-02   0.89039E+10 0.44361E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001027                             5
a  epsilon       -0.015822                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.617          40.062          2.1926         0.24735
v  Velocity[Y]            -31.018          31.745         0.86689         0.58475
v  Velocity[Z]            -60.999          51.401        -0.96695      -0.0013619
v  ǁVelocityǁ          0.00035316          69.892          6.1929          5.2877
v  Pressure           -4.6023e+05      2.7617e+05      1.5079e+05      1.3439e+05
v  k                    1.547e-06          22.335        0.085829        0.049571
v  epsilon              0.0023536       7.562e+06          4969.3          54.978
v  TurbVisc            8.5971e-12         0.32659       0.0017835         0.02632
v  total_pressure           39769      7.7617e+05      6.5079e+05      6.3439e+05


 TIME FOR THE TIME STEP              430:        0.70918E+02

===============================================================


 INSTANT    0.431000000E+03   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.365807501E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.74399E+02 0.19961E+02
   Friction velocity        uet   :  0.19381E-01 0.55954E+01
   Friction velocity        uk    :  0.18996E-01 0.60176E+01
   Dimensionless distance   yplus :  0.21395E-03 0.27632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12628
   Nb of faces within the viscous sub-layer     :      11517
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67528E+01     120   0.19207E+00   0.49838E+03 0.65381E+03 
c  Velocity[X]                                      0.14713E+03 
c  Velocity[Y]                                      0.14685E+03 
c  Velocity[Z]                                      0.20440E+03 
c  Pressure     0.14983E+00    1007   0.76408E-02   0.36037E+00 0.23125E+04 
c  k            0.40740E+00      71   0.86975E-02   0.16809E+01 0.15166E+04 
c  epsilon      0.11634E+05      48   0.50514E-02   0.25733E+10 0.26720E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0012698                             4
a  epsilon        -0.02212                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.346          39.466          2.1959         0.24707
v  Velocity[Y]            -28.854          31.462         0.86789          0.5851
v  Velocity[Z]            -55.187           55.16        -0.97445      -0.0011078
v  ǁVelocityǁ          0.00034961          61.796          6.2116          5.2903
v  Pressure           -4.6035e+05      2.7687e+05      1.5123e+05      1.3478e+05
v  k                     1.64e-06          27.234        0.086212        0.049642
v  epsilon             0.00053853      7.5113e+06          4976.1          55.249
v  TurbVisc            8.5732e-12         0.32659       0.0017984        0.026325
v  total_pressure           39650      7.7687e+05      6.5123e+05      6.3478e+05


 TIME FOR THE TIME STEP              431:        0.79281E+02

===============================================================


 INSTANT    0.432000000E+03   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ----------------------------------------------------------------------------------
c  Velocity     0.67560E+01     118   0.18958E+00   0.49823E+03 0.64559E+03 
c  Velocity[X]                                      0.15154E+03 
c  Velocity[Y]                                      0.15500E+03 
c  Velocity[Z]                                      0.19170E+03 
c  Pressure     0.15791E+00     697   0.74919E-02   0.37978E+00 0.41361E+03 
c  k            0.41902E+00      70   0.70065E-02   0.18121E+01 0.17348E+04 
c  epsilon      0.11908E+05      48   0.38700E-02   0.12303E+10 0.11956E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013331                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.925          39.767          2.2066         0.24614
v  Velocity[Y]            -28.428          31.738         0.87474         0.58586
v  Velocity[Z]            -65.613          59.135        -0.99326      -0.0011171
v  ǁVelocityǁ          0.00036421          79.924          6.2685          5.2989
v  Pressure            -4.671e+05      2.7915e+05      1.5178e+05      1.3541e+05
v  k                   1.9496e-06          27.498        0.087718        0.049774
v  epsilon              0.0030551      7.5279e+06          5088.9          55.966
v  TurbVisc             8.594e-12         0.34832       0.0018356        0.026335
v  total_pressure           32905      7.7915e+05      6.5178e+05      6.3541e+05


 TIME FOR THE TIME STEP              434:        0.71539E+02

===============================================================


 INSTANTc  Velocity[X]                                      0.15245E+03 
c  Velocity[Y]                                      0.14399E+03 
c  Velocity[Z]                                      0.20826E+03 
c  Pressure     0.15212E+00     696   0.73871E-02   0.36735E+00 0.66830E+03 
c  k            0.40841E+00      71   0.78270E-02   0.18241E+01 0.21953E+04 
c  epsilon      0.11776E+05      49   0.64983E-02   0.22221E+11 0.64478E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011991                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.896          38.996          2.1992         0.24642
v  Velocity[Y]            -32.781          31.932         0.86921         0.58536
v  Velocity[Z]            -51.809          66.586        -0.98154       -0.001322
v  ǁVelocityǁ          0.00035215          69.023          6.2309          5.2933
v  Pressure           -4.6449e+05      2.7746e+05      1.5121e+05      1.3486e+05
v  k                     1.74e-06          30.615        0.086941        0.049697
v  epsilon              0.0026796      7.5818e+06          5073.3          55.546
v  TurbVisc            8.5919e-12         0.33203       0.0018124        0.026329
v  total_pressure           35512      7.7746e+05      6.5121e+05      6.3486e+05


 TIME FOR THE TIME STEP              432:        0.75272E+02

===============================================================


 INSTANT    0.433000000E+03   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         0.168595146E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12874E+03 0.21511E+02
   Friction velocity        uet   :  0.20328E-01 0.56449E+01
   Friction velocity        uk    :  0.19898E-01 0.60183E+01
   Dimensionless distance   yplus :  0.21261E-03 0.32386E+02
   ------------------------------------------------------------------------------------------------
c  Velocity     0.67560E+01     118   0.18958E+00   0.49823E+03 0.64559E+03 
c  Velocity[X]                                      0.15154E+03 
c  Velocity[Y]                                      0.15500E+03 
c  Velocity[Z]                                      0.19170E+03 
c  Pressure     0.15791E+00     697   0.74919E-02   0.37978E+00 0.41361E+03 
c  k            0.41902E+00      70   0.70065E-02   0.18121E+01 0.17348E+04 
c  epsilon      0.11908E+05      48   0.38700E-02   0.12303E+10 0.11956E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013331                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.925          39.767          2.2066         0.24614
v  Velocity[Y]            -28.428          31.738         0.87474         0.58586
v  Velocity[Z]            -65.613          59.135        -0.99326      -0.0011171
v  ǁVelocityǁ          0.00036421          79.924          6.2685          5.2989
v  Pressure            -4.671e+05      2.7915e+05      1.5178e+05      1.3541e+05
v  k                   1.9496e-06          27.498        0.087718        0.049774
v  epsilon              0.0030551      7.5279e+06          5088.9          55.966
v  TurbVisc             8.594e-12         0.34832       0.0018356        0.026335
v  total_pressure           32905      7.7915e+05      6.5178e+05      6.3541e+05


 TIME FOR THE TIME STEP              434:        0.69165E+02

===============================================================


 INSTANT    0.435000000E+03   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.228670401E-17
Rough wall                6           0         0.000000000E+00
Symmetry               Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67672E+01     118   0.18538E+00   0.51532E+03 0.65986E+03 
c  Velocity[X]                                      0.13953E+03 
c  Velocity[Y]                                      0.14966E+03 
c  Velocity[Z]                                      0.22613E+03 
c  Pressure     0.15676E+00     735   0.77551E-02   0.37840E+00 0.66223E+03 
c  k            0.42715E+00      68   0.65766E-02   0.99209E+00 0.13094E+04 
c  epsilon      0.12151E+05      46   0.45189E-02   0.22246E+10 0.23688E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013346                             4
a  epsilon       -0.065522                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.128          39.543          2.2122         0.24557
v  Velocity[Y]            -30.081          31.515         0.88221         0.58608
v  Velocity[Z]             -64.66          70.162         -1.0003      -0.0013791
v  ǁVelocityǁ          0.00036034          72.357          6.3034          5.3044
v  Pressure           -4.7135e+05      2.8125e+05      1.5246e+05      1.3603e+05
v  k                   2.1711e-06          25.735        0.088612        0.049842
v  epsilon               0.003461      7.6752e+06          5145.3          56.426
v  TurbVisc            8.5617e-12         0.35271       0.0018547         0.02634
v  total_pressure           28649      7.8125e+05      6.5246e+05-----------------------------------------------------------------------------
c  Velocity     0.67560E+01     118   0.18958E+00   0.49823E+03 0.64559E+03 
c  Velocity[X]                                      0.15154E+03 
c  Velocity[Y]                                      0.15500E+03 
c  Velocity[Z]                                      0.19170E+03 
c  Pressure     0.15791E+00     697   0.74919E-02   0.37978E+00 0.41361E+03 
c  k            0.41902E+00      70   0.70065E-02   0.18121E+01 0.17348E+04 
c  epsilon      0.11908E+05      48   0.38700E-02   0.12303E+10 0.11956E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013331                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.925          39.767          2.2066         0.24614
v  Velocity[Y]            -28.428          31.738         0.87474         0.58586
v  Velocity[Z]            -65.613          59.135        -0.99326      -0.0011171
v  ǁVelocityǁ          0.00036421          79.924          6.2685          5.2989
v  Pressure            -4.671e+05      2.7915e+05      1.5178e+05      1.3541e+05
v  k                   1.9496e-06          27.498        0.087718        0.049774
v  epsilon              0.0030551      7.5279e+06          5088.9          55.966
v  TurbVisc             8.594e-12         0.34832       0.0018356        0.026335
v  total_pressure           32905      7.7915e+05      6.5178e+05      6.3541e+05


 TIME FOR THE TIME STEP              434:        0.65703E+02

===============================================================


 INSTANT    0.435000000E+03   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.228670401E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10656E+03 0.24049E+02
   Friction velocity        uet   :  0.33857E-01 0.56049E+01
   Friction velocity   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67672E+01     118   0.18538E+00   0.51532E+03 0.65986E+03 
c  Velocity[X]                                      0.13953E+03 
c  Velocity[Y]                                      0.14966E+03 
c  Velocity[Z]                                      0.22613E+03 
c  Pressure     0.15676E+00     735   0.77551E-02   0.37840E+00 0.66223E+03 
c  k            0.42715E+00      68   0.65766E-02   0.99209E+00 0.13094E+04 
c  epsilon      0.12151E+05      46   0.45189E-02   0.22246E+10 0.23688E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013346                             4
a  epsilon       -0.065522                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.128          39.543          2.2122         0.24557
v  Velocity[Y]            -30.081          31.515         0.88221         0.58608
v  Velocity[Z]             -64.66          70.162         -1.0003      -0.0013791
v  ǁVelocityǁ          0.00036034          72.357          6.3034          5.3044
v  Pressure           -4.7135e+05      2.8125e+05      1.5246e+05      1.3603e+05
v  k                   2.1711e-06          25.735        0.088612        0.049842
v  epsilon               0.003461      7.6752e+06          5145.3          56.426
v  TurbVisc            8.5617e-12         0.35271       0.0018547         0.02634
v  total_pressure           28649      7.8125e+05      6.5246e+05      6.3603e+05


 TIME FOR THE TIME STEP              436:        0.76858E+02

===============================================================


 INSTANT    0.437000000E+03   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         0.370406344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245867E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13936E+03 0.22929E+02
   Friction velocity        uet   :  0.27829E-01 0.57307E+01
   Friction velocity        uk    :  0.27473E-01 0.60308E+01
   Dimensionless distance   yplus :  0.21599E-03 0.26922E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12960
   Nb of faces within the viscous sub-layer     :      11189
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67705E+01     119   0.18496E+00   0.50133E+03 0.65380E+03 
c  Velocity[X]                                      0.13932E+03 
c  Velocity[Y]                                      0.13849E+03 
c  Velocity[Z]                                      0.22353E+03 
c  Pressure     0.15247E+00     861   0.85409E-02   0.36438E+00 0.62684E+03 
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67672E+01     118   0.18538E+00   0.51532E+03 0.65986E+03 
c  Velocity[X]                                      0.13953E+03 
c  Velocity[Y]                                      0.14966E+03 
c  Velocity[Z]                                      0.22613E+03 
c  Pressure     0.15676E+00     735   0.77551E-02   0.37840E+00 0.66223E+03 
c  k            0.42715E+00      68   0.65766E-02   0.99209E+00 0.13094E+04 
c  epsilon      0.12151E+05      46   0.45189E-02   0.22246E+10 0.23688E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013346                             4
a  epsilon       -0.065522                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.128          39.543          2.2122         0.24557
v  Velocity[Y]            -30.081          31.515         0.88221         0.58608
v  Velocity[Z]             -64.66          70.162         -1.0003      -0.0013791
v  ǁVelocityǁ          0.00036034          72.357          6.3034          5.3044
v  Pressure           -4.7135e+05      2.8125e+05      1.5246e+05      1.3603e+05
v  k                   2.1711e-06          25.735        0.088612        0.049842
v  epsilon               0.003461      7.6752e+06          5145.3          56.426
v  TurbVisc            8.5617e-12         0.35271       0.0018547         0.02634
v  total_pressure           28649      7.8125e+05      6.5246e+05      6.3603e+05


 TIME FOR THE TIME STEP              436:        0.71954E+02

===============================================================


 INSTANT    0.437000000E+03   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         0.370406344E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245867E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13936E+03 0.22929E+02
   Friction velocity        uet   :  0.27829E-01 0.57307E+01
   Friction velocity        uk    :  0.27473E-01 0.60308E+01
   Dimensionless distance   yplus :  0.21599E-03 0.26922E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12960
   Nb of faces within the viscous sub-layer     :      11189
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67705E+01     119   0.18496E+00   0.50133E+03 0.65380E+03 
c  Velocity[X]                                      0.13932E+03 
c  Velocity[Y]                                      0.13849E+03 
c  Velocity[Z]                                      0.22353E+03 
c  Pressure     0.15247E+00     861   0.85409E-02   0.36438E+00 0.62684E+03 
c  k            0.44335E+00      66   0.83577E-02   0.13134E+01 0.13927E+04 
c  epsilon      0.12188E+05      45   0.45281E-02   0.16883E+10 0.25877E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0014595                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.503          38.533          2.2135         0.24547
v  Velocity[Y]            -32.466          31.008         0.88671         0.58641
v  Velocity[Z]            -54.791          48.627         -1.0022     -0.00074212
v  ǁVelocityǁ           0.0003593          61.408          6.3198          5.3072
v  Pressure           -4.7271e+05      2.8226e+05      1.5269e+05      1.3625e+05
v  k                   2.2838e-06          28.153        0.088919        0.049877
v  epsilon              0.0036697      7.5297e+06          5158.3          56.593
v  TurbVisc            4.8641e-12         0.35597       0.0018633        0.026343
v  total_pressure           27289      7.8226e+05      6.5269e+05      6.3625e+05


 TIME FOR THE TIME STEP              437:        0.67025E+02

===============================================================


 INSTANT    0.438000000E+03   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         0.739819456E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87897E+02 0.12684E+02
   Friction velocity        uet   :  0.32546E-01 0.56405E+01
   Friction velocity        uk    :  0.43222E-01 0.60001E+01
   Dimensionless distance   yplus :  0.21528E-03 0.25225E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13005
   Nb of faces within the viscous sub-layer     :      11139
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67733E+01     118   0.18390E+00   0.49288E+03 0.64115E+03 
c  Velocity[X]                                      0.14615E+03 
c  Velocity[Y]                                      0.14414E+03 
c  Velocity[Z]                                      0.20259E+03 
c  Pressure     0.16699E+00     897   0.81399E-02   0.39998E+00 0.51212E+03 
c  k            0.46093E+00      65   0.58074E-02   0.12386E+01 0.17036E+04 
c  epsilon      0.12258E+05      45   0.38705E-02   0.67907E+10 0.38902E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0014301                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.208          40.258          2.2136         0.24523
v  Velocity[Y]            -28.581          31.781         0.89038         0.58672
v  Velocity[Z]            -60.168          70.835         -1.0025     -0.00085482
v  ǁVelocityǁ          0.00035628          72.601          6.3345          5.3101
v  Pressure           -4.7409e+05      2.8284e+05        1.53e+05      1.3655e+05
v  k                   2.3966e-06          30.398        0.089454        0.049931
v  epsilon              0.0038805       7.543e+06          5212.4          56.929
v  TurbVisc            8.5487e-12         0.38302       0.0018712        0.026345
v  total_pressure           25907      7.8284e+05        6.53e+05      6.3655e+05


 TIME FOR THE TIME STEP              438:        0.78535E+02

===============================================================


 INSTANT    0.439000000E+03   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         0.363826082E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245868E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Max------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67825E+01     117   0.18775E+00   0.45910E+03 0.64081E+03 
c  Velocity[X]                                      0.14673E+03 
c  Velocity[Y]                                      0.14146E+03 
c  Velocity[Z]                                      0.17091E+03 
c  Pressure     0.17067E+00     691   0.67361E-02   0.40798E+00 0.32012E+03 
c  k            0.51997E+00      66   0.70286E-02   0.19832E+01 0.14396E+04 
c  epsilon      0.12453E+05      47   0.40645E-02   0.26326E+10 0.21750E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001492                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.673          39.483          2.2108         0.24555
v  Velocity[Y]            -28.884           31.78         0.89716         0.58707
v  Velocity[Z]            -60.919          63.237         -1.0036     -0.00071786
v  ǁVelocityǁ          0.00036071           69.58          6.3596          5.3136
v  Pressure           -4.7578e+05      2.8464e+05      1.5352e+05      1.3705e+05
v  k                   2.6194e-06          36.022        0.090343        0.050095
v  epsilon              0.0043016      7.5544e+06          5264.9          57.803
v  TurbVisc            8.5218e-12         0.43873       0.0018879        0.026351
v  total_pressure           24218      7.8464e+05      6.5352e+05      6.3705e+05


 TIME FOR THE TIME STEP              440:        0.69657E+02

===============================================================


 INSTANT    0.441000000E+03   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67866E+01     117   0.18843E+00   0.50302E+03 0.66298E+03 
c  Velocity[X]                                      0.15108E+03 
c  Velocity[Y]                                      0.15386E+03 
c  Velocity[Z]                                      0.19808E+03 
c  Pressure     0.15831E+00     739   0.63688E-02   0.37766E+00 0.10028E+04 
c  k            0.58074E+00      67   0.65714E-02   0.14750E+01 0.11179E+04 
c  epsilon      0.12697E+05      47   0.43243E-02   0.21855E+10 0.12329E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00155                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.367          39.283          2.2062          0.2455
v  Velocity[Y]            -34.428          31.075         0.90279         0.58757
v  Velocity[Z]            -57.525          94.943          -1.004     -0.00024467
v  ǁVelocityǁ          0.00037475          98.477          6.3809          5.3175
v  Pressure           -4.7872e+05      2.8681e+05      1.5446e+05      1.3789e+05
v  k                   2.8342e-06          39.676        0.091101      ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67825E+01     117   0.18775E+00   0.45910E+03 0.64081E+03 
c  Velocity[X]                                      0.14673E+03 
c  Velocity[Y]                                      0.14146E+03 
c  Velocity[Z]                                      0.17091E+03 
c  Pressure     0.17067E+00     691   0.67361E-02   0.40798E+00 0.32012E+03 
c  k            0.51997E+00      66   0.70286E-02   0.19832E+01 0.14396E+04 
c  epsilon      0.12453E+05      47   0.40645E-02   0.26326E+10 0.21750E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001492                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.673          39.483          2.2108         0.24555
v  Velocity[Y]            -28.884           31.78         0.89716         0.58707
v  Velocity[Z]            -60.919          63.237         -1.0036     -0.00071786
v  ǁVelocityǁ          0.00036071           69.58          6.3596          5.3136
v  Pressure           -4.7578e+05      2.8464e+05      1.5352e+05      1.3705e+05
v  k                   2.6194e-06          36.022        0.090343        0.050095
v  epsilon              0.0043016      7.5544e+06          5264.9          57.803
v  TurbVisc            8.5218e-12         0.43873       0.0018879        0.026351
v  total_pressure           24218      7.8464e+05      6.5352e+05      6.3705e+05


 TIME FOR THE TIME STEP              440:        0.71049E+02

===============================================================


 INSTANT    0.441000000E+03   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.446074561E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
--------------------------------------------------------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67866E+01     117   0.18843E+00   0.50302E+03 0.66298E+03 
c  Velocity[X]                                      0.15108E+03 
c  Velocity[Y]                                      0.15386E+03 
c  Velocity[Z]                                      0.19808E+03 
c  Pressure     0.15831E+00     739   0.63688E-02   0.37766E+00 0.10028E+04 
c  k            0.58074E+00      67   0.65714E-02   0.14750E+01 0.11179E+04 
c  epsilon      0.12697E+05      47   0.43243E-02   0.21855E+10 0.12329E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00155                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.367          39.283          2.2062          0.2455
v  Velocity[Y]            -34.428          31.075         0.90279         0.58757
v  Velocity[Z]            -57.525          94.943          -1.004     -0.00024467
v  ǁVelocityǁ          0.00037475          98.477          6.3809          5.3175
v  Pressure           -4.7872e+05      2.8681e+05      1.5446e+05      1.3789e+05
v  k                   2.8342e-06          39.676        0.091101        0.050293
v  epsilon              0.0047146      7.5468e+06          5306.7          58.839
v  TurbVisc             8.571e-12         0.48949       0.0019043        0.026357
v  total_pressure           21284      7.8681e+05      6.5446e+05      6.3789e+05


 TIME FOR THE TIME STEP              442:        0.74262E+02

===============================================================


 INSTANT    0.443000000E+03   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Bounda   Nb of faces within the viscous sub-layer     :      10975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67886E+01     117   0.18361E+00   0.50315E+03 0.65710E+03 
c  Velocity[X]                                      0.14589E+03 
c  Velocity[Y]                                      0.15188E+03 
c  Velocity[Z]                                      0.20538E+03 
c  Pressure     0.15123E+00     712   0.62866E-02   0.36073E+00 0.14172E+04 
c  k            0.62610E+00      69   0.72870E-02   0.35008E+01 0.18109E+04 
c  epsilon      0.12960E+05      48   0.62959E-02   0.92756E+10 0.48233E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0015245                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.444          38.802          2.2025          0.2461
v  Velocity[Y]            -27.057          30.456         0.90589         0.58772
v  Velocity[Z]            -66.098          61.404         -1.0059     -0.00017123
v  ǁVelocityǁ          0.00037284          72.581          6.3999          5.3214
v  Pressure           -4.7926e+05      2.8819e+05      1.5501e+05       1.384e+05
v  k         Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67866E+01     117   0.18843E+00   0.50302E+03 0.66298E+03 
c  Velocity[X]                                      0.15108E+03 
c  Velocity[Y]                                      0.15386E+03 
c  Velocity[Z]                                      0.19808E+03 
c  Pressure     0.15831E+00     739   0.63688E-02   0.37766E+00 0.10028E+04 
c  k            0.58074E+00      67   0.65714E-02   0.14750E+01 0.11179E+04 
c  epsilon      0.12697E+05      47   0.43243E-02   0.21855E+10 0.12329E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00155                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.367          39.283          2.2062          0.2455
v  Velocity[Y]            -34.428          31.075         0.90279         0.58757
v  Velocity[Z]            -57.525          94.943          -1.004     -0.00024467
v  ǁVelocityǁ          0.00037475          98.477          6.3809          5.3175
v  Pressure           -4.7872e+05      2.8681e+05      1.5446e+05      1.3789e+05
v  k                   2.8342e-06          39.676        0.091101        0.050293
v  epsilon              0.0047146      7.5468e+06          5306.7          58.839
v  TurbVisc             8.571e-12         0.48949       0.0019043        0.026357
v  total_pressure           21284      7.8681e+05      6.5446e+05      6.3789e+05


 TIME FOR THE TIME STEP              442:        0.64750E+02

===============================================================


 INSTANT    0.443000000E+03   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         0.104250982E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------------   Nb of faces within the viscous sub-layer     :      10975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67886E+01     117   0.18361E+00   0.50315E+03 0.65710E+03 
c  Velocity[X]                                      0.14589E+03 
c  Velocity[Y]                                      0.15188E+03 
c  Velocity[Z]                                      0.20538E+03 
c  Pressure     0.15123E+00     712   0.62866E-02   0.36073E+00 0.14172E+04 
c  k            0.62610E+00      69   0.72870E-02   0.35008E+01 0.18109E+04 
c  epsilon      0.12960E+05      48   0.62959E-02   0.92756E+10 0.48233E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0015245                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.444          38.802          2.2025          0.2461
v  Velocity[Y]            -27.057          30.456         0.90589         0.58772
v  Velocity[Z]            -66.098          61.404         -1.0059     -0.00017123
v  ǁVelocityǁ          0.00037284          72.581          6.3999          5.3214
v  Pressure           -4.7926e+05      2.8819e+05      1.5501e+05       1.384e+05
v  k                   3.0357e-06          39.613         0.09183        0.050483
v  epsilon              0.0051142      7.7647e+06          5360.8            59.8
v  TurbVisc            8.6261e-12         0.52646       0.0019191        0.026363
v  total_pressure           20740      7.8819e+05      6.5501e+05       6.384e+05


 TIME FOR THE TIME STEP              444:        0.72596E+02

===============================================================


 INSTANT    0.445000000E+03   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------   Nb of reversal of the velocity at the wall   :      13305
   Nb of faces within the viscous sub-layer     :      10923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67965E+01     116   0.19167E+00   0.44770E+03 0.62996E+03 
c  Velocity[X]                                      0.13629E+03 
c  Velocity[Y]                                      0.14651E+03 
c  Velocity[Z]                                      0.16490E+03 
c  Pressure     0.15186E+00     664   0.67493E-02   0.36295E+00 0.15435E+04 
c  k            0.64639E+00      70   0.66936E-02   0.39452E+01 0.16717E+04 
c  epsilon      0.13119E+05      51   0.55034E-02   0.39168E+10 0.17747E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016204                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.953          39.008           2.201         0.24636
v  Velocity[Y]            -27.706           30.25         0.90738         0.58765
v  Velocity[Z]            -61.505          69.645         -1.0069      3.4801e-05
v  ǁVelocityǁ          0.00038074          75.586          6.4182          5.3249
v  Pressure           -4.8254e+   Nb of faces within the viscous sub-layer     :      10975
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67886E+01     117   0.18361E+00   0.50315E+03 0.65710E+03 
c  Velocity[X]                                      0.14589E+03 
c  Velocity[Y]                                      0.15188E+03 
c  Velocity[Z]                                      0.20538E+03 
c  Pressure     0.15123E+00     712   0.62866E-02   0.36073E+00 0.14172E+04 
c  k            0.62610E+00      69   0.72870E-02   0.35008E+01 0.18109E+04 
c  epsilon      0.12960E+05      48   0.62959E-02   0.92756E+10 0.48233E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0015245                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.444          38.802          2.2025          0.2461
v  Velocity[Y]            -27.057          30.456         0.90589         0.58772
v  Velocity[Z]            -66.098          61.404         -1.0059     -0.00017123
v  ǁVelocityǁ          0.00037284          72.581          6.3999          5.3214
v  Pressure           -4.7926e+05      2.8819e+05      1.5501e+05       1.384e+05
v  k                   3.0357e-06          39.613         0.09183        0.050483
v  epsilon              0.0051142      7.7647e+06          5360.8            59.8
v  TurbVisc            8.6261e-12         0.52646       0.0019191        0.026363
v  total_pressure           20740      7.8819e+05      6.5501e+05       6.384e+05


 TIME FOR THE TIME STEP              444:        0.67123E+02

===============================================================


 INSTANT    0.445000000E+03   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.228630572E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDI   Nb of reversal of the velocity at the wall   :      13305
   Nb of faces within the viscous sub-layer     :      10923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67965E+01     116   0.19167E+00   0.44770E+03 0.62996E+03 
c  Velocity[X]                                      0.13629E+03 
c  Velocity[Y]                                      0.14651E+03 
c  Velocity[Z]                                      0.16490E+03 
c  Pressure     0.15186E+00     664   0.67493E-02   0.36295E+00 0.15435E+04 
c  k            0.64639E+00      70   0.66936E-02   0.39452E+01 0.16717E+04 
c  epsilon      0.13119E+05      51   0.55034E-02   0.39168E+10 0.17747E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016204                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.953          39.008           2.201         0.24636
v  Velocity[Y]            -27.706           30.25         0.90738         0.58765
v  Velocity[Z]            -61.505          69.645         -1.0069      3.4801e-05
v  ǁVelocityǁ          0.00038074          75.586          6.4182          5.3249
v  Pressure           -4.8254e+05      2.8852e+05      1.5523e+05      1.3871e+05
v  k                   3.2241e-06           31.74        0.092338        0.050575
v  epsilon              0.0054999      7.5822e+06          5358.1          60.313
v  TurbVisc            8.8381e-12         0.48047       0.0019316        0.026367
v  total_pressure           17460      7.8852e+05      6.5523e+05      6.3871e+05


 TIME FOR THE TIME STEP              446:        0.71370E+02

===============================================================


 INSTANT    0.447000000E+03   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW I   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13384
   Nb of faces within the viscous sub-layer     :      10876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68013E+01     115   0.18610E+00   0.46768E+03 0.63699E+03 
c  Velocity[X]                                      0.13962E+03 
c  Velocity[Y]                                      0.14442E+03 
c  Velocity[Z]                                      0.18364E+03 
c  Pressure     0.14250E+00     623   0.79110E-02   0.34044E+00 0.68583E+03 
c  k            0.59342E+00      69   0.73858E-02   0.17043E+01 0.10565E+04 
c  epsilon      0.12957E+05      50   0.52495E-02   0.13312E+10 0.44691E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0032858                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.328          38.235          2.2025         0.24673
v  Velocity[Y]            -28.642            30.4         0.90636         0.58777
v  Velocity[Z]             -62.28          71.848         -1.0115     -0.00039259
v  ǁVelocityǁ          0.00039856          74.154      Nb of reversal of the velocity at the wall   :      13305
   Nb of faces within the viscous sub-layer     :      10923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67965E+01     116   0.19167E+00   0.44770E+03 0.62996E+03 
c  Velocity[X]                                      0.13629E+03 
c  Velocity[Y]                                      0.14651E+03 
c  Velocity[Z]                                      0.16490E+03 
c  Pressure     0.15186E+00     664   0.67493E-02   0.36295E+00 0.15435E+04 
c  k            0.64639E+00      70   0.66936E-02   0.39452E+01 0.16717E+04 
c  epsilon      0.13119E+05      51   0.55034E-02   0.39168E+10 0.17747E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016204                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.953          39.008           2.201         0.24636
v  Velocity[Y]            -27.706           30.25         0.90738         0.58765
v  Velocity[Z]            -61.505          69.645         -1.0069      3.4801e-05
v  ǁVelocityǁ          0.00038074          75.586          6.4182          5.3249
v  Pressure           -4.8254e+05      2.8852e+05      1.5523e+05      1.3871e+05
v  k                   3.2241e-06           31.74        0.092338        0.050575
v  epsilon              0.0054999      7.5822e+06          5358.1          60.313
v  TurbVisc            8.8381e-12         0.48047       0.0019316        0.026367
v  total_pressure           17460      7.8852e+05      6.5523e+05      6.3871e+05


 TIME FOR THE TIME STEP              446:        0.74175E+02

===============================================================


 INSTANT    0.447000000E+03   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         0.248025044E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13384
   Nb of faces within the viscous sub-layer     :      10876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68013E+01     115   0.18610E+00   0.46768E+03 0.63699E+03 
c  Velocity[X]                                      0.13962E+03 
c  Velocity[Y]                                      0.14442E+03 
c  Velocity[Z]                                      0.18364E+03 
c  Pressure     0.14250E+00     623   0.79110E-02   0.34044E+00 0.68583E+03 
c  k            0.59342E+00      69   0.73858E-02   0.17043E+01 0.10565E+04 
c  epsilon      0.12957E+05      50   0.52495E-02   0.13312E+10 0.44691E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0032858                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.328          38.235          2.2025         0.24673
v  Velocity[Y]            -28.642            30.4         0.90636         0.58777
v  Velocity[Z]             -62.28          71.848         -1.0115     -0.00039259
v  ǁVelocityǁ          0.00039856          74.154          6.4368           5.329
v  Pressure           -4.8432e+05      2.8954e+05      1.5607e+05       1.394e+05
v  k                   3.4057e-06          27.745        0.092893        0.050577
v  epsilon              0.0058731      7.7138e+06          5404.5          60.213
v  TurbVisc            9.3831e-12         0.43295        0.001943        0.026369
v  total_pressure           15675      7.8954e+05      6.5607e+05       6.394e+05


 TIME FOR THE TIME STEP              448:        0.70641E+02

===============================================================


 INSTANT    0.449000000E+03   TIME STEP NUMBER             449
 ================================   Dimensionless distance   yplus :  0.22747E-03 0.29446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13405
   Nb of faces within the viscous sub-layer     :      10835
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67979E+01     115   0.18597E+00   0.48850E+03 0.65834E+03 
c  Velocity[X]                                      0.14799E+03 
c  Velocity[Y]                                      0.15427E+03 
c  Velocity[Z]                                      0.18623E+03 
c  Pressure     0.16383E+00     701   0.59138E-02   0.39003E+00 0.68301E+03 
c  k            0.53568E+00      67   0.59027E-02   0.80918E+00 0.10650E+04 
c  epsilon      0.12891E+05      47   0.12130E-01   0.34199E+10 0.98200E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0041361                             4
a  epsilon      -0.0041623                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -15.06          38.878          2.2057         0.24654
v  Velocity[Y]            -28.031          31.069         0.90486         0.58774
v  Velocity[Z]            -55.69   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13384
   Nb of faces within the viscous sub-layer     :      10876
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68013E+01     115   0.18610E+00   0.46768E+03 0.63699E+03 
c  Velocity[X]                                      0.13962E+03 
c  Velocity[Y]                                      0.14442E+03 
c  Velocity[Z]                                      0.18364E+03 
c  Pressure     0.14250E+00     623   0.79110E-02   0.34044E+00 0.68583E+03 
c  k            0.59342E+00      69   0.73858E-02   0.17043E+01 0.10565E+04 
c  epsilon      0.12957E+05      50   0.52495E-02   0.13312E+10 0.44691E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0032858                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.328          38.235          2.2025         0.24673
v  Velocity[Y]            -28.642            30.4         0.90636         0.58777
v  Velocity[Z]             -62.28          71.848         -1.0115     -0.00039259
v  ǁVelocityǁ          0.00039856          74.154          6.4368           5.329
v  Pressure           -4.8432e+05      2.8954e+05      1.5607e+05       1.394e+05
v  k                   3.4057e-06          27.745        0.092893        0.050577
v  epsilon              0.0058731      7.7138e+06          5404.5          60.213
v  TurbVisc            9.3831e-12         0.43295        0.001943        0.026369
v  total_pressure           15675      7.8954e+05      6.5607e+05       6.394e+05


 TIME FOR THE TIME STEP              448:        0.64443E+02

===============================================================


 INSTANT    0.449000000E+03   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         0.366707355E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1       Dimensionless distance   yplus :  0.22747E-03 0.29446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13405
   Nb of faces within the viscous sub-layer     :      10835
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67979E+01     115   0.18597E+00   0.48850E+03 0.65834E+03 
c  Velocity[X]                                      0.14799E+03 
c  Velocity[Y]                                      0.15427E+03 
c  Velocity[Z]                                      0.18623E+03 
c  Pressure     0.16383E+00     701   0.59138E-02   0.39003E+00 0.68301E+03 
c  k            0.53568E+00      67   0.59027E-02   0.80918E+00 0.10650E+04 
c  epsilon      0.12891E+05      47   0.12130E-01   0.34199E+10 0.98200E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0041361                             4
a  epsilon      -0.0041623                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -15.06          38.878          2.2057         0.24654
v  Velocity[Y]            -28.031          31.069         0.90486         0.58774
v  Velocity[Z]            -55.693          94.009         -1.0154      0.00010349
v  ǁVelocityǁ          0.00041455           97.22          6.4551          5.3334
v  Pressure           -4.8893e+05       2.897e+05      1.5651e+05      1.3976e+05
v  k                     3.59e-06          24.783        0.093531        0.050544
v  epsilon              0.0041623       7.692e+06          5467.5          59.959
v  TurbVisc            9.9284e-12          0.3901       0.0019553        0.026371
v  total_pressure           11074       7.897e+05      6.5651e+05      6.3976e+05


 TIME FOR THE TIME STEP              450:        0.68947E+02

========================================   Friction velocity        uet   :  0.21128E-01 0.56095E+01
   Friction velocity        uk    :  0.21118E-01 0.60121E+01
   Dimensionless distance   yplus :  0.23102E-03 0.27632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13468
   Nb of faces within the viscous sub-layer     :      10815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68005E+01     115   0.18767E+00   0.45580E+03 0.63576E+03 
c  Velocity[X]                                      0.12831E+03 
c  Velocity[Y]                                      0.13637E+03 
c  Velocity[Z]                                      0.19112E+03 
c  Pressure     0.14211E+00     953   0.60518E-02   0.33975E+00 0.42264E+03 
c  k            0.49532E+00      66   0.38472E-02   0.48309E+00 0.82502E+03 
c  epsilon      0.12744E+05      46   0.39899E-02   0.19598E+10 0.26684E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038567                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.965          38.537           2.211         0.24707
v  Velocity[Y]            -29.463           29.79       Dimensionless distance   yplus :  0.22747E-03 0.29446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13405
   Nb of faces within the viscous sub-layer     :      10835
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.67979E+01     115   0.18597E+00   0.48850E+03 0.65834E+03 
c  Velocity[X]                                      0.14799E+03 
c  Velocity[Y]                                      0.15427E+03 
c  Velocity[Z]                                      0.18623E+03 
c  Pressure     0.16383E+00     701   0.59138E-02   0.39003E+00 0.68301E+03 
c  k            0.53568E+00      67   0.59027E-02   0.80918E+00 0.10650E+04 
c  epsilon      0.12891E+05      47   0.12130E-01   0.34199E+10 0.98200E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0041361                             4
a  epsilon      -0.0041623                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -15.06          38.878          2.2057         0.24654
v  Velocity[Y]            -28.031          31.069         0.90486         0.58774
v  Velocity[Z]            -55.693          94.009         -1.0154      0.00010349
v  ǁVelocityǁ          0.00041455           97.22          6.4551          5.3334
v  Pressure           -4.8893e+05       2.897e+05      1.5651e+05      1.3976e+05
v  k                     3.59e-06          24.783        0.093531        0.050544
v  epsilon              0.0041623       7.692e+06          5467.5          59.959
v  TurbVisc            9.9284e-12          0.3901       0.0019553        0.026371
v  total_pressure           11074       7.897e+05      6.5651e+05      6.3976e+05


 TIME FOR THE TIME STEP              450:        0.62079E+02

===============================================================


 INSTANT    0.451000000E+03   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         0.271878806E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15             Friction velocity        uet   :  0.21128E-01 0.56095E+01
   Friction velocity        uk    :  0.21118E-01 0.60121E+01
   Dimensionless distance   yplus :  0.23102E-03 0.27632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13468
   Nb of faces within the viscous sub-layer     :      10815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68005E+01     115   0.18767E+00   0.45580E+03 0.63576E+03 
c  Velocity[X]                                      0.12831E+03 
c  Velocity[Y]                                      0.13637E+03 
c  Velocity[Z]                                      0.19112E+03 
c  Pressure     0.14211E+00     953   0.60518E-02   0.33975E+00 0.42264E+03 
c  k            0.49532E+00      66   0.38472E-02   0.48309E+00 0.82502E+03 
c  epsilon      0.12744E+05      46   0.39899E-02   0.19598E+10 0.26684E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038567                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.965          38.537           2.211         0.24707
v  Velocity[Y]            -29.463           29.79         0.90407         0.58779
v  Velocity[Z]            -56.033          67.213         -1.0216     -0.00025713
v  ǁVelocityǁ          0.00042737          75.595          6.4731          5.3373
v  Pressure           -4.9157e+05      2.9002e+05       1.569e+05      1.4004e+05
v  k                   3.7837e-06          23.299        0.093937        0.050539
v  epsilon              0.0066322       7.634e+06          5497.6          59.625
v  TurbVisc            1.0224e-11         0.36241       0.0019682        0.026374
v  total_pressure            8427      7.9002e+05       6.569e+05      6.4004e+05


 TIME FOR THE TIME STEP              452:   Rel velocity at the wall uiptn : -0.73816E+02 0.18666E+02
   Friction velocity        uet   :  0.87131E-02 0.56640E+01
   Friction velocity        uk    :  0.87084E-02 0.60173E+01
   Dimensionless distance   yplus :  0.23370E-03 0.26687E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13488
   Nb of faces within the viscous sub-layer     :      10750
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68050E+01     115   0.18799E+00   0.45004E+03 0.63657E+03 
c  Velocity[X]                                      0.13342E+03 
c  Velocity[Y]                                      0.13680E+03 
c  Velocity[Z]                                      0.17981E+03 
c  Pressure     0.12396E+00     716   0.52144E-02   0.29664E+00 0.10858E+04 
c  k            0.49247E+00      68   0.48166E-02   0.61330E+00 0.93185E+03 
c  epsilon      0.12780E+05      46   0.36475E-02   0.20921E+10 0.22773E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037894                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.985          38.217             Friction velocity        uet   :  0.21128E-01 0.56095E+01
   Friction velocity        uk    :  0.21118E-01 0.60121E+01
   Dimensionless distance   yplus :  0.23102E-03 0.27632E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13468
   Nb of faces within the viscous sub-layer     :      10815
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68005E+01     115   0.18767E+00   0.45580E+03 0.63576E+03 
c  Velocity[X]                                      0.12831E+03 
c  Velocity[Y]                                      0.13637E+03 
c  Velocity[Z]                                      0.19112E+03 
c  Pressure     0.14211E+00     953   0.60518E-02   0.33975E+00 0.42264E+03 
c  k            0.49532E+00      66   0.38472E-02   0.48309E+00 0.82502E+03 
c  epsilon      0.12744E+05      46   0.39899E-02   0.19598E+10 0.26684E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038567                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.965          38.537           2.211         0.24707
v  Velocity[Y]            -29.463           29.79         0.90407         0.58779
v  Velocity[Z]            -56.033          67.213         -1.0216     -0.00025713
v  ǁVelocityǁ          0.00042737          75.595          6.4731          5.3373
v  Pressure           -4.9157e+05      2.9002e+05       1.569e+05      1.4004e+05
v  k                   3.7837e-06          23.299        0.093937        0.050539
v  epsilon              0.0066322       7.634e+06          5497.6          59.625
v  TurbVisc            1.0224e-11         0.36241       0.0019682        0.026374
v  total_pressure            8427      7.9002e+05       6.569e+05      6.4004e+05


 TIME FOR THE TIME STEP              452:        0.71790E+02

===============================================================


 INSTANT    0.453000000E+03   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.494190219E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245838E+01
Free inlet               13           0    Rel velocity at the wall uiptn : -0.73816E+02 0.18666E+02
   Friction velocity        uet   :  0.87131E-02 0.56640E+01
   Friction velocity        uk    :  0.87084E-02 0.60173E+01
   Dimensionless distance   yplus :  0.23370E-03 0.26687E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13488
   Nb of faces within the viscous sub-layer     :      10750
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68050E+01     115   0.18799E+00   0.45004E+03 0.63657E+03 
c  Velocity[X]                                      0.13342E+03 
c  Velocity[Y]                                      0.13680E+03 
c  Velocity[Z]                                      0.17981E+03 
c  Pressure     0.12396E+00     716   0.52144E-02   0.29664E+00 0.10858E+04 
c  k            0.49247E+00      68   0.48166E-02   0.61330E+00 0.93185E+03 
c  epsilon      0.12780E+05      46   0.36475E-02   0.20921E+10 0.22773E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037894                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.985          38.217          2.2167         0.24724
v  Velocity[Y]            -28.942          30.447         0.90537         0.58756
v  Velocity[Z]            -59.479          62.081         -1.0297     -0.00036358
v  ǁVelocityǁ          0.00041942          70.547          6.4907          5.3414
v  Pressure           -4.9582e+05      2.9128e+05      1.5756e+05      1.4052e+05
v  k                   3.9856e-06          21.797        0.094406        0.050616
v  epsilon              0.0070331       7.689e+06          5524.1          59.691
v  TurbVisc            1.0272e-11         0.33885       0.0019819        0.026381
v  total_pressure          4182.9      7.9128e+05      6.5756e+0------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82615E+02 0.14690E+02
   Friction velocity        uet   :  0.26496E-01 0.56550E+01
   Friction velocity        uk    :  0.28921E-01 0.60113E+01
   Dimensionless distance   yplus :  0.23045E-03 0.28630E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13567
   Nb of faces within the viscous sub-layer     :      10728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68040E+01     115   0.18517E+00   0.43299E+03 0.62298E+03 
c  Velocity[X]                                      0.13204E+03 
c  Velocity[Y]                                      0.13577E+03 
c  Velocity[Z]                                      0.16519E+03 
c  Pressure     0.12788E+00     609   0.51501E-02   0.30568E+00 0.87614E+03 
c  k            0.50070E+00      68   0.51974E-02   0.91807E+00 0.10329E+04 
c  epsilon      0.12808E+05      46   0.31629E-02   0.12569E+10 0.18026E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038024                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  -------------   Rel velocity at the wall uiptn : -0.73816E+02 0.18666E+02
   Friction velocity        uet   :  0.87131E-02 0.56640E+01
   Friction velocity        uk    :  0.87084E-02 0.60173E+01
   Dimensionless distance   yplus :  0.23370E-03 0.26687E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13488
   Nb of faces within the viscous sub-layer     :      10750
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68050E+01     115   0.18799E+00   0.45004E+03 0.63657E+03 
c  Velocity[X]                                      0.13342E+03 
c  Velocity[Y]                                      0.13680E+03 
c  Velocity[Z]                                      0.17981E+03 
c  Pressure     0.12396E+00     716   0.52144E-02   0.29664E+00 0.10858E+04 
c  k            0.49247E+00      68   0.48166E-02   0.61330E+00 0.93185E+03 
c  epsilon      0.12780E+05      46   0.36475E-02   0.20921E+10 0.22773E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037894                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.985          38.217          2.2167         0.24724
v  Velocity[Y]            -28.942          30.447         0.90537         0.58756
v  Velocity[Z]            -59.479          62.081         -1.0297     -0.00036358
v  ǁVelocityǁ          0.00041942          70.547          6.4907          5.3414
v  Pressure           -4.9582e+05      2.9128e+05      1.5756e+05      1.4052e+05
v  k                   3.9856e-06          21.797        0.094406        0.050616
v  epsilon              0.0070331       7.689e+06          5524.1          59.691
v  TurbVisc            1.0272e-11         0.33885       0.0019819        0.026381
v  total_pressure          4182.9      7.9128e+05      6.5756e+05      6.4052e+05


 TIME FOR THE TIME STEP              454:        0.75885E+02

===============================================================


 INSTANT    0.455000000E+03   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         0.426307688E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46    ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82615E+02 0.14690E+02
   Friction velocity        uet   :  0.26496E-01 0.56550E+01
   Friction velocity        uk    :  0.28921E-01 0.60113E+01
   Dimensionless distance   yplus :  0.23045E-03 0.28630E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13567
   Nb of faces within the viscous sub-layer     :      10728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68040E+01     115   0.18517E+00   0.43299E+03 0.62298E+03 
c  Velocity[X]                                      0.13204E+03 
c  Velocity[Y]                                      0.13577E+03 
c  Velocity[Z]                                      0.16519E+03 
c  Pressure     0.12788E+00     609   0.51501E-02   0.30568E+00 0.87614E+03 
c  k            0.50070E+00      68   0.51974E-02   0.91807E+00 0.10329E+04 
c  epsilon      0.12808E+05      46   0.31629E-02   0.12569E+10 0.18026E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038024                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.903          37.602          2.2218         0.24748
v  Velocity[Y]            -32.181          30.129         0.90811         0.58773
v  Velocity[Z]            -65.557          59.223          -1.037     -0.00036104
v  ǁVelocityǁ          0.00041544          76.717          6.5079          5.3459
v  Pressure           -4.9787e+05      2.9169e+05      1.5761e+05      1.4066e+05
v  k                   4.1831e-06          22.484        0.094762        0.050731
v  epsilon              0.0074307      7.5134e+06          5544.9          59.975
v  TurbVisc            1.0221e-11         0.32659       0.0019946        0.026391
v                                           Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71639E+02 0.22269E+02
   Friction velocity        uet   :  0.28788E-01 0.56396E+01
   Friction velocity        uk    :  0.43448E-01 0.60237E+01
   Dimensionless distance   yplus :  0.22867E-03 0.30428E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13615
   Nb of faces within the viscous sub-layer     :      10692
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68078E+01     115   0.18655E+00   0.46169E+03 0.63455E+03 
c  Velocity[X]                                      0.14018E+03 
c  Velocity[Y]                                      0.13785E+03 
c  Velocity[Z]                                      0.18366E+03 
c  Pressure     0.12630E+00     676   0.55776E-02   0.30050E+00 0.89604E+03 
c  k            0.52691E+00      68   0.79462E-02   0.19686E+01 0.18350E+04 
c  epsilon      0.12999E+05      47   0.56047E-02   0.13538E+11 0.44286E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037634                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.82615E+02 0.14690E+02
   Friction velocity        uet   :  0.26496E-01 0.56550E+01
   Friction velocity        uk    :  0.28921E-01 0.60113E+01
   Dimensionless distance   yplus :  0.23045E-03 0.28630E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13567
   Nb of faces within the viscous sub-layer     :      10728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68040E+01     115   0.18517E+00   0.43299E+03 0.62298E+03 
c  Velocity[X]                                      0.13204E+03 
c  Velocity[Y]                                      0.13577E+03 
c  Velocity[Z]                                      0.16519E+03 
c  Pressure     0.12788E+00     609   0.51501E-02   0.30568E+00 0.87614E+03 
c  k            0.50070E+00      68   0.51974E-02   0.91807E+00 0.10329E+04 
c  epsilon      0.12808E+05      46   0.31629E-02   0.12569E+10 0.18026E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038024                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.903          37.602          2.2218         0.24748
v  Velocity[Y]            -32.181          30.129         0.90811         0.58773
v  Velocity[Z]            -65.557          59.223          -1.037     -0.00036104
v  ǁVelocityǁ          0.00041544          76.717          6.5079          5.3459
v  Pressure           -4.9787e+05      2.9169e+05      1.5761e+05      1.4066e+05
v  k                   4.1831e-06          22.484        0.094762        0.050731
v  epsilon              0.0074307      7.5134e+06          5544.9          59.975
v  TurbVisc            1.0221e-11         0.32659       0.0019946        0.026391
v  total_pressure          2128.9      7.9169e+05      6.5761e+05      6.4066e+05


 TIME FOR THE TIME STEP              456:        0.65068E+02

===============================================================


 INSTANT    0.457000000E+03   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.644624602E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0                                                Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71639E+02 0.22269E+02
   Friction velocity        uet   :  0.28788E-01 0.56396E+01
   Friction velocity        uk    :  0.43448E-01 0.60237E+01
   Dimensionless distance   yplus :  0.22867E-03 0.30428E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13615
   Nb of faces within the viscous sub-layer     :      10692
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68078E+01     115   0.18655E+00   0.46169E+03 0.63455E+03 
c  Velocity[X]                                      0.14018E+03 
c  Velocity[Y]                                      0.13785E+03 
c  Velocity[Z]                                      0.18366E+03 
c  Pressure     0.12630E+00     676   0.55776E-02   0.30050E+00 0.89604E+03 
c  k            0.52691E+00      68   0.79462E-02   0.19686E+01 0.18350E+04 
c  epsilon      0.12999E+05      47   0.56047E-02   0.13538E+11 0.44286E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037634                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.853          39.515          2.2251         0.24701
v  Velocity[Y]            -29.299          30.942         0.91297         0.58767
v  Velocity[Z]             -64.89          70.663         -1.0447     -0.00074723
v  ǁVelocityǁ           0.0004145          75.838          6.5251          5.3509
v  Pressure           -5.0132e+05      2.9277e+05      1.5813e+05      1.4112e+05
v  k                   4.3509e-06          27.789        0.095346         0.05084
v  epsilon              0.0077138      7.6856e+06          5628.1          60.501
v  TurbVisc            1------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69781E+02 0.15778E+02
   Friction velocity        uet   :  0.26709E-01 0.56679E+01
   Friction velocity        uk    :  0.52041E-01 0.60127E+01
   Dimensionless distance   yplus :  0.22891E-03 0.29690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13682
   Nb of faces within the viscous sub-layer     :      10676
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68127E+01     116   0.18480E+00   0.47123E+03 0.63566E+03 
c  Velocity[X]                                      0.13795E+03 
c  Velocity[Y]                                      0.14601E+03 
c  Velocity[Z]                                      0.18727E+03 
c  Pressure     0.11440E+00     590   0.47900E-02   0.27027E+00 0.77014E+03 
c  k            0.55562E+00      66   0.67234E-02   0.15332E+01 0.12678E+04 
c  epsilon      0.13129E+05      47   0.45984E-02   0.37026E+10 0.30545E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038065                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum                                                Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71639E+02 0.22269E+02
   Friction velocity        uet   :  0.28788E-01 0.56396E+01
   Friction velocity        uk    :  0.43448E-01 0.60237E+01
   Dimensionless distance   yplus :  0.22867E-03 0.30428E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13615
   Nb of faces within the viscous sub-layer     :      10692
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68078E+01     115   0.18655E+00   0.46169E+03 0.63455E+03 
c  Velocity[X]                                      0.14018E+03 
c  Velocity[Y]                                      0.13785E+03 
c  Velocity[Z]                                      0.18366E+03 
c  Pressure     0.12630E+00     676   0.55776E-02   0.30050E+00 0.89604E+03 
c  k            0.52691E+00      68   0.79462E-02   0.19686E+01 0.18350E+04 
c  epsilon      0.12999E+05      47   0.56047E-02   0.13538E+11 0.44286E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037634                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.853          39.515          2.2251         0.24701
v  Velocity[Y]            -29.299          30.942         0.91297         0.58767
v  Velocity[Z]             -64.89          70.663         -1.0447     -0.00074723
v  ǁVelocityǁ           0.0004145          75.838          6.5251          5.3509
v  Pressure           -5.0132e+05      2.9277e+05      1.5813e+05      1.4112e+05
v  k                   4.3509e-06          27.789        0.095346         0.05084
v  epsilon              0.0077138      7.6856e+06          5628.1          60.501
v  TurbVisc            1.0199e-11         0.39649       0.0020042          0.0264
v  total_pressure         -1322.6      7.9277e+05      6.5813e+05      6.4112e+05


 TIME FOR THE TIME STEP              458:        0.64667E+02

===============================================================


 INSTANT    0.459000000E+03   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         0.153476522E-17
Rough wall                6           0         0------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69781E+02 0.15778E+02
   Friction velocity        uet   :  0.26709E-01 0.56679E+01
   Friction velocity        uk    :  0.52041E-01 0.60127E+01
   Dimensionless distance   yplus :  0.22891E-03 0.29690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13682
   Nb of faces within the viscous sub-layer     :      10676
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68127E+01     116   0.18480E+00   0.47123E+03 0.63566E+03 
c  Velocity[X]                                      0.13795E+03 
c  Velocity[Y]                                      0.14601E+03 
c  Velocity[Z]                                      0.18727E+03 
c  Pressure     0.11440E+00     590   0.47900E-02   0.27027E+00 0.77014E+03 
c  k            0.55562E+00      66   0.67234E-02   0.15332E+01 0.12678E+04 
c  epsilon      0.13129E+05      47   0.45984E-02   0.37026E+10 0.30545E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038065                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.984          38.897          2.2279         0.24664
v  Velocity[Y]            -29.538          30.869         0.91726         0.58774
v  Velocity[Z]            -57.712          47.088         -1.0491      -0.0006557
v  ǁVelocityǁ          0.00041982          66.669           6.541          5.3545
v  Pressure           -5.0436e+05      2.9386e+05      1.5822e+05      1.4127e+05
v  k                    4.458e-06          32.578        0.095721        0.050912
v  epsilon             ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80444E+02 0.16380E+02
   Friction velocity        uet   :  0.42995E-01 0.56925E+01
   Friction velocity        uk    :  0.47992E-01 0.60408E+01
   Dimensionless distance   yplus :  0.23250E-03 0.28181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13686
   Nb of faces within the viscous sub-layer     :      10640
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68158E+01     115   0.18650E+00   0.47026E+03 0.63752E+03 
c  Velocity[X]                                      0.14107E+03 
c  Velocity[Y]                                      0.14568E+03 
c  Velocity[Z]                                      0.18351E+03 
c  Pressure     0.15297E+00     681   0.53583E-02   0.35865E+00 0.64601E+03 
c  k            0.58893E+00      65   0.50961E-02   0.10008E+01 0.14021E+04 
c  epsilon      0.13389E+05      45   0.48022E-02   0.14319E+11 0.46606E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037972                             3
a  epsilon


  ** Computed fields on cells
     -----------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.69781E+02 0.15778E+02
   Friction velocity        uet   :  0.26709E-01 0.56679E+01
   Friction velocity        uk    :  0.52041E-01 0.60127E+01
   Dimensionless distance   yplus :  0.22891E-03 0.29690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13682
   Nb of faces within the viscous sub-layer     :      10676
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68127E+01     116   0.18480E+00   0.47123E+03 0.63566E+03 
c  Velocity[X]                                      0.13795E+03 
c  Velocity[Y]                                      0.14601E+03 
c  Velocity[Z]                                      0.18727E+03 
c  Pressure     0.11440E+00     590   0.47900E-02   0.27027E+00 0.77014E+03 
c  k            0.55562E+00      66   0.67234E-02   0.15332E+01 0.12678E+04 
c  epsilon      0.13129E+05      47   0.45984E-02   0.37026E+10 0.30545E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038065                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.984          38.897          2.2279         0.24664
v  Velocity[Y]            -29.538          30.869         0.91726         0.58774
v  Velocity[Z]            -57.712          47.088         -1.0491      -0.0006557
v  ǁVelocityǁ          0.00041982          66.669           6.541          5.3545
v  Pressure           -5.0436e+05      2.9386e+05      1.5822e+05      1.4127e+05
v  k                    4.458e-06          32.578        0.095721        0.050912
v  epsilon              0.0077819      7.6861e+06          5658.7           61.01
v  TurbVisc             1.024e-11         0.45446       0.0020112        0.026406
v  total_pressure         -4361.1      7.9386e+05      6.5822e+05      6.4127e+05


 TIME FOR THE TIME STEP              460:        0.57765E+02

===============================================================


 INSTANT    0.461000000E+03   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80444E+02 0.16380E+02
   Friction velocity        uet   :  0.42995E-01 0.56925E+01
   Friction velocity        uk    :  0.47992E-01 0.60408E+01
   Dimensionless distance   yplus :  0.23250E-03 0.28181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13686
   Nb of faces within the viscous sub-layer     :      10640
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68158E+01     115   0.18650E+00   0.47026E+03 0.63752E+03 
c  Velocity[X]                                      0.14107E+03 
c  Velocity[Y]                                      0.14568E+03 
c  Velocity[Z]                                      0.18351E+03 
c  Pressure     0.15297E+00     681   0.53583E-02   0.35865E+00 0.64601E+03 
c  k            0.58893E+00      65   0.50961E-02   0.10008E+01 0.14021E+04 
c  epsilon      0.13389E+05      45   0.48022E-02   0.14319E+11 0.46606E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037972                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.036          38.887          2.2311         0.24689
v  Velocity[Y]            -31.663           30.96         0.92171         0.58766
v  Velocity[Z]            -63.298          88.342         -1.0528     -0.00062076
v  ǁVelocityǁ           0.0004209          92.176           6.557          5.3588
v  Pressure           -5.0524e+05      2.9485e+05       1.586e+05      1.4162e+05
v  k                   4.4726e-06   ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12667E+03 0.15503E+02
   Friction velocity        uet   :  0.44295E-01 0.56449E+01
   Friction velocity        uk    :  0.55265E-01 0.60484E+01
   Dimensionless distance   yplus :  0.23174E-03 0.30428E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13726
   Nb of faces within the viscous sub-layer     :      10633
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68222E+01     115   0.18989E+00   0.49128E+03 0.63859E+03 
c  Velocity[X]                                      0.13975E+03 
c  Velocity[Y]                                      0.14026E+03 
c  Velocity[Z]                                      0.21128E+03 
c  Pressure     0.12603E+00     533   0.49163E-02   0.29439E+00 0.15610E+04 
c  k            0.61048E+00      63   0.33162E-02   0.56909E+00 0.77334E+03 
c  epsilon      0.13555E+05      44   0.26543E-02   0.19083E+10 0.17185E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.00371   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80444E+02 0.16380E+02
   Friction velocity        uet   :  0.42995E-01 0.56925E+01
   Friction velocity        uk    :  0.47992E-01 0.60408E+01
   Dimensionless distance   yplus :  0.23250E-03 0.28181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13686
   Nb of faces within the viscous sub-layer     :      10640
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68158E+01     115   0.18650E+00   0.47026E+03 0.63752E+03 
c  Velocity[X]                                      0.14107E+03 
c  Velocity[Y]                                      0.14568E+03 
c  Velocity[Z]                                      0.18351E+03 
c  Pressure     0.15297E+00     681   0.53583E-02   0.35865E+00 0.64601E+03 
c  k            0.58893E+00      65   0.50961E-02   0.10008E+01 0.14021E+04 
c  epsilon      0.13389E+05      45   0.48022E-02   0.14319E+11 0.46606E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037972                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.036          38.887          2.2311         0.24689
v  Velocity[Y]            -31.663           30.96         0.92171         0.58766
v  Velocity[Z]            -63.298          88.342         -1.0528     -0.00062076
v  ǁVelocityǁ           0.0004209          92.176           6.557          5.3588
v  Pressure           -5.0524e+05      2.9485e+05       1.586e+05      1.4162e+05
v  k                   4.4726e-06          34.433        0.096155        0.050957
v  epsilon              0.0073244      7.6494e+06          5740.4          61.415
v  TurbVisc            1.0292e-11         0.47426       0.0020151        0.026407
v  total_pressure         -5237.4      7.9485e+05       6.586e+05      6.4162e+05


 TIME FOR THE TIME STEP              462:        0.75670E+02

===============================================================


 INSTANT    0.463000000E+03   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                    ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12667E+03 0.15503E+02
   Friction velocity        uet   :  0.44295E-01 0.56449E+01
   Friction velocity        uk    :  0.55265E-01 0.60484E+01
   Dimensionless distance   yplus :  0.23174E-03 0.30428E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13726
   Nb of faces within the viscous sub-layer     :      10633
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68222E+01     115   0.18989E+00   0.49128E+03 0.63859E+03 
c  Velocity[X]                                      0.13975E+03 
c  Velocity[Y]                                      0.14026E+03 
c  Velocity[Z]                                      0.21128E+03 
c  Pressure     0.12603E+00     533   0.49163E-02   0.29439E+00 0.15610E+04 
c  k            0.61048E+00      63   0.33162E-02   0.56909E+00 0.77334E+03 
c  epsilon      0.13555E+05      44   0.26543E-02   0.19083E+10 0.17185E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037139                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.135           38.85          2.2343           0.247
v  Velocity[Y]            -31.252          30.224         0.92368         0.58786
v  Velocity[Z]            -65.845            48.4         -1.0564        -0.00101
v  ǁVelocityǁ          0.00042154          73.707          6.5698          5.3628
v  Pressure           -5.0853e+05        2.95e+05     Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63266E+02 0.17949E+02
   Friction velocity        uet   :  0.42368E-01 0.56974E+01
   Friction velocity        uk    :  0.45876E-01 0.60377E+01
   Dimensionless distance   yplus :  0.23128E-03 0.33411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13719
   Nb of faces within the viscous sub-layer     :      10637
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68356E+01     116   0.18538E+00   0.42006E+03 0.61520E+03 
c  Velocity[X]                                      0.13212E+03 
c  Velocity[Y]                                      0.12723E+03 
c  Velocity[Z]                                      0.16071E+03 
c  Pressure     0.13764E+00     700   0.45548E-02   0.32062E+00 0.89332E+03 
c  k            0.64817E+00      62   0.37754E-02   0.68476E+00 0.96131E+03 
c  epsilon      0.13852E+05      43   0.49133E-02   0.59150E+10 0.36465E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037682                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.022          38.283          2.2358         0.24657
v  Velocity[Y]            -30.331          30.605         0.92334         0.58815
v  Velocity[Z]            -64.672           69.45         -1.0584       -0.001201
v  ǁVelocityǁ          0.00042209          74.151          6.5789          5.3671
v  Pressure           -5.1223e+05       2.953e+05      1.5882e+05      1.4183e+05
v  k                   4.1668e-06          36.087        0.096534        0.051074
v  epsilon              0.0057559      7.5884e+06          5788.8          62.299
v  TurbVisc            1.0324e-11         0.48233        0.002017        0.026409
v  total_pressure          -12229       7.953e+05      6.5882e+05      6.4183e+05


 TIME FOR THE TIME STEP              466:        0.75206E+02

===============================================================


 INSTANT    0.467000000E+03   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.327091156E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13691E+03 0.19774E+02
   Friction velocity        uet   :  0.31495E-01 0.56766E+01
   Friction velocity        uk    :  0.31404E-01 0.60862E+01
   Dimensionless distance   yplus :  0.23162E-03 0.31812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13721
   Nb of faces within the viscous sub-layer     :      10632
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68356E+01     116   0.18938E+00   0.49245E+03 0.64539E+03 
c  Velocity[X]                                      0.13848E+03 
c Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63266E+02 0.17949E+02
   Friction velocity        uet   :  0.42368E-01 0.56974E+01
   Friction velocity        uk    :  0.45876E-01 0.60377E+01
   Dimensionless distance   yplus :  0.23128E-03 0.33411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13719
   Nb of faces within the viscous sub-layer     :      10637
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68356E+01     116   0.18538E+00   0.42006E+03 0.61520E+03 
c  Velocity[X]                                      0.13212E+03 
c  Velocity[Y]                                      0.12723E+03 
c  Velocity[Z]                                      0.16071E+03 
c  Pressure     0.13764E+00     700   0.45548E-02   0.32062E+00 0.89332E+03 
c  k            0.64817E+00      62   0.37754E-02   0.68476E+00 0.96131E+03 
c  epsilon      0.13852E+05      43   0.49133E-02   0.59150E+10 0.36465E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037682                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.022          38.283          2.2358         0.24657
v  Velocity[Y]            -30.331          30.605         0.92334         0.58815
v  Velocity[Z]            -64.672           69.45         -1.0584       -0.001201
v  ǁVelocityǁ          0.00042209          74.151          6.5789       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88969E+02 0.24692E+02
   Friction velocity        uet   :  0.36662E-01 0.56853E+01
   Friction velocity        uk    :  0.35577E-01 0.60555E+01
   Dimensionless distance   yplus :  0.23255E-03 0.34546E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13727
   Nb of faces within the viscous sub-layer     :      10635
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68329E+01     116   0.18735E+00   0.49754E+03 0.64954E+03 
c  Velocity[X]                                      0.15065E+03 
c  Velocity[Y]                                      0.14147E+03 
c  Velocity[Z]                                      0.20542E+03 
c  Pressure     0.14116E+00     483   0.44948E-02   0.32604E+00 0.15172E+04 
c  k            0.65848E+00      66   0.56444E-02   0.14658E+01 0.11220E+04 
c  epsilon      0.14002E+05      46   0.32993E-02   0.21236E+10 0.17116E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038181                             3
a  epsilon       -0.046766                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.033           37.92          2.2375         0.24731
v  Velocity[Y]            -31.625          29.905         0.92196         0.58786
v  Velocity[Z]            -66.534          47.457         -1.0593      -0.0016363
v  ǁVelocityǁ          0.00042812          75.954          6.5856          5.3707
v  Pressure           -5.1582e+05      2.9507e+05      1.5881e+05      1.4188e+05
v  k                   3.8427e-06          33.565        0.096592        0.051079
v  epsilon              0.0049967      7.5863e+06          5800.6          62.508
v  TurbVisc            1.0351e-11         0.47138       0.0020165        0.026406
v  total_pressure          -15817      7.9507e+05      6.5881e+05      6.4188e+05


 TIME FOR THE TIME STEP              468:        0.66273E+02

===============================================================


 INSTANT    0.469000000E+03   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         0.226093223E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92897E+02 0.19251E+02
   Friction velocity        uet   :  0.41361E-01 0.58465E+01
   Friction velocity        uk    :  0.40800E-01 0.60920E+01
   Dimensionless distance   yplus :  0.23331E-03 0.31858E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13713
   Nb of faces within the viscous sub-layer     :      10633
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68435E+01     11Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.88969E+02 0.24692E+02
   Friction velocity        uet   :  0.36662E-01 0.56853E+01
   Friction velocity        uk    :  0.35577E-01 0.60555E+01
   Dimensionless distance   yplus :  0.23255E-03 0.34546E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13727
   Nb of faces within the viscous sub-layer     :      10635
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68329E+01     116   0.18735E+00   0.49754E+03 0.64954E+03 
c  Velocity[X]                                      0.15065E+03 
c  Velocity[Y]                                      0.14147E+03 
c  Velocity[Z]                                      0.20542E+03 
c  Pressure     0.14116E+00     483   0.44948E-02   0.32604E+00 0.15172E+04 
c  k            0.65848E+00      66   0.56444E-02   0.14658E+01 0.11220E+04 
c  epsilon      0.14002E+05      46   0.32993E-02   0.21236E+10 0.17116E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038181                             3
a  epsilon       -0.046766                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.033           37.92          2.2375         0.24731
v  Velocity[Y]            -31.625          29.905         0.92196         0.58786
v  Velocity[Z]            -6Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13058E+03 0.18006E+02
   Friction velocity        uet   :  0.43735E-01 0.56670E+01
   Friction velocity        uk    :  0.43493E-01 0.60367E+01
   Dimensionless distance   yplus :  0.23402E-03 0.36739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13729
   Nb of faces within the viscous sub-layer     :      10639
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68386E+01     116   0.19040E+00   0.49356E+03 0.64528E+03 
c  Velocity[X]                                      0.14499E+03 
c  Velocity[Y]                                      0.14332E+03 
c  Velocity[Z]                                      0.20526E+03 
c  Pressure     0.15880E+00     804   0.55882E-02   0.36526E+00 0.17447E+04 
c  k            0.63534E+00      68   0.10099E-01   0.34201E+01 0.12813E+04 
c  epsilon      0.13963E+05      47   0.51869E-02   0.58598E+09 0.15687E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037596                             3
a  epsilon        -0.27573                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.082          43.451          2.2379         0.24775
v  Velocity[Y]             -32.65          29.708         0.91775         0.58737
v  Velocity[Z]            -83.202          79.336          -1.058      -0.0017402
v  ǁVelocityǁ          0.00043391          92.765          6.5896          5.3745
v  Pressure           -5.1936e+05       2.951e+05      1.5843e+05      1.4171e+05
v  k                   3.4931e-06          29.435        0.096624         0.05103
v  epsilon              0.0043462      7.6883e+06            5808          62.279
v  TurbVisc            1.0371e-11         0.40903       0.0020163        0.026403
v  total_pressure          -19359       7.951e+05      6.5843e+05      6.4171e+05


 TIME FOR THE TIME STEP              470:        0.67897E+02

===============================================================


 INSTANT    0.471000000E+03   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         0.571574299E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14699E+03 0.17547E+02
   Friction velocity        uet   :  0.45622E-01 0.59260E+01
   Friction velocity        uk    :  0.55132E-01 0.60927E+01
   Dimensionless distance   yplus :  0.23621E-03 0.31754E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13745
   Nb of faces within the viscous sub-layer     :      10638
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derivFree inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13058E+03 0.18006E+02
   Friction velocity        uet   :  0.43735E-01 0.56670E+01
   Friction velocity        uk    :  0.43493E-01 0.60367E+01
   Dimensionless distance   yplus :  0.23402E-03 0.36739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13729
   Nb of faces within the viscous sub-layer     :      10639
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68386E+01     116   0.19040E+00   0.49356E+03 0.64528E+03 
c  Velocity[X]                                      0.14499E+03 
c  Velocity[Y]                                      0.14332E+03 
c  Velocity[Z]                                      0.20526E+03 
c  Pressure     0.15880E+00     804   0.55882E-02   0.36526E+00 0.17447E+04 
c  k            0.63534E+00      68   0.10099E-01   0.34201E+01 0.12813E+04 
c  epsilon      0.13963E+05      47   0.51869E-02   0.58598E+09 0.15687E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037596                             3
a  epsilon        -0.27573                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.082          43.451          2.237Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81079E+02 0.27000E+02
   Friction velocity        uet   :  0.25798E-01 0.57004E+01
   Friction velocity        uk    :  0.25860E-01 0.60514E+01
   Dimensionless distance   yplus :  0.23484E-03 0.33133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13730
   Nb of faces within the viscous sub-layer     :      10603
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68438E+01     116   0.18770E+00   0.48208E+03 0.64828E+03 
c  Velocity[X]                                      0.14163E+03 
c  Velocity[Y]                                      0.14355E+03 
c  Velocity[Z]                                      0.19691E+03 
c  Pressure     0.14649E+00     517   0.51783E-02   0.33789E+00 0.90120E+03 
c  k            0.62021E+00      69   0.11448E-01   0.40138E+01 0.14326E+04 
c  epsilon      0.13874E+05      49   0.67157E-02   0.16737E+10 0.14731E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.003837                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.035          43.114          2.2378         0.24813
v  Velocity[Y]            -30.951          29.544         0.91183         0.58742
v  Velocity[Z]            -68.871          47.724         -1.0581      -0.0023766
v  ǁVelocityǁ           0.0004224           81.58          6.5904          5.3778
v  Pressure           -5.2219e+05       2.956e+05      1.5858e+05      1.4181e+05
v  k                     3.15e-06            31.7        0.096772        0.051063
v  epsilon              0.0038337      7.5616e+06          5825.4          62.262
v  TurbVisc            1.0374e-11         0.45628       0.0020186        0.026402
v  total_pressure          -22194       7.956e+05      6.5858e+05      6.4181e+05


 TIME FOR THE TIME STEP              472:        0.57917E+02

===============================================================


 INSTANT    0.473000000E+03   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.808282459E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12848E+03 0.16346E+02
   Friction velocity        uet   :  0.39635E-01 0.56535E+01
   Friction velocity        uk    :  0.39398E-01 0.61170E+01
   Dimensionless distance   yplus :  0.23286E-03 0.27508E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13717
   Nb of faces within the viscous sub-layer     :      10609
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81079E+02 0.27000E+02
   Friction velocity        uet   :  0.25798E-01 0.57004E+01
   Friction velocity        uk    :  0.25860E-01 0.60514E+01
   Dimensionless distance   yplus :  0.23484E-03 0.33133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13730
   Nb of faces within the viscous sub-layer     :      10603
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68438E+01     116   0.18770E+00   0.48208E+03 0.64828E+03 
c  Velocity[X]                                      0.14163E+03 
c  Velocity[Y]                                      0.14355E+03 
c  Velocity[Z]                                      0.19691E+03 
c  Pressure     0.14649E+00     517   0.51783E-02   0.33789E+00 0.90120E+03 
c  k            0.62021E+00      69   0.11448E-01   0.40138E+01 0.14326E+04 
c  epsilon      0.13874E+05      49   0.67157E-02   0.16737E+10 0.14731E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.003837                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83637E+02 0.13833E+02
   Friction velocity        uet   :  0.45569E-01 0.57042E+01
   Friction velocity        uk    :  0.45037E-01 0.60657E+01
   Dimensionless distance   yplus :  0.23308E-03 0.31328E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13709
   Nb of faces within the viscous sub-layer     :      10592
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68572E+01     116   0.19251E+00   0.46956E+03 0.63385E+03 
c  Velocity[X]                                      0.14309E+03 
c  Velocity[Y]                                      0.13967E+03 
c  Velocity[Z]                                      0.18680E+03 
c  Pressure     0.14726E+00     623   0.62540E-02   0.34106E+00 0.33811E+03 
c  k            0.60021E+0Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81079E+02 0.27000E+02
   Friction velocity        uet   :  0.25798E-01 0.57004E+01
   Friction velocity        uk    :  0.25860E-01 0.60514E+01
   Dimensionless distance   yplus :  0.23484E-03 0.33133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13730
   Nb of faces within the viscous sub-layer     :      10603
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68438E+01     116   0.18770E+00   0.48208E+03 0.64828E+03 
c  Velocity[X]                                      0.14163E+03 
c  Velocity[Y]                                      0.14355E+03 
c  Velocity[Z]                                      0.19691E+03 
c  Pressure     0.14649E+00     517   0.51783E-02   0.33789E+00 0.90120E+03 
c  k            0.62021E+00      69   0.11448E-01   0.40138E+01 0.14326E+04 
c  epsilon      0.13874E+05      49   0.67157E-02   0.16737E+10 0.14731E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.003837                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.035          43.114          2.2378         0.24813
v  Velocity[Y]            -30.951          29.544         0.91183         0.58742
v  Velocity[Z]            -68.871          47.724         -1.0581      -0.0023766
v  ǁVelocityǁ           0.0004224           81.58          6.5904          5.3778
v  Pressure           -5.2219e+05       2.956e+05      1.5858e+05      1.4181e+05
v  k                     3.15e-06            31.7        0.096772        0.051063
v  epsilon              0.0038337      7.5616e+06          5825.4          62.262
v  TurbVisc            1.0374e-11         0.45628       0.0020186        0.026402
v  total_pressure          -22194       7.956e+05      6.5858e+05      6.4181e+05


 TIME FOR THE TIME STEP              472:        0.67383E+02

=====================================Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.83637E+02 0.13833E+02
   Friction velocity        uet   :  0.45569E-01 0.57042E+01
   Friction velocity        uk    :  0.45037E-01 0.60657E+01
   Dimensionless distance   yplus :  0.23308E-03 0.31328E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13709
   Nb of faces within the viscous sub-layer     :      10592
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68572E+01     116   0.19251E+00   0.46956E+03 0.63385E+03 
c  Velocity[X]                                      0.14309E+03 
c  Velocity[Y]                                      0.13967E+03 
c  Velocity[Z]                                      0.18680E+03 
c  Pressure     0.14726E+00     623   0.62540E-02   0.34106E+00 0.33811E+03 
c  k            0.60021E+00      68   0.99948E-02   0.40155E+01 0.12383E+04 
c  epsilon      0.13675E+05      46   0.58510E-02   0.96566E+09 0.71468E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038137                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.626380013E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97529E+02 0.18030E+02
   Friction velocity        uet   :  0.44544E-01 0.60267E+01
   Friction velocity        uk    :  0.48734E-01 0.60663E+01
   Dimensionless distance   yplus :  0.23245E-03 0.29236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13709
   Nb of faces within the viscous sub-layer     :      10597
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68681E+01     115   0.18674E+00   0.48053E+03 0.64699E+03 
c  Velocity[X]                                      0.13949E+03 
c  Velocity[Y]                                      0.14247E+03 
c  Velocity[Z]                                      0.19857E+03 
c  Pressure     0.14184E+00     555   0.64133E-02   0.32962E+00 0.49891E+03 
c  k            0.65861E+00      72   0.55750E-02   0.17071E+01 0.97068E+03 
c  epsilon      0.13813E+05      51   0.36023E-02   0.51199E+09 0.18203E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0036664                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -14.92          37.718          2.2366         0.25028
v  Velocity[Y]            -32.363          29.585         0.90246         0.58686
v  Velocity[Z]            -67.299          46.579          -1.057      -0.0025573
v  ǁVelocityǁ          0.00043008           75.19          6.5906          5.3857
v  Pressure              -5.3e+05      2.9573e+05      1.5877e+05      1.4193e+05
v  k                   2.5897e-06          37.583        0.096971        0.051198
v  epsilon              0.0032279      7.6362e+06          5822.7          62.674
v  TurbVisc            1.0366e-11         0.56516       0.0020276        0.026403
v  total_pressure          -30003      7.9573e+05      6.5877e+05      6.4193e+05


 TIME FOR THE TIME STEP              476:        0.70897E+02

===============================================================


 INSTANT    0.477000000E+03   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.591026887E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.85946E+02 0.30510E+02
   Friction velocity        uet   :  0.22452E-01 0.57967E+01
   Friction velocity        uk    :  0.37973E-01 0.61117E+01
   Dimensionless distance   yplus :  0.23399E-03 0.30426E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13681
   Nb of faces within the viscous sub-layer     :      10600
   Total number of wall faces                   :      41Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.626380013E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97529E+02 0.18030E+02
   Friction velocity        uet   :  0.44544E-01 0.60267E+01
   Friction velocity        uk    :  0.48734E-01 0.60663E+01
   Dimensionless distance   yplus :  0.23245E-03 0.29236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13709
   Nb of faces within the viscous sub-layer     :      10597
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68681E+01     115   0.18674E+00   0.48053E+03 0.64699E+03 
c  Velocity[X]                                      0.13949E+03 
c  Velocity[Y]                                      0.14247E+03 
c  Velocity[Z]                                      0.19857E+03 
c  Pressure     0.14184E+00     555   0.64133E-02   0.32962E+00 0.49891E+03 
c  k            0.65861E+00      72   0.55750E-02   0.17071E+01 0.97068E+03 
c  epsilon      0.13813E+05      51   0.36023E-02   0.51199E+09 0.18203E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0036664                             2
a  epsilon


  ** Computed fields on cells
   ---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.714295500E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77414E+02 0.18677E+02
   Friction velocity        uet   :  0.30120E-01 0.56834E+01
   Friction velocity        uk    :  0.30003E-01 0.60282E+01
   Dimensionless distance   yplus :  0.23347E-03 0.30012E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13711
   Nb of faces within the viscous sub-layer     :      10594
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68789E+01     115   0.19073E+00   0.49354E+03 0.63299E+03 
c  Velocity[X]                                      0.14386E+03 
c  Velocity[Y]                           Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.626380013E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97529E+02 0.18030E+02
   Friction velocity        uet   :  0.44544E-01 0.60267E+01
   Friction velocity        uk    :  0.48734E-01 0.60663E+01
   Dimensionless distance   yplus :  0.23245E-03 0.29236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13709
   Nb of faces within the viscous sub-layer     :      10597
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68681E+01     115   0.18674E+00   0.48053E+03 0.64699E+03 
c  Velocity[X]                                      0.13949E+03 
c  Velocity[Y]                                      0.14247E+03 
c  Velocity[Z]                                      0.19857E+03 
c  Pressure     0.14184E+00     555   0.64133E-02   0.32962E+00 0.49891E+03 
c  k            0.65861E+00      72   0.55750E-02   0.17071E+01 0.97068E+03 
c  epsilon      0.13813E+05      51   0.36023E-02   0.51199E+09 0.18203E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0036664                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -14.92          37.718          2.2366         0.25028
v  Velocity[Y]            -32.363          29.585         0.90246         0.58686
v  Velocity[Z]            -67.299          46.579          -1.057      -0.0025573
v  ǁVelocityǁ          0.00043008           75.19          6.5906          5.3857
v  Pressure              -5.3e+05      2.9573e+05      1.5877e+05      1.4193e+05
v  k                   2.5897e-06          37.583        0.096971        0.051198
v  epsilon              0.0032279      7.6362e+06          5822.7          62.674
v  TurbVisc            1.0366e-11         0.56516       0.0020276        ---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.714295500E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.77414E+02 0.18677E+02
   Friction velocity        uet   :  0.30120E-01 0.56834E+01
   Friction velocity        uk    :  0.30003E-01 0.60282E+01
   Dimensionless distance   yplus :  0.23347E-03 0.30012E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13711
   Nb of faces within the viscous sub-layer     :      10594
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68789E+01     115   0.19073E+00   0.49354E+03 0.63299E+03 
c  Velocity[X]                                      0.14386E+03 
c  Velocity[Y]                                      0.14216E+03 
c  Velocity[Z]                                      0.20752E+03 
c  Pressure     0.15135E+00     603   0.55953E-02   0.34843E+00 0.58391E+03 
c  k            0.66372E+00      70   0.47483E-02   0.14051E+01 0.11063E+04 
c  epsilon      0.13870E+05      50   0.30896E-02   0.13620E+10 0.18640E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.003574---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.613982375E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245860E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12252E+03 0.18338E+02
   Friction velocity        uet   :  0.34679E-01 0.56633E+01
   Friction velocity        uk    :  0.33681E-01 0.60655E+01
   Dimensionless distance   yplus :  0.23613E-03 0.27706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13704
   Nb of faces within the viscous sub-layer     :      10568
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68887E+01     114   0.18775E+00   0.48607E+03 0.63956E+03 
c  Velocity[X]                                      0.14408E+03 
c  Velocity[Y]                                      0.14354E+03 
c  Velocity[Z]                                      0.19844E+03 
c  Pressure     0.14657E+00     614   0.56361E-02   0.33723E+00 0.78047E+03 
c  k            0.64312E+00      67   0.45947E-02   0.81820E+00 0.96962E+03 
c  epsilon      0.13828E+05      47   0.34851E-02   0.26285E+10 0.21002E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0035881                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.648          36.741          2.2367          0.2525
v  Velocity[Y]             -31.78          29.649         0.89701         0.58554
v  Velocity[Z]            -54.881          48.918         -1.0588      -0.0024565
v  ǁVelocityǁ          0.00043808          65.979          6.5963          5.3945
v  Pressure           -5.3571e+05      2.9593e+05      1.5916e+05      1.4227e+05
v  k                   1.5534e-06          37.833        0.097319         0.05129
v  epsilon              0.0029821      7.6722e+06          5830.4          62.861
v  TurbVisc              6.57e-15         0.52981       0.0020434        0.026408
v  total_pressure          -35712      7.9593e+05      6.5916e+05      6.4227e+05


 TIME FOR THE TIME STEP              480:        0.72781E+02

===============================================================


 INSTANT    0.481000000E+03   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         0.505113075E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98385E+02 0.23654E+02
   Friction velocity        uet   :  0.23103E-01 0.56039E+01
   Friction velocity        uk    :  0.24053E-01 0.61007E+01
   Dimensionless distance   yplus :  0.23716E-03 0.27894E+02
   -------------------------------------------------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.613982375E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245860E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12252E+03 0.18338E+02
   Friction velocity        uet   :  0.34679E-01 0.56633E+01
   Friction velocity        uk    :  0.33681E-01 0.60655E+01
   Dimensionless distance   yplus :  0.23613E-03 0.27706E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13704
   Nb of faces within the viscous sub-layer     :      10568
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.68887E+01     114   0.18775E+00   0.48607E+03 0.63956E+03 
c  Velocity[X]                                      0.14408E+03 
c  Velocity[Y]                                      0.14354E+03 
c  Velocity[Z]                                      0.19844E+03 
c  Pressure     0.14657E+00     614   0.56361E-02   0.33723E+00 0.78047E+03 
c  k            0.64312E+00      67   0.45947E-02   0.81820E+00 0.96962E+03 
c  epsilon      0.13828E+05      47   0.34851E-02   0.26285E+10 0.21002E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  cl   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.339182129E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245847E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66754E+02 0.19821E+02
   Friction velocity        uet   :  0.35359E-01 0.56687E+01
   Friction velocity        uk    :  0.34410E-01 0.60292E+01
   Dimensionless distance   yplus :  0.23655E-03 0.28382E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13696
   Nb of faces within the viscous sub-layer     :      10562
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69029E+01     114   0.18733E+00   0.44752E+03 0.62543E+03 
c  Velocity[X]                                      0.14130E+03 
c  Velocity[Y]                                      0.14314E+03 
c  Velocity[Z]                                      0.16308E+03 
c  Pressure     0.14357E+00     612   0.49001E-02   0.33006E+00 0.10037E+04 
c  k            0.61153E+00      66   0.43825E-02   0.93656E+00 0.11963E+04 
c  epsilon      0.13666E+05      45   0.39522E-02   0.58358E+10 0.34421E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038433                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.542          38.143          2.2372           0.253
v  Velocity[Y]            -30.255          30.253         0.89438         0.58518
v  Velocity[Z]            -56.246          65.759         -1.0614      -0.0020278
v  ǁVelocityǁ          0.00043382          69.581          6.5996          5.3978
v  Pressure            -5.368e+05      2.9586e+05      1.5915e+05      1.4234e+05
v  k                   2.1486e-06          32.317         0.09731        0.051277
v  epsilon               0.002908      7.6067e+06          5816.1          62.497
v  TurbVisc            1.0391e-11         0.46148       0.0020532        0.026411
v  total_pressure          -36795      7.9586e+05      6.5915e+05      6.4234e+05


 TIME FOR THE TIME STEP              482:        0.69563E+02

===============================================================


 INSTANT    0.483000000E+03   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.853372879E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11246E+03 0.24158E+02
   Friction velocity        uet   :  0.13739E-01 0.56244E+01
   Friction velocity        uk    :  0.25921E-01 0.60114E+01
   Dimensionless distance   yplus :   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.339182129E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245847E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66754E+02 0.19821E+02
   Friction velocity        uet   :  0.35359E-01 0.56687E+01
   Friction velocity        uk    :  0.34410E-01 0.60292E+01
   Dimensionless distance   yplus :  0.23655E-03 0.28382E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13696
   Nb of faces within the viscous sub-layer     :      10562
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69029E+01     114   0.18733E+00   0.44752E+03 0.62543E+03 
c  Velocity[X]                                      0.14130E+03 
c  Velocity[Y]                                      0.14314E+03 
c  Velocity[Z]                                      0.16308E+03 
c  Pressure     0.14357E+00     612   0.49001E-02   0.33006E+00 0.10037E+04 
c  k            0.61153E+00      66   0.43825E-02   0.93656E+00 0.11963E+04 
c  epsilon      0.13666E+05      45   0.39522E-02   0.58358E+10 0.34421E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     --------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.738119525E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59193E+02 0.16123E+02
   Friction velocity        uet   :  0.29051E-01 0.56730E+01
   Friction velocity        uk    :  0.29102E-01 0.60108E+01
   Dimensionless distance   yplus :  0.23416E-03 0.31085E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13690
   Nb of faces within the viscous sub-layer     :      10522
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69173E+01     114   0.18825E+00   0.46851E+03 0.62763E+03 
c  Velocity[X]                                      0.14097E+03 
c  Velocity[Y]                                      0.14207E+03 
c  Velocity[Z]                                      0.18546E+03 
c  Pressure     0.13889E+00     604   0.55251E-02   0.31827E+00 0.17842E+04 
c  k            0.62841E+00      66   0.59866E-02   0.18949E+01 0.12053E+04 
c  epsilon      0.13785E+05      45   0.43342E-02   0.27179E+10 0.23415E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0036381                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.566          36.955          2.2387         0.25436
v  Velocity[Y]                -32          29.755         0.89187         0.58544
v  Velocity[Z]            -63.331          47.989         -1.0667       -0.002569
v  ǁVelocityǁ          0.00042593          71.032          6.6032          5.4019
v  Pressure           -5.3796e+05      2.9569e+05      1.5908e+05      1.4238e+05
v  k                   2.0711e-06          37.316        0.097633        0.051327
v  epsilon              0.0028365      7.6238e+06          5847.6          62.644
v  TurbVisc             1.034e-11         0.47917        0.002063        0.026413
v  total_pressure          -37959      7.9569e+05      6.5908e+05      6.4238e+05


 TIME FOR THE TIME STEP              484:        0.71053E+02

===============================================================


 INSTANT    0.485000000E+03   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.647948771E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245847E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76182E+02 0.17603E+02
   Friction velocity        uet   :  0.30304E-01 0.56039E+01
   Friction velocity         ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.738119525E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.59193E+02 0.16123E+02
   Friction velocity        uet   :  0.29051E-01 0.56730E+01
   Friction velocity        uk    :  0.29102E-01 0.60108E+01
   Dimensionless distance   yplus :  0.23416E-03 0.31085E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13690
   Nb of faces within the viscous sub-layer     :      10522
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69173E+01     114   0.18825E+00   0.46851E+03 0.62763E+03 
c  Velocity[X]                                      0.14097E+03 
c  Velocity[Y]                                      0.14207E+03 
c  Velocity[Z]                                      0.18546E+03 
c  Pressure     0.13889E+00     604   0.55251E-02   0.31827E+00 0.17842E+04 
c  k            0.62841E+00      66   0.59866E-02   0.18949E+01 0.12053E+04 
c  epsilon      0.13785E+05      45   0.43342E-02   0.27179E+10 0.23415E+05 
----------------------------------------------------------------------- INSTANT    0.486000000E+03   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         0.119394496E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80005E+02 0.19997E+02
   Friction velocity        uet   :  0.37923E-01 0.56450E+01
   Friction velocity        uk    :  0.36783E-01 0.60333E+01
   Dimensionless distance   yplus :  0.23261E-03 0.30990E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13680
   Nb of faces within the viscous sub-layer     :      10501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69271E+01     113   0.18925E+00   0.45623E+03 0.62060E+03 
c  Velocity[X]                                      0.14283E+03 
c  Velocity[Y]                                      0.14464E+03 
c  Velocity[Z]                                      0.16876E+03 
c  Pressure     0.13962E+00     719   0.43961E-02   0.31787E+00 0.95220E+03 
c  k            0.68643E+00      65   0.95615E-02   0.31006E+01 0.11727E+04 
c  epsilon      0.14028E+05      47   0.58222E-02   0.15321E+10 0.20366E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.003746                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.638          37.095           2.239         0.25469
v  Velocity[Y]            -31.418          29.693         0.89053          0.5856
v  Velocity[Z]            -53.499          70.762         -1.0696      -0.0019028
v  ǁVelocityǁ          0.00042267           74.66          6.6053          5.4042
v  Pressure           -5.4063e+05      2.9535e+05      1.5898e+05      1.4241e+05
v  k                   1.9994e-06          42.505        0.097811        0.051456
v  epsilon              0.0027525      7.6388e+06          5839.2          63.183
v  TurbVisc            1.0283e-11         0.53457       0.0020757        0.026416
v  total_pressure          -40633      7.9535e+05      6.5898e+05      6.4241e+05


 TIME FOR THE TIME STEP              486:        0.66297E+02

===============================================================


 INSTANT    0.487000000E+03   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         0.675906832E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13691E+03 0.24219E+02
   Friction velocity       INSTANT    0.486000000E+03   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         0.119394496E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.80005E+02 0.19997E+02
   Friction velocity        uet   :  0.37923E-01 0.56450E+01
   Friction velocity        uk    :  0.36783E-01 0.60333E+01
   Dimensionless distance   yplus :  0.23261E-03 0.30990E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13680
   Nb of faces within the viscous sub-layer     :      10501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69271E+01     113   0.18925E+00   0.45623E+03 0.62060E+03 
c  Velocity[X]                                      0.14283E+03 
c  Velocity[Y]                                      0.14464E+03 
c  Velocity[Z]                                      0.16876E+03 
c  Pressure     0.13962E+00     719   0.43961E-02   0.31787E+00 0.95220E+03 
c  k            0.68643E+00      65   0.95615E-02   0.31006E+01 0.11727E+04 
c  epsilon      0.14028E+05      47   0.58222E-02   0.15321E+10 0.20366E+05 
-----===============================================================


 INSTANT    0.488000000E+03   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         0.550321488E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63418E+02 0.19937E+02
   Friction velocity        uet   :  0.28597E-01 0.56947E+01
   Friction velocity        uk    :  0.28981E-01 0.60773E+01
   Dimensionless distance   yplus :  0.23073E-03 0.30022E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13678
   Nb of faces within the viscous sub-layer     :      10526
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69310E+01     113   0.18662E+00   0.45610E+03 0.62986E+03 
c  Velocity[X]                                      0.14161E+03 
c  Velocity[Y]                                      0.13330E+03 
c  Velocity[Z]                                      0.18119E+03 
c  Pressure     0.11701E+00     537   0.46026E-02   0.26761E+00 0.12054E+04 
c  k            0.62308E+00      70   0.67929E-02   0.27816E+01 0.14226E+04 
c  epsilon      0.13872E+05      48   0.54297E-02   0.23740E+10 0.35698E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0037409                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.707          36.847          2.2403         0.25558
v  Velocity[Y]            -36.572          29.808         0.88893         0.58582
v  Velocity[Z]            -54.881          48.779         -1.0727      -0.0022834
v  ǁVelocityǁ          0.00041918          61.734           6.607          5.4071
v  Pressure           -5.4115e+05      2.9519e+05      1.5891e+05      1.4246e+05
v  k                   1.9417e-06          30.683        0.097702        0.051382
v  epsilon              0.0026593       7.706e+06          5822.1           62.67
v  TurbVisc            1.0181e-11         0.46781       0.0020875        0.026419
v  total_pressure          -41150      7.9519e+05      6.5891e+05      6.4246e+05


 TIME FOR THE TIME STEP              488:        0.63287E+02

===============================================================


 INSTANT    0.489000000E+03   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.400312760E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245867E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at th===============================================================


 INSTANT    0.488000000E+03   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         0.550321488E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245841E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63418E+02 0.19937E+02
   Friction velocity        uet   :  0.28597E-01 0.56947E+01
   Friction velocity        uk    :  0.28981E-01 0.60773E+01
   Dimensionless distance   yplus :  0.23073E-03 0.30022E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13678
   Nb of faces within the viscous sub-layer     :      10526
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69310E+01     113   0.18662E+00   0.45610E+03 0.62986E+03 
c  Velocity[X]                                      0.14161E+03 
c  Velocity[Y]                                      0.13330E+03 
c  Velocity[Z]                                      0.18119E+03 
c  Pressure     0.11701E+00     537   0.46026E-02   0.26761E+00 0.12054E+04 
c  k            0.62308E+00      70   0.67929E-02   0.27816E+01 0.14226E+04 
c  epsilon      0.13 TIME FOR THE TIME STEP              489:        0.65636E+02

===============================================================


 INSTANT    0.490000000E+03   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.203837358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86384E+02 0.21107E+02
   Friction velocity        uet   :  0.21357E-01 0.56810E+01
   Friction velocity        uk    :  0.55064E-01 0.60379E+01
   Dimensionless distance   yplus :  0.23058E-03 0.30122E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13696
   Nb of faces within the viscous sub-layer     :      10519
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69368E+01     112   0.18876E+00   0.46666E+03 0.62239E+03 
c  Velocity[X]                                      0.14099E+03 
c  Velocity[Y]                                      0.14470E+03 
c  Velocity[Z]                                      0.18098E+03 
c  Pressure     0.13374E+00     677   0.50956E-02   0.30492E+00 0.31572E+03 
c  k            0.56177E+00      72   0.41820E-02   0.94155E+00 0.11341E+04 
c  epsilon      0.13574E+05      52   0.38551E-02   0.32310E+10 0.31908E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0034832                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.594          36.628           2.241         0.25585
v  Velocity[Y]            -32.435          30.149         0.88843         0.58612
v  Velocity[Z]            -59.611          78.202         -1.0744      -0.0018408
v  ǁVelocityǁ          0.00041575          84.929          6.6093           5.409
v  Pressure           -5.4403e+05      2.9553e+05      1.5895e+05      1.4254e+05
v  k                   1.7261e-06          27.217        0.097596        0.051271
v  epsilon              0.0025594      7.6597e+06          5805.9          61.841
v  TurbVisc            1.0098e-11         0.36814       0.0020949        0.026419
v  total_pressure          -44032      7.9553e+05      6.5895e+05      6.4254e+05


 TIME FOR THE TIME STEP              490:        0.69504E+02

===============================================================


 INSTANT    0.491000000E+03   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         0.330657179E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
-------------------- TIME FOR THE TIME STEP              489:        0.69443E+02

===============================================================


 INSTANT    0.490000000E+03   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000        -0.203837358E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245864E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86384E+02 0.21107E+02
   Friction velocity        uet   :  0.21357E-01 0.56810E+01
   Friction velocity        uk    :  0.55064E-01 0.60379E+01
   Dimensionless distance   yplus :  0.23058E-03 0.30122E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13696
   Nb of faces within the viscous sub-layer     :      10519
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69368E+01     112   0.18876E+00   0.46666E+03 0.62239E+03 
c  Velocity[X]                                      0.14099E+03 
c  Velocity[Y]                                      0.14470E+03 
c  Velocity[Z]                                      0.18098E+03 
c  Pressure     0.13374E+00     677   0.50956E-02   0.30492E+00 0.31572E+03 
c  k         v  total_pressure          -42760      7.9518e+05      6.5886e+05      6.4251e+05


 TIME FOR THE TIME STEP              491:        0.65791E+02

===============================================================


 INSTANT    0.492000000E+03   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         0.581447110E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10620E+03 0.22118E+02
   Friction velocity        uet   :  0.42496E-01 0.57017E+01
   Friction velocity        uk    :  0.57367E-01 0.60680E+01
   Dimensionless distance   yplus :  0.22926E-03 0.30427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13698
   Nb of faces within the viscous sub-layer     :      10537
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69373E+01     111   0.18888E+00   0.48083E+03 0.63865E+03 
c  Velocity[X]                                      0.14360E+03 
c  Velocity[Y]                                      0.13923E+03 
c  Velocity[Z]                                      0.19800E+03 
c  Pressure     0.11417E+00     694   0.45462E-02   0.26097E+00 0.35857E+03 
c  k            0.59270E+00      69   0.60749E-02   0.95806E+00 0.90699E+03 
c  epsilon      0.13649E+05      49   0.36579E-02   0.88154E+09 0.14785E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0035824                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.616          37.373          2.2418          0.2565
v  Velocity[Y]            -33.607          29.677         0.88751         0.58522
v  Velocity[Z]            -53.215          47.074          -1.074      -0.0016054
v  ǁVelocityǁ            0.000414          65.117          6.6103          5.4114
v  Pressure           -5.4324e+05      2.9483e+05      1.5869e+05      1.4237e+05
v  k                   2.3402e-07          29.458        0.097536        0.051326
v  epsilon              0.0024518      7.7106e+06          5779.8          62.141
v  TurbVisc            1.0019e-11         0.38402       0.0020988         0.02642
v  total_pressure          -43238      7.9483e+05      6.5869e+05      6.4237e+05


 TIME FOR THE TIME STEP              492:        0.72133E+02

===============================================================


 INSTANT    0.493000000E+03   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         0.109596521E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245866E+01
Free inlet               13           0         0.000000000E+00
Convective 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  total_pressure          -42760      7.9518e+05      6.5886e+05      6.4251e+05


 TIME FOR THE TIME STEP              491:        0.60992E+02

===============================================================


 INSTANT    0.492000000E+03   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         0.581447110E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245844E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10620E+03 0.22118E+02
   Friction velocity        uet   :  0.42496E-01 0.57017E+01
   Friction velocity        uk    :  0.57367E-01 0.60680E+01
   Dimensionless distance   yplus :  0.22926E-03 0.30427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13698
   Nb of faces within the viscous sub-layer     :      10537
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69373E+01     111   0.18888E+00   0.48083E+03 0.63865E+03 
c  Velocity[X]                                      0.14360E+03 
c  Velocity[Y]                                      0.13923E+03 
c  Velocity[Z]                                      0.19800E+03 
c  Pressv  TurbVisc            2.6211e-14         0.41255       0.0020999        0.026421
v  total_pressure          -39486      7.9559e+05      6.5919e+05      6.4276e+05


 TIME FOR THE TIME STEP              493:        0.74524E+02

===============================================================


 INSTANT    0.494000000E+03   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.309927481E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10595E+03 0.20994E+02
   Friction velocity        uet   :  0.26992E-01 0.57047E+01
   Friction velocity        uk    :  0.27059E-01 0.60607E+01
   Dimensionless distance   yplus :  0.22993E-03 0.31464E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13738
   Nb of faces within the viscous sub-layer     :      10543
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69401E+01     111   0.18722E+00   0.47843E+03 0.62908E+03 
c  Velocity[X]                                      0.14892E+03 
c  Velocity[Y]                                      0.15137E+03 
c  Velocity[Z]                                      0.17813E+03 
c  Pressure     0.12034E+00     645   0.47821E-02   0.27479E+00 0.10394E+04 
c  k            0.64957E+00      66   0.41641E-02   0.77378E+00 0.79841E+03 
c  epsilon      0.13823E+05      45   0.35843E-02   0.84466E+09 0.12109E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0036635                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.672          38.177           2.242         0.25699
v  Velocity[Y]            -33.471          29.936         0.88746         0.58574
v  Velocity[Z]            -53.124          66.259         -1.0736      -0.0014316
v  ǁVelocityǁ          0.00041724          71.161           6.612           5.414
v  Pressure           -5.4033e+05      2.9516e+05      1.5869e+05      1.4238e+05
v  k                   1.8168e-06          31.018        0.097508         0.05144
v  epsilon              0.0023425      7.5675e+06          5750.3          62.822
v  TurbVisc            1.0044e-11         0.44541       0.0021003        0.026421
v  total_pressure          -40328      7.9516e+05      6.5869e+05      6.4238e+05


 TIME FOR THE TIME STEP              494:        0.65647E+02

===============================================================


 INSTANT    0.495000000E+03   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.469353056E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245845E+01
Free inlet               13           0         0.000000000E+00
Convective 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  TurbVisc            2.6211e-14         0.41255       0.0020999        0.026421
v  total_pressure          -39486      7.9559e+05      6.5919e+05      6.4276e+05


 TIME FOR THE TIME STEP              493:        0.80168E+02

===============================================================


 INSTANT    0.494000000E+03   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.309927481E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10595E+03 0.20994E+02
   Friction velocity        uet   :  0.26992E-01 0.57047E+01
   Friction velocity        uk    :  0.27059E-01 0.60607E+01
   Dimensionless distance   yplus :  0.22993E-03 0.31464E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13738
   Nb of faces within the viscous sub-layer     :      10543
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69401E+01     111   0.18722E+00   0.47843E+03 0.62908E+03 
c  Velocity[X]                                      0.14892E+03 
c  Velocity[Y]                                      0.15v  epsilon              0.0022891      7.6498e+06          5766.1          62.955
v  TurbVisc             1.005e-11         0.45313       0.0021006        0.026422
v  total_pressure          -38906       7.955e+05       6.591e+05      6.4268e+05


 TIME FOR THE TIME STEP              495:        0.63524E+02

===============================================================


 INSTANT    0.496000000E+03   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         0.343576348E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75570E+02 0.20039E+02
   Friction velocity        uet   :  0.44612E-01 0.57284E+01
   Friction velocity        uk    :  0.52196E-01 0.60667E+01
   Dimensionless distance   yplus :  0.23005E-03 0.32948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13732
   Nb of faces within the viscous sub-layer     :      10559
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69406E+01     112   0.18653E+00   0.45894E+03 0.62151E+03 
c  Velocity[X]                                      0.14625E+03 
c  Velocity[Y]                                      0.13944E+03 
c  Velocity[Z]                                      0.17325E+03 
c  Pressure     0.11971E+00     877   0.45030E-02   0.27218E+00 0.14703E+04 
c  k            0.66535E+00      63   0.45866E-02   0.71866E+00 0.86099E+03 
c  epsilon      0.13949E+05      42   0.50549E-02   0.33874E+10 0.22243E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038434                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -14.658          36.788           2.241         0.25762
v  Velocity[Y]            -33.462           29.94         0.88623          0.5852
v  Velocity[Z]            -55.626           46.79          -1.075      -0.0017404
v  ǁVelocityǁ          0.00041386          67.369          6.6114          5.4162
v  Pressure           -5.3873e+05       2.951e+05      1.5861e+05      1.4234e+05
v  k                   1.1901e-06          32.399        0.097531        0.051485
v  epsilon              0.0022362      7.6401e+06          5762.4          63.165
v  TurbVisc            1.2793e-15         0.45309       0.0020994        0.026421
v  total_pressure          -38726       7.951e+05      6.5861e+05      6.4234e+05


 TIME FOR THE TIME STEP              496:        0.68286E+02

===============================================================


 INSTANT    0.497000000E+03   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         0.298592272E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245842E+01
Free inlet               13           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  epsilon              0.0022891      7.6498e+06          5766.1          62.955
v  TurbVisc             1.005e-11         0.45313       0.0021006        0.026422
v  total_pressure          -38906       7.955e+05       6.591e+05      6.4268e+05


 TIME FOR THE TIME STEP              495:        0.65518E+02

===============================================================


 INSTANT    0.496000000E+03   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         0.343576348E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75570E+02 0.20039E+02
   Friction velocity        uet   :  0.44612E-01 0.57284E+01
   Friction velocity        uk    :  0.52196E-01 0.60667E+01
   Dimensionless distance   yplus :  0.23005E-03 0.32948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13732
   Nb of faces within the viscous sub-layer     :      10559
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69406E+01     112   0.18653E+00   0.45894E+03 0.62151E+03 
c  Velocity[X]                         v  k                   1.7831e-06          31.869        0.097491        0.051475
v  epsilon              0.0021838      7.7548e+06          5753.6          63.115
v  TurbVisc            4.9518e-12         0.45316       0.0021002        0.026421
v  total_pressure          -35531      7.9578e+05      6.5897e+05      6.4261e+05


 TIME FOR THE TIME STEP              497:        0.71117E+02

===============================================================


 INSTANT    0.498000000E+03   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         0.195191246E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10097E+03 0.21888E+02
   Friction velocity        uet   :  0.46089E-01 0.57014E+01
   Friction velocity        uk    :  0.47656E-01 0.60955E+01
   Dimensionless distance   yplus :  0.22885E-03 0.30994E+02
   ---------------v  epsilon              0.0022891      7.6498e+06          5766.1          62.955
v  TurbVisc             1.005e-11         0.45313       0.0021006        0.026422
v  total_pressure          -38906       7.955e+05       6.591e+05      6.4268e+05


 TIME FOR THE TIME STEP              495:        0.67405E+02

===============================================================


 INSTANT    0.496000000E+03   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         0.343576348E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.75570E+02 0.20039E+02
   Friction velocity        uet   :  0.44612E-01 0.57284E+01
   Friction velocity        uk    :  0.52196E-01 0.60667E+01
   Dimensionless distance   yplus :  0.23005E-03 0.32948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13732
   Nb of faces within the viscous sub-layer     :      10559
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69406E+01     112   0.18653E+00   0.45894E+03 0.62151E+03 
c  Velocity[X]                                      0.14625E+03 
c  Velocity[Y]                                      0.13944E+03 
c  Velocity[Z]                                      0.17325E+03 
c  Pressure     0.11971E+00     877   0.45030E-02   0.27218E+00 0.14703E+04 
c  k            0.66535E+00      63   0.45866E-02   0.71866E+00 0.86099E+03 
c  epsilon      0.13949E+05      42   0.50549E-02   0.33874E+10 0.22243E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038434                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                 v  k                   1.7831e-06          31.869        0.097491        0.051475
v  epsilon              0.0021838      7.7548e+06          5753.6          63.115
v  TurbVisc            4.9518e-12         0.45316       0.0021002        0.026421
v  total_pressure          -35531      7.9578e+05      6.5897e+05      6.4261e+05


 TIME FOR THE TIME STEP              497:        0.63405E+02

===============================================================


 INSTANT    0.498000000E+03   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         0.195191246E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10097E+03 0.21888E+02
   Friction velocity        uet   :  0.46089E-01 0.57014E+01
   Friction velocity        uk    :  0.47656E-01 0.60955E+01
   Dimensionless distance   yplus :  0.22885E-03 0.30994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13736
   Nb of faces within the viscous sub-layer     :      10566
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69584E+01     11v  Pressure           -5.3375e+05      2.9581e+05      1.5889e+05      1.4251e+05
v  k                   1.7688e-06           35.17        0.097217        0.051497
v  epsilon               0.002081      7.6627e+06          5707.1          63.124
v  TurbVisc            9.9669e-12         0.46688       0.0020992         0.02642
v  total_pressure          -33749      7.9581e+05      6.5889e+05      6.4251e+05


 TIME FOR THE TIME STEP              499:        0.65248E+02

===============================================================


 INSTANT    0.500000000E+03   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.817369830E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12267E+03 0.20213E+02
   Friction velocity        uet   :  0.37455E-01 0.57357E+01
   Friction velocity        uk    :  0.37278E-01 0.60896E+01
   Dimensionless distance   yplus :  0.22716E-03 0.31304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13742
   Nb of faces within the viscous sub-layer     :      10548
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.69552E+01     114   0.18827E+00   0.49110E+03 0.64463E+03 
c  Velocity[X]                                      0.14855E+03 
c  Velocity[Y]                                      0.14411E+03 
c  Velocity[Z]                                      0.19844E+03 
c  Pressure     0.12025E+00     693   0.45135E-02   0.27140E+00 0.49112E+03 
c  k            0.68649E+00      69   0.62483E-02   0.29182E+01 0.12163E+04 
c  epsilon      0.13829E+05      47   0.41880E-02   0.84472E+09 0.13769E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0038952                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -14.62          36.901          2.2376         0.25819
v  Velocity[Y]            -34.179          29.127         0.88019         0.58611
v  Velocity[Z]              -52.1          45.248         -1.0779      -0.0017592
v  ǁVelocityǁ          0.00040915          65.635          6.6079          5.4203
v  Pressure           -5.3709e+05      2.9582e+05      1.5862e+05      1.4226e+05
v  k                   1.7665e-06          37.768        0.097263        0.051563
v  epsilon              0.0020246      7.6905e+06          5708.9          63.487
v  TurbVisc            9.9572e-12         0.50332       0.0020986         0.02642
v  total_pressure          -37088      7.9582e+05      6.5862e+05      6.4226e+05


 TIME FOR THE TIME STEP              500:        0.78219E+02

===============================================================


 INSTANT    0.501000000E+03   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         0.421732858E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245843E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surfav  Pressure           -5.3375e+05      2.9581e+05      1.5889e+05      1.4251e+05
v  k                   1.7688e-06           35.17        0.097217        0.051497
v  epsilon               0.002081      7.6627e+06          5707.1          63.124
v  TurbVisc            9.9669e-12         0.46688       0.0020992         0.02642
v  total_pressure          -33749      7.9581e+05      6.5889e+05      6.4251e+05


 TIME FOR THE TIME STEP              499:        0.72336E+02

===============================================================


 INSTANT    0.500000000E+03   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.221245855E+01
Smooth wall               5       41000         0.817369830E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.221245846E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12267E+03 0.20213E+02
   Friction velocity        uet   :  0.37455E-01 0.57357E+01
   Friction velocity        uk    :  0.37278E-01 0.60896E+01
   Dimensionless distance   yplus :  0.22716E-03 0.31304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13742
   Nb of faces within the viscous sub-layer     :      10548
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
----------------------------v  ǁVelocityǁ          0.00040897          118.51          6.8423          6.3746
v  Pressure           -4.3094e+05      5.4282e+05      3.2229e+05      2.9227e+05
v  k                   1.7698e-06          36.086         0.09765         0.05822
v  epsilon              0.0020075      7.6308e+06          5705.7          65.038
v  TurbVisc            9.9273e-12         0.52611       0.0020988        0.026421
v  total_pressure           69060      1.0428e+06      8.2229e+05      7.9227e+05


 TIME FOR THE TIME STEP              501:        0.81558E+02

===============================================================


 INSTANT    0.502000000E+03   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         0.730076237E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969739E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11447E+03 0.30413E+02
   Friction velocity        uet   :  0.13547E-01 0.86699E+01
   Friction velocity        uk    :  0.32699E-01 0.61838E+01
   Dimensionless distance   yplus :  0.22804E-03 0.28890E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14694
   Nb of faces within the viscous sub-layer     :      10275
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96665E+01     146   0.17354E+00   0.47870E+04 0.16675E+04 
c  Velocity[X]                                      0.11289E+04 
c  Velocity[Y]                                      0.14012E+04 
c  Velocity[Z]                                      0.22569E+04 
c  Pressure     0.23230E+00    1163   0.71761E-01   0.48754E+00 0.16833E+06 
c  k            0.80430E+00     105   0.91583E-02   0.13312E+02 0.30117E+04 
c  epsilon      0.15187E+05      68   0.19788E-01   0.40309E+11 0.88242E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.017655                             4
a  epsilon         -260.76                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.965          55.141          2.4039         0.31583
v  Velocity[Y]            -56.609           61.27          1.0718         0.71857
v  Velocity[Z]            -95.776          85.733         -1.1088      -0.0043733
v  ǁVelocityǁ          0.00040823          105.15          6.9632          6.3478
v  Pressure           -5.3974e+05      3.9579e+05      2.4256e+05      2.1002e+05
v  k                   1.7834e-06          32.982        0.099995        0.064495
v  epsilon              0.0019748      7.9174e+06          5839.4          70.765
v  TurbVisc            9.9352e-12         0.49124       0.0022204        0.029513
v  total_pressure          -39738      8.9579e+05      7.4256e+05      7.1002e+05


 TIME FOR THE TIME STEP              502:        0.91197E+02

===============================================================


 INSTANT    0.503000000E+03   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         0.883751507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlv  ǁVelocityǁ          0.00040897          118.51          6.8423          6.3746
v  Pressure           -4.3094e+05      5.4282e+05      3.2229e+05      2.9227e+05
v  k                   1.7698e-06          36.086         0.09765         0.05822
v  epsilon              0.0020075      7.6308e+06          5705.7          65.038
v  TurbVisc            9.9273e-12         0.52611       0.0020988        0.026421
v  total_pressure           69060      1.0428e+06      8.2229e+05      7.9227e+05


 TIME FOR THE TIME STEP              501:        0.10547E+03

===============================================================


 INSTANT    0.502000000E+03   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         0.730076237E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969739E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11447E+03 0.30413E+02
   Friction velocity        uet   :  0.13547E-01 0.86699E+01
   Friction velocity        uk    :  0.32699E-01 0.61838E+01
   Dimensionless distance   yplus :  0.22804E-03 0.28890E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14694
   Nb of faces within the viscous sub-layer     :      10275
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_itev  Velocity[Y]            -46.251          48.043          1.0765         0.71825
v  Velocity[Z]            -78.352          90.811         -1.1269      -0.0013004
v  ǁVelocityǁ          0.00041673          95.479          7.0414          6.3816
v  Pressure           -5.7307e+05      3.8965e+05      2.3046e+05      2.0169e+05
v  k                   1.8023e-06           37.43         0.10079        0.067847
v  epsilon              0.0019664      7.9873e+06          5915.5          71.554
v  TurbVisc            9.9409e-12          0.4385       0.0022678        0.031111
v  total_pressure          -73065      8.8965e+05      7.3046e+05      7.0169e+05


 TIME FOR THE TIME STEP              503:        0.91632E+02

===============================================================


 INSTANT    0.504000000E+03   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.504345410E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19347E+03 0.24373E+02
   Friction velocity        uet   :  0.31399E-01 0.70966E+01
   Friction velocity        uk    :  0.33189E-01 0.64034E+01
   Dimensionless distance   yplus :  0.23072E-03 0.35703E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14760
   Nb of faces within the viscous sub-layer     :      10105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93856E+01     131   0.17290E+00   0.22929E+04 0.12796E+04 
c  Velocity[X]                                      0.57914E+03 
c  Velocity[Y]                                      0.70050E+03 
c  Velocity[Z]                                      0.10133E+04 
c  Pressure     0.21760E+00     894   0.17766E-01   0.43944E+00 0.90293E+04 
c  k            0.77938E+00      97   0.13482E-01   0.14395E+02 0.30553E+04 
c  epsilon      0.16069E+05      59   0.14345E-01   0.96431E+11 0.13625E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0034451                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.051          58.412           2.462         0.31525
v  Velocity[Y]            -71.516          42.384          1.0773         0.71798
v  Velocity[Z]            -85.051          109.07         -1.1429     -0.00065157
v  ǁVelocityǁ          0.00042483          113.33          7.1105          6.4022
v  Pressure           -5.8631e+05      3.9418e+05      2.2955e+05      2.0197e+05
v  k                   1.8254e-06          49.053         0.10165        0.070121
v  epsilon              0.0019384      1.0754e+07          6050.6           71.76
v  TurbVisc            1.0033e-11         0.41812       0.0023083        0.032408
v  total_pressure          -86313      8.9418e+05      7.2955e+05      7.0197e+05


 TIME FOR THE TIME STEP              504:        0.76722E+02

===============================================================


 INSTANT    0.505000000E+03   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.103297076E-16
Rough wall                6           0         0.000000000E+00
Symmetry          v  Velocity[Y]            -46.251          48.043          1.0765         0.71825
v  Velocity[Z]            -78.352          90.811         -1.1269      -0.0013004
v  ǁVelocityǁ          0.00041673          95.479          7.0414          6.3816
v  Pressure           -5.7307e+05      3.8965e+05      2.3046e+05      2.0169e+05
v  k                   1.8023e-06           37.43         0.10079        0.067847
v  epsilon              0.0019664      7.9873e+06          5915.5          71.554
v  TurbVisc            9.9409e-12          0.4385       0.0022678        0.031111
v  total_pressure          -73065      8.8965e+05      7.3046e+05      7.0169e+05


 TIME FOR THE TIME STEP              503:        0.99052E+02

===============================================================


 INSTANT    0.504000000E+03   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.504345410E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19347E+03 0.24373E+02
   Friction velocity        uet   :  0.31399E-01 0.70966E+01
   Friction velocity        uk    :  0.33189E-01 0.64034E+01
   Dimensionless distance   yplus :  0.23072E-03 0.35703E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14760
   Nb of faces within the viscous sub-layer     :      10105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   *v  Velocity[X]             -15.09          60.167          2.4871         0.31456
v  Velocity[Y]            -66.127          41.606          1.0758         0.71779
v  Velocity[Z]            -114.46          68.115         -1.1591      -0.0018119
v  ǁVelocityǁ          0.00042244          132.95          7.1758           6.417
v  Pressure           -5.9291e+05      3.9776e+05      2.3035e+05      2.0311e+05
v  k                   1.8492e-06          32.542         0.10214        0.071787
v  epsilon              0.0018944      8.4184e+06          6097.1          71.824
v  TurbVisc            1.0089e-11         0.41835        0.002343        0.033446
v  total_pressure          -92907      8.9776e+05      7.3035e+05      7.0311e+05


 TIME FOR THE TIME STEP              505:        0.82025E+02

===============================================================


 INSTANT    0.506000000E+03   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.101841255E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969710E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Y]            -46.251          48.043          1.0765         0.71825
v  Velocity[Z]            -78.352          90.811         -1.1269      -0.0013004
v  ǁVelocityǁ          0.00041673          95.479          7.0414          6.3816
v  Pressure           -5.7307e+05      3.8965e+05      2.3046e+05      2.0169e+05
v  k                   1.8023e-06           37.43         0.10079        0.067847
v  epsilon              0.0019664      7.9873e+06          5915.5          71.554
v  TurbVisc            9.9409e-12          0.4385       0.0022678        0.031111
v  total_pressure          -73065      8.8965e+05      7.3046e+05      7.0169e+05


 TIME FOR THE TIME STEP              503:        0.93051E+02

===============================================================


 INSTANT    0.504000000E+03   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.504345410E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19347E+03 0.24373E+02
   Friction velocity        uet   :  0.31399E-01 0.70966E+01
   Friction velocity        uk    :  0.33189E-01 0.64034E+01
   Dimensionless distance   yplus :  0.23072E-03 0.35703E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14760
   Nb of faces within the viscous sub-layer     :      10105
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.93856E+01     131   0.17290E+00   0.22929E+04 0.12796E+04 
c  Velocity[X]                                      0.57914E+03 
c  Velocity[Y]                                      0.70050E+03 
c  Velocity[Z]                                      0.10133E+04 
c  Pressure     0.21760E+00     894   0.17766E-01   0.43944E+00 0.90293E+04 
c  k            0.77938E+00      97   0.13482E-01   0.14395E+02 0.30553E+04 
c  epsilon      0.16069E+05      59   0.14345E-01   0.96431E+11 0.13625E+06 
------------------------------------------v  Velocity[X]             -15.09          60.167          2.4871         0.31456
v  Velocity[Y]            -66.127          41.606          1.0758         0.71779
v  Velocity[Z]            -114.46          68.115         -1.1591      -0.0018119
v  ǁVelocityǁ          0.00042244          132.95          7.1758           6.417
v  Pressure           -5.9291e+05      3.9776e+05      2.3035e+05      2.0311e+05
v  k                   1.8492e-06          32.542         0.10214        0.071787
v  epsilon              0.0018944      8.4184e+06          6097.1          71.824
v  TurbVisc            1.0089e-11         0.41835        0.002343        0.033446
v  total_pressure          -92907      8.9776e+05      7.3035e+05      7.0311e+05


 TIME FOR THE TIME STEP              505:        0.78841E+02

===============================================================


 INSTANT    0.506000000E+03   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.101841255E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969710E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12595E+03 0.27221E+02
   Friction velocity        uet   :  0.33988E-01 0.91881E+01
   Friction velocity        uk    :  0.32426E-01 0.66180E+01
   Dimensionless distance   yplus :  0.23297E-03 0.33272E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14690
   Nb of faces within the viscous sub-layer     :      10034
   Total number of wall faces                   :      4
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.407          55.265          2.5362         0.31204
v  Velocity[Y]            -47.926          39.857          1.0802         0.71836
v  Velocity[Z]            -77.455          60.502         -1.1897      -0.0022535
v  ǁVelocityǁ          0.00042091          97.263           7.312          6.4443
v  Pressure           -6.0921e+05      4.0278e+05      2.3101e+05      2.0433e+05
v  k                   1.9023e-06          21.731         0.10374        0.074046
v  epsilon              0.0017552      1.1534e+07            6307          72.112
v  TurbVisc            1.0236e-11         0.41838       0.0024116        0.035005
v  total_pressure     -1.0921e+05      9.0278e+05      7.3101e+05      7.0433e+05


 TIME FOR THE TIME STEP              507:        0.75186E+02

===============================================================


 INSTANT    0.508000000E+03   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         0.532756152E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           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]             -15.09          60.167          2.4871         0.31456
v  Velocity[Y]            -66.127          41.606          1.0758         0.71779
v  Velocity[Z]            -114.46          68.115         -1.1591      -0.0018119
v  ǁVelocityǁ          0.00042244          132.95          7.1758           6.417
v  Pressure           -5.9291e+05      3.9776e+05      2.3035e+05      2.0311e+05
v  k                   1.8492e-06          32.542         0.10214        0.071787
v  epsilon              0.0018944      8.4184e+06          6097.1          71.824
v  TurbVisc            1.0089e-11         0.41835        0.002343        0.033446
v  total_pressure          -92907      8.9776e+05      7.3035e+05      7.0311e+05


 TIME FOR THE TIME STEP              505:        0.80809E+02

===============================================================


 INSTANT    0.506000000E+03   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.101841255E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969710E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12595E+03 0.27221E+02
   Friction velocity        uet   :  0.33988E-01 0.91881E+01
   Friction velocity        uk    :  0.32426E-01 0.66180E+01
   Dimensionless distance   yplus :  0.23297E-03 0.33272E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14690
   Nb of faces within the viscous sub-layer     :      10034
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.96351E+01     127   0.17928E+00   0.17438E+04 0.11383E+04 
c  Velocity[X]                                      0.45312E+03 
c  Velocity[Y]                                      0.51242E+03 
c  Velocity[Z]                                      0.77829E+03 
c  Pressure     0.22209E+00     821   0.12942E-01   0.43385E+00 0.14550E+04 
c  k            0.64841E+00      92   0.96070E-02   0.51964E+01 0.21531E+04 
c  epsilon      0.15431E+05      53   0.12365E
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.407          55.265          2.5362         0.31204
v  Velocity[Y]            -47.926          39.857          1.0802         0.71836
v  Velocity[Z]            -77.455          60.502         -1.1897      -0.0022535
v  ǁVelocityǁ          0.00042091          97.263           7.312          6.4443
v  Pressure           -6.0921e+05      4.0278e+05      2.3101e+05      2.0433e+05
v  k                   1.9023e-06          21.731         0.10374        0.074046
v  epsilon              0.0017552      1.1534e+07            6307          72.112
v  TurbVisc            1.0236e-11         0.41838       0.0024116        0.035005
v  total_pressure     -1.0921e+05      9.0278e+05      7.3101e+05      7.0433e+05


 TIME FOR THE TIME STEP              507:        0.82074E+02

===============================================================


 INSTANT    0.508000000E+03   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         0.532756152E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15237E+03 0.26991E+02
   Friction velocity        uet   :  0.27087E-01 0.67868E+01
   Friction velocity        uk    :  0.26998E-01 0.67610E+01
   Dimensionless distance   yplus :  0.23182E-03 0.27105E+02
   ------------------------------------------------------
  a  k             -0.004071                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.643          46.388          2.5804         0.31169
v  Velocity[Y]            -39.216          39.481          1.0917         0.71845
v  Velocity[Z]            -67.871          59.145          -1.215      -0.0019594
v  ǁVelocityǁ           0.0004325          81.723          7.4447          6.4667
v  Pressure           -6.2876e+05      4.1106e+05      2.3055e+05      2.0451e+05
v  k                   1.9753e-06          20.742         0.10558        0.075388
v  epsilon              0.0015961      8.8833e+06          6497.9          72.421
v  TurbVisc            1.0515e-11         0.41838       0.0024728        0.036038
v  total_pressure     -1.2876e+05      9.1106e+05      7.3055e+05      7.0451e+05


 TIME FOR THE TIME STEP              509:        0.78579E+02

===============================================================


 INSTANT    0.510000000E+03   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.632842757E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface        
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.407          55.265          2.5362         0.31204
v  Velocity[Y]            -47.926          39.857          1.0802         0.71836
v  Velocity[Z]            -77.455          60.502         -1.1897      -0.0022535
v  ǁVelocityǁ          0.00042091          97.263           7.312          6.4443
v  Pressure           -6.0921e+05      4.0278e+05      2.3101e+05      2.0433e+05
v  k                   1.9023e-06          21.731         0.10374        0.074046
v  epsilon              0.0017552      1.1534e+07            6307          72.112
v  TurbVisc            1.0236e-11         0.41838       0.0024116        0.035005
v  total_pressure     -1.0921e+05      9.0278e+05      7.3101e+05      7.0433e+05


 TIME FOR THE TIME STEP              507:        0.80397E+02

===============================================================


 INSTANT    0.508000000E+03   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         0.532756152E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15237E+03 0.26991E+02
   Friction velocity        uet   :  0.27087E-01 0.67868E+01
   Friction velocity        uk    :  0.26998E-01 0.67610E+01
   Dimensionless distance   yplus :  0.23182E-03 0.27105E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14887
   Nb of faces within the viscous sub-layer     :       9948
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.97991E+01     124   0.17728E+00   0.13782E+04 0.10096E+04 
c  Velocity[X]                                      0.37593E+03 
c  Velocity[Y]                                      0.41612E+03 
c  Velocity[Z]                                      0.58613E+03 
c  Pressure     0.21460Ea  k             -0.004071                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -15.643          46.388          2.5804         0.31169
v  Velocity[Y]            -39.216          39.481          1.0917         0.71845
v  Velocity[Z]            -67.871          59.145          -1.215      -0.0019594
v  ǁVelocityǁ           0.0004325          81.723          7.4447          6.4667
v  Pressure           -6.2876e+05      4.1106e+05      2.3055e+05      2.0451e+05
v  k                   1.9753e-06          20.742         0.10558        0.075388
v  epsilon              0.0015961      8.8833e+06          6497.9          72.421
v  TurbVisc            1.0515e-11         0.41838       0.0024728        0.036038
v  total_pressure     -1.2876e+05      9.1106e+05      7.3055e+05      7.0451e+05


 TIME FOR THE TIME STEP              509:        0.79496E+02

===============================================================


 INSTANT    0.510000000E+03   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.632842757E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78305E+02 0.22483E+02
   Friction velocity        uet   :  0.33804E-01 0.58661E+01
   Friction velocity        uk    :  0.45063E-01 0.68277E+01
   D-  -------  --------------  --------------  ------------  ------------
a  k             -0.016629                             4
a  epsilon         -1731.3                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.188          46.539          2.6209         0.31074
v  Velocity[Y]            -37.281          37.794          1.0966         0.71668
v  Velocity[Z]            -75.374          62.306         -1.2255      -0.0016636
v  ǁVelocityǁ          0.00046684          86.727           7.554          6.4834
v  Pressure           -6.5454e+05       4.165e+05      2.2924e+05        2.04e+05
v  k                   1.8437e-06          26.559         0.10866        0.076309
v  epsilon              0.0014707      9.6152e+06          6981.4          73.854
v  TurbVisc            1.0994e-11         0.41838       0.0025288        0.036688
v  total_pressure     -1.5454e+05       9.165e+05      7.2924e+05        7.04e+05


 TIME FOR THE TIME STEP              511:        0.74213E+02

===============================================================


 INSTANT    0.512000000E+03   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.729801690E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98530E+02 0.20980E+02
   Friction velocity        uet   :  0.47161E-01 0.64689E+01
   Friction velocity        uk    :  0.60651E-01 0.68916E+01
   Dimensionless distance   yplus :  0.24165E-03 0.30017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15319
   Nb of faces within the viscous sub-layer     :       9721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10005E+02     122   0.18370E+00   0.12374E+04 0.93170E+03 
c  Velocity[X]                                      0.35034E+03 
c  Velocity[Y]                                      0.39113E+03 
c  Velocity[Z]                                      0.49589E+03 
c  Pressure     0.22017E+00     692   0.10740E-01   0.42906E+00 0.79419E+03 
c  k            0.63884E+00      84   0.68286E-02   0.26747E+01 0.22029E+04 
c  epsilon      0.17771E+05      49   0.80366E-02   0.38035E+11 0.19972E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.6974e-05                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.346          44.947          2.6403         0.30989
v  Velocity[Y]            -34.997          37.922           1.096         0.71615
v  Velocity[Z]            -65.039          65.211         -1.2267      -0.0015177
v  ǁVelocityǁ           0.0005015          77.426          7.5999          6.4906
v  Pressure           -6.6756e+05      4.1931e+05        2.29e+05      2.0397e+05
v  k                   1.7704e-06          29.796         0.11037        0.076663
v  epsilon              0.0014337      9.8798e+06          7249.3          74.723
v  TurbVisc            1.1781e-11         0.41838       0.0025563         0.03691
v  total_pressure     -1.6756e+05      9.1931e+05        7.29e+05      7.0397e+05


 TIME FOR THE TIME STEP              512:        0.69877E+02

===============================================================


 INSTANT    0.513000000E+03   TIME STEP NUMBER             513
 ==============================================-  -------  --------------  --------------  ------------  ------------
a  k             -0.016629                             4
a  epsilon         -1731.3                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.188          46.539          2.6209         0.31074
v  Velocity[Y]            -37.281          37.794          1.0966         0.71668
v  Velocity[Z]            -75.374          62.306         -1.2255      -0.0016636
v  ǁVelocityǁ          0.00046684          86.727           7.554          6.4834
v  Pressure           -6.5454e+05       4.165e+05      2.2924e+05        2.04e+05
v  k                   1.8437e-06          26.559         0.10866        0.076309
v  epsilon              0.0014707      9.6152e+06          6981.4          73.854
v  TurbVisc            1.0994e-11         0.41838       0.0025288        0.036688
v  total_pressure     -1.5454e+05       9.165e+05      7.2924e+05        7.04e+05


 TIME FOR THE TIME STEP              511:        0.74986E+02

===============================================================


 INSTANT    0.512000000E+03   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.729801690E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98530
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.024961                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.404          47.151          2.6588         0.30929
v  Velocity[Y]            -36.252          37.624          1.0942         0.71563
v  Velocity[Z]            -75.649          64.294         -1.2269      -0.0017839
v  ǁVelocityǁ          0.00053212           87.06          7.6396          6.4989
v  Pressure           -6.8013e+05      4.2073e+05      2.2843e+05      2.0368e+05
v  k                   1.7175e-06           33.16         0.11214        0.076988
v  epsilon              0.0014194      9.7356e+06          7546.8          75.858
v  TurbVisc            1.1875e-11         0.41838        0.002583        0.037081
v  total_pressure     -1.8013e+05      9.2073e+05      7.2843e+05      7.0368e+05


 TIME FOR THE TIME STEP              513:        0.81679E+02

===============================================================


 INSTANT    0.514000000E+03   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         0.946446332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet-  -------  --------------  --------------  ------------  ------------
a  k             -0.016629                             4
a  epsilon         -1731.3                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.188          46.539          2.6209         0.31074
v  Velocity[Y]            -37.281          37.794          1.0966         0.71668
v  Velocity[Z]            -75.374          62.306         -1.2255      -0.0016636
v  ǁVelocityǁ          0.00046684          86.727           7.554          6.4834
v  Pressure           -6.5454e+05       4.165e+05      2.2924e+05        2.04e+05
v  k                   1.8437e-06          26.559         0.10866        0.076309
v  epsilon              0.0014707      9.6152e+06          6981.4          73.854
v  TurbVisc            1.0994e-11         0.41838       0.0025288        0.036688
v  total_pressure     -1.5454e+05       9.165e+05      7.2924e+05        7.04e+05


 TIME FOR THE TIME STEP              511:        0.65074E+02

===============================================================


 INSTANT    0.512000000E+03   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.729801690E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98530E+02 0.20980E+02
   Friction velocity        uet   :  0.47161E-01 0.64689E+01
   Friction velocity        uk    :  0.60651E-01 0.68916E+01
   Dimensionless distance   yplus :  0.24165E-03 0.30017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15319
   Nb of faces within the viscous sub-layer     :       9721
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10005E+02     122 
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.024961                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.404          47.151          2.6588         0.30929
v  Velocity[Y]            -36.252          37.624          1.0942         0.71563
v  Velocity[Z]            -75.649          64.294         -1.2269      -0.0017839
v  ǁVelocityǁ          0.00053212           87.06          7.6396          6.4989
v  Pressure           -6.8013e+05      4.2073e+05      2.2843e+05      2.0368e+05
v  k                   1.7175e-06           33.16         0.11214        0.076988
v  epsilon              0.0014194      9.7356e+06          7546.8          75.858
v  TurbVisc            1.1875e-11         0.41838        0.002583        0.037081
v  total_pressure     -1.8013e+05      9.2073e+05      7.2843e+05      7.0368e+05


 TIME FOR THE TIME STEP              513:        0.81093E+02

===============================================================


 INSTANT    0.514000000E+03   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         0.946446332E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
--------------------------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015436                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.767          49.815          2.6908         0.30827
v  Velocity[Y]            -33.137          37.209          1.0847          0.7149
v  Velocity[Z]             -76.53          63.687         -1.2286      -0.0027544
v  ǁVelocityǁ          0.00060778          84.645          7.7079          6.5165
v  Pressure           -7.0115e+05      4.2223e+05      2.2744e+05      2.0301e+05
v  k                   1.7009e-06          39.799         0.11569        0.077548
v  epsilon              0.0014793       9.177e+06          8193.1          78.149
v  TurbVisc            1.3916e-11         0.46232         0.00263        0.037311
v  total_pressure     -2.0115e+05      9.2223e+05      7.2744e+05      7.0301e+05


 TIME FOR THE TIME STEP              515:        0.70451E+02

===============================================================


 INSTANT    0.516000000E+03   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.370192095E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19044E+03 0.12810E+02
   Friction velocity        uet   :  0.34858E-01 0.66416E+01
   Friction velocity        uk    :  0.60840E-01 0.68672E+01
   Dimensionless distance   yplus :  0.27583E-03 0.35019E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15644
   Nb of faces within the viscous sub-layer     :       9454
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10109E+02     120   0.18271E+00   0.11552E+04 0.87449E+03 
c  Velocity[X]                                      0.34026E+03 
c  Velocity[Y]                                      0.30326E+03 
c  Velocity[Z]                                      0.51167E+03 
c  Pressure     0.20329E+00    1098   0.80841E-02   0.38947E+00 0.20359E+04 
c  k            0.84459E+00      78   0.75609E-02   0.51741E+01 0.25500E+04 
c  epsilon      0.19824E+05      48   0.86710E-02   0.10223E+12 0.40418E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.012509                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.788          46.748          2.7035         0.30912
v  Velocity[Y]            -33.629          36.931          1.0793         0.71532
v  Velocity[Z]            -66.226          57.613         -1.2305      -0.0026216
v  ǁVelocityǁ          0.00064833          79.679          7.7361          6.5244
v  Pressure           -7.0935e+05      4.2273e+05      2.2669e+05      2.0251e+05
v  k                   1.7624e-06          45.323         0.11723        0.077829
v  epsilon               0.001572      9.1339e+06          8494.7          79.375
v  TurbVisc            1.5132e-11         0.49605       0.0026484        0.037388
v  total_pressure     -2.0935e+05      9.2273e+05      7.2669e+05      7.0251e+05


 TIME FOR THE TIME STEP              516:        0.87187E-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015436                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.767          49.815          2.6908         0.30827
v  Velocity[Y]            -33.137          37.209          1.0847          0.7149
v  Velocity[Z]             -76.53          63.687         -1.2286      -0.0027544
v  ǁVelocityǁ          0.00060778          84.645          7.7079          6.5165
v  Pressure           -7.0115e+05      4.2223e+05      2.2744e+05      2.0301e+05
v  k                   1.7009e-06          39.799         0.11569        0.077548
v  epsilon              0.0014793       9.177e+06          8193.1          78.149
v  TurbVisc            1.3916e-11         0.46232         0.00263        0.037311
v  total_pressure     -2.0115e+05      9.2223e+05      7.2744e+05      7.0301e+05


 TIME FOR THE TIME STEP              515:        0.74100E+02

===============================================================


 INSTANT    0.516000000E+03   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.370192095E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
     c  epsilon      0.20517E+05      48   0.11136E-01   0.85942E+11 0.24175E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.013975                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.045          51.676          2.7136         0.30947
v  Velocity[Y]              -33.6           37.48          1.0735         0.71533
v  Velocity[Z]            -96.012          68.249         -1.2343      -0.0028755
v  ǁVelocityǁ          0.00068128          109.28          7.7613          6.5329
v  Pressure           -7.1457e+05      4.2289e+05      2.2637e+05      2.0237e+05
v  k                   1.8928e-06           49.94         0.11857         0.07812
v  epsilon              0.0017024       9.157e+06            8751           80.62
v  TurbVisc            1.7549e-11         0.55202       0.0026645         0.03745
v  total_pressure     -2.1457e+05      9.2289e+05      7.2637e+05      7.0237e+05


 TIME FOR THE TIME STEP              517:        0.71783E+02

===============================================================


 INSTANT    0.518000000E+03   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015436                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -16.767          49.815          2.6908         0.30827
v  Velocity[Y]            -33.137          37.209          1.0847          0.7149
v  Velocity[Z]             -76.53          63.687         -1.2286      -0.0027544
v  ǁVelocityǁ          0.00060778          84.645          7.7079          6.5165
v  Pressure           -7.0115e+05      4.2223e+05      2.2744e+05      2.0301e+05
v  k                   1.7009e-06          39.799         0.11569        0.077548
v  epsilon              0.0014793       9.177e+06          8193.1          78.149
v  TurbVisc            1.3916e-11         0.46232         0.00263        0.037311
v  total_pressure     -2.0115e+05      9.2223e+05      7.2744e+05      7.0301e+05


 TIME FOR THE TIME STEP              515:        0.77277E+02

===============================================================


 INSTANT    0.516000000E+03   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.370192095E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19044E+03 0.12810E+02
   Friction velocity        uet   :  0.34858E-01 0.66416E+01
   Friction velocity        uk    :  0.60840E-01 0.68672E+01
   Dimensionless distance   yplus :  0.27583E-03 0.35019E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15644
   Nb of faces within the viscous sub-layer     :       9454
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_c  epsilon      0.20517E+05      48   0.11136E-01   0.85942E+11 0.24175E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.013975                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.045          51.676          2.7136         0.30947
v  Velocity[Y]              -33.6           37.48          1.0735         0.71533
v  Velocity[Z]            -96.012          68.249         -1.2343      -0.0028755
v  ǁVelocityǁ          0.00068128          109.28          7.7613          6.5329
v  Pressure           -7.1457e+05      4.2289e+05      2.2637e+05      2.0237e+05
v  k                   1.8928e-06           49.94         0.11857         0.07812
v  epsilon              0.0017024       9.157e+06            8751           80.62
v  TurbVisc            1.7549e-11         0.55202       0.0026645         0.03745
v  total_pressure     -2.1457e+05      9.2289e+05      7.2637e+05      7.0237e+05


 TIME FOR THE TIME STEP              517:        0.75335E+02

===============================================================


 INSTANT    0.518000000E+03   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         0.401608746E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
 c  Pressure     0.19955E+00     647   0.67189E-02   0.37917E+00 0.13204E+04 
c  k            0.10907E+01      74   0.75926E-02   0.79320E+01 0.20203E+04 
c  epsilon      0.22245E+05      50   0.81314E-02   0.76641E+11 0.33353E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.012857                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.455          47.913          2.7304         0.30948
v  Velocity[Y]            -34.836           37.59          1.0571         0.71539
v  Velocity[Z]            -60.714          59.465         -1.2401        -0.00278
v  ǁVelocityǁ          0.00076397          74.295          7.7993          6.5449
v  Pressure           -7.2686e+05      4.2266e+05      2.2539e+05      2.0186e+05
v  k                   2.2351e-06          55.623         0.12096        0.078833
v  epsilon              0.0021585      9.2347e+06          9218.9          83.853
v  TurbVisc            2.0648e-11         0.63747       0.0026915        0.037541
v  total_pressure     -2.2686e+05      9.2266e+05      7.2539e+05      7.0186e+05


 TIME FOR THE TIME STEP              519:        0.76222E+02

===============================================================


 INSTANT    0.520000000E+03   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------c  epsilon      0.20517E+05      48   0.11136E-01   0.85942E+11 0.24175E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.013975                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.045          51.676          2.7136         0.30947
v  Velocity[Y]              -33.6           37.48          1.0735         0.71533
v  Velocity[Z]            -96.012          68.249         -1.2343      -0.0028755
v  ǁVelocityǁ          0.00068128          109.28          7.7613          6.5329
v  Pressure           -7.1457e+05      4.2289e+05      2.2637e+05      2.0237e+05
v  k                   1.8928e-06           49.94         0.11857         0.07812
v  epsilon              0.0017024       9.157e+06            8751           80.62
v  TurbVisc            1.7549e-11         0.55202       0.0026645         0.03745
v  total_pressure     -2.1457e+05      9.2289e+05      7.2637e+05      7.0237e+05


 TIME FOR THE TIME STEP              517:        0.76582E+02

===============================================================


 INSTANT    0.518000000E+03   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         0.401608746E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969745E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12271E+03 0.11901E+02
   Friction velocity        uet   :  0.33619E-01 0.80244E+01
   Friction velocity        uk    :  0.51768E-01 0.68659E+01
   Dimensionless distance   yplus :  0.29050E-03 0.32637E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15754
   Nb of faces within the viscous sub-layer     :       9359
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-c  Pressure     0.19955E+00     647   0.67189E-02   0.37917E+00 0.13204E+04 
c  k            0.10907E+01      74   0.75926E-02   0.79320E+01 0.20203E+04 
c  epsilon      0.22245E+05      50   0.81314E-02   0.76641E+11 0.33353E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.012857                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.455          47.913          2.7304         0.30948
v  Velocity[Y]            -34.836           37.59          1.0571         0.71539
v  Velocity[Z]            -60.714          59.465         -1.2401        -0.00278
v  ǁVelocityǁ          0.00076397          74.295          7.7993          6.5449
v  Pressure           -7.2686e+05      4.2266e+05      2.2539e+05      2.0186e+05
v  k                   2.2351e-06          55.623         0.12096        0.078833
v  epsilon              0.0021585      9.2347e+06          9218.9          83.853
v  TurbVisc            2.0648e-11         0.63747       0.0026915        0.037541
v  total_pressure     -2.2686e+05      9.2266e+05      7.2539e+05      7.0186e+05


 TIME FOR THE TIME STEP              519:        0.67244E+02

===============================================================


 INSTANT    0.520000000E+03   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        -0.120388823E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00c  Velocity[Z]                                      0.35207E+03 
c  Pressure     0.18288E+00    1005   0.67675E-02   0.34417E+00 0.65781E+03 
c  k            0.11476E+01      74   0.98993E-02   0.17005E+02 0.23341E+04 
c  epsilon      0.23114E+05      51   0.74030E-02   0.37227E+11 0.82388E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014228                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -17.55          51.433          2.7434         0.30955
v  Velocity[Y]            -34.722          38.422          1.0376         0.71394
v  Velocity[Z]            -81.325          66.497         -1.2443      -0.0027032
v  ǁVelocityǁ          0.00083546           96.34          7.8276          6.5555
v  Pressure           -7.3067e+05      4.2337e+05       2.256e+05      2.0226e+05
v  k                   2.3476e-06            48.6          0.1226        0.079525
v  epsilon               0.002764      9.2277e+06          9523.3          86.448
v  TurbVisc            2.3112e-11         0.59561        0.002709        0.037606
v  total_pressure     -2.3067e+05      9.2337e+05       7.256e+05      7.0226e+05


 TIME FOR THE TIME STEP              521:        0.70184E+02

===============================================================


 INSTANT    0.522000000E+03   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-------------------------------------------c  Pressure     0.19955E+00     647   0.67189E-02   0.37917E+00 0.13204E+04 
c  k            0.10907E+01      74   0.75926E-02   0.79320E+01 0.20203E+04 
c  epsilon      0.22245E+05      50   0.81314E-02   0.76641E+11 0.33353E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.012857                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.455          47.913          2.7304         0.30948
v  Velocity[Y]            -34.836           37.59          1.0571         0.71539
v  Velocity[Z]            -60.714          59.465         -1.2401        -0.00278
v  ǁVelocityǁ          0.00076397          74.295          7.7993          6.5449
v  Pressure           -7.2686e+05      4.2266e+05      2.2539e+05      2.0186e+05
v  k                   2.2351e-06          55.623         0.12096        0.078833
v  epsilon              0.0021585      9.2347e+06          9218.9          83.853
v  TurbVisc            2.0648e-11         0.63747       0.0026915        0.037541
v  total_pressure     -2.2686e+05      9.2266e+05      7.2539e+05      7.0186e+05


 TIME FOR THE TIME STEP              519:        0.75507E+02

===============================================================


 INSTANT    0.520000000E+03   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        -0.120388823E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.97376E+02 0.89276E+01
   Friction velocity        uet   :  0.25108E-01 0.59921E+01
   Friction velocity        uk    :  0.33434E-01 0.68485E+01
   Dimensionless distance   yplus :  0.30674E-03 0.34285E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15818
   Nb of faces within the viscous sub-layer     :       9295
   Total number of wall faces                   :      41000
--------------------c  Velocity[Z]                                      0.35207E+03 
c  Pressure     0.18288E+00    1005   0.67675E-02   0.34417E+00 0.65781E+03 
c  k            0.11476E+01      74   0.98993E-02   0.17005E+02 0.23341E+04 
c  epsilon      0.23114E+05      51   0.74030E-02   0.37227E+11 0.82388E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014228                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -17.55          51.433          2.7434         0.30955
v  Velocity[Y]            -34.722          38.422          1.0376         0.71394
v  Velocity[Z]            -81.325          66.497         -1.2443      -0.0027032
v  ǁVelocityǁ          0.00083546           96.34          7.8276          6.5555
v  Pressure           -7.3067e+05      4.2337e+05       2.256e+05      2.0226e+05
v  k                   2.3476e-06            48.6          0.1226        0.079525
v  epsilon               0.002764      9.2277e+06          9523.3          86.448
v  TurbVisc            2.3112e-11         0.59561        0.002709        0.037606
v  total_pressure     -2.3067e+05      9.2337e+05       7.256e+05      7.0226e+05


 TIME FOR THE TIME STEP              521:        0.83663E+02

===============================================================


 INSTANT    0.522000000E+03   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.747546761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+0c  Velocity[Y]                                      0.26646E+03 
c  Velocity[Z]                                      0.42979E+03 
c  Pressure     0.18368E+00     648   0.69197E-02   0.34752E+00 0.99194E+03 
c  k            0.11244E+01      76   0.11757E-01   0.21028E+02 0.22387E+04 
c  epsilon      0.22818E+05      53   0.89095E-02   0.19881E+11 0.20372E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016943                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.716          57.432          2.7524         0.30873
v  Velocity[Y]            -35.163          37.966           1.018         0.71435
v  Velocity[Z]            -89.798          64.502         -1.2484      -0.0027098
v  ǁVelocityǁ          0.00089144          106.95          7.8493          6.5649
v  Pressure           -7.3734e+05      4.2268e+05      2.2506e+05      2.0207e+05
v  k                   2.5622e-06           54.05         0.12396        0.080222
v  epsilon              0.0034205      9.3899e+06          9685.8          88.772
v  TurbVisc            2.4854e-11         0.64999       0.0027288        0.037655
v  total_pressure     -2.3734e+05      9.2268e+05      7.2506e+05      7.0207e+05


 TIME FOR THE TIME STEP              523:        0.68214E+02

===============================================================


 INSTANT    0.524000000E+03   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ----------c  Velocity[Z]                                      0.35207E+03 
c  Pressure     0.18288E+00    1005   0.67675E-02   0.34417E+00 0.65781E+03 
c  k            0.11476E+01      74   0.98993E-02   0.17005E+02 0.23341E+04 
c  epsilon      0.23114E+05      51   0.74030E-02   0.37227E+11 0.82388E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014228                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -17.55          51.433          2.7434         0.30955
v  Velocity[Y]            -34.722          38.422          1.0376         0.71394
v  Velocity[Z]            -81.325          66.497         -1.2443      -0.0027032
v  ǁVelocityǁ          0.00083546           96.34          7.8276          6.5555
v  Pressure           -7.3067e+05      4.2337e+05       2.256e+05      2.0226e+05
v  k                   2.3476e-06            48.6          0.1226        0.079525
v  epsilon               0.002764      9.2277e+06          9523.3          86.448
v  TurbVisc            2.3112e-11         0.59561        0.002709        0.037606
v  total_pressure     -2.3067e+05      9.2337e+05       7.256e+05      7.0226e+05


 TIME FOR THE TIME STEP              521:        0.82116E+02

===============================================================


 INSTANT    0.522000000E+03   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.747546761E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11552E+03 0.11361E+02
   Friction velocity        uet   :  0.31940E-01 0.67588E+01
   Friction velocity        uk    :  0.45770E-01 0.68569E+01
   Dimensionless distance   yplus :  0.32033E-03 0.34651E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15881
   Nb of faces within the viscous sub-layer     :       9259
   Total number c  Velocity[Y]                                      0.26646E+03 
c  Velocity[Z]                                      0.42979E+03 
c  Pressure     0.18368E+00     648   0.69197E-02   0.34752E+00 0.99194E+03 
c  k            0.11244E+01      76   0.11757E-01   0.21028E+02 0.22387E+04 
c  epsilon      0.22818E+05      53   0.89095E-02   0.19881E+11 0.20372E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016943                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.716          57.432          2.7524         0.30873
v  Velocity[Y]            -35.163          37.966           1.018         0.71435
v  Velocity[Z]            -89.798          64.502         -1.2484      -0.0027098
v  ǁVelocityǁ          0.00089144          106.95          7.8493          6.5649
v  Pressure           -7.3734e+05      4.2268e+05      2.2506e+05      2.0207e+05
v  k                   2.5622e-06           54.05         0.12396        0.080222
v  epsilon              0.0034205      9.3899e+06          9685.8          88.772
v  TurbVisc            2.4854e-11         0.64999       0.0027288        0.037655
v  total_pressure     -2.3734e+05      9.2268e+05      7.2506e+05      7.0207e+05


 TIME FOR THE TIME STEP              523:        0.69770E+02

===============================================================


 INSTANT    0.524000000E+03   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         0.878641357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969710E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+c  Velocity[X]                                      0.32540E+03 
c  Velocity[Y]                                      0.30283E+03 
c  Velocity[Z]                                      0.50352E+03 
c  Pressure     0.18565E+00     643   0.78484E-02   0.35305E+00 0.12015E+04 
c  k            0.11409E+01      77   0.50751E-02   0.51584E+01 0.14333E+04 
c  epsilon      0.22775E+05      55   0.58623E-02   0.25413E+11 0.13119E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016502                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.704          48.332          2.7568         0.30838
v  Velocity[Y]            -44.314          37.074          1.0013         0.71415
v  Velocity[Z]             -90.76           65.78         -1.2575      -0.0026401
v  ǁVelocityǁ          0.00092338           103.1           7.868           6.571
v  Pressure           -7.4093e+05      4.2203e+05      2.2523e+05      2.0242e+05
v  k                   2.8898e-06          52.867         0.12511        0.080775
v  epsilon              0.0042097      9.3062e+06            9786          90.828
v  TurbVisc            2.6081e-11         0.84452       0.0027579        0.037695
v  total_pressure     -2.4093e+05      9.2203e+05      7.2523e+05      7.0242e+05


 TIME FOR THE TIME STEP              525:        0.64715E+02

===============================================================


 INSTANT    0.526000000E+03   TIME STEP NUMBER             526
 =======================================================c  Velocity[Y]                                      0.26646E+03 
c  Velocity[Z]                                      0.42979E+03 
c  Pressure     0.18368E+00     648   0.69197E-02   0.34752E+00 0.99194E+03 
c  k            0.11244E+01      76   0.11757E-01   0.21028E+02 0.22387E+04 
c  epsilon      0.22818E+05      53   0.89095E-02   0.19881E+11 0.20372E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016943                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.716          57.432          2.7524         0.30873
v  Velocity[Y]            -35.163          37.966           1.018         0.71435
v  Velocity[Z]            -89.798          64.502         -1.2484      -0.0027098
v  ǁVelocityǁ          0.00089144          106.95          7.8493          6.5649
v  Pressure           -7.3734e+05      4.2268e+05      2.2506e+05      2.0207e+05
v  k                   2.5622e-06           54.05         0.12396        0.080222
v  epsilon              0.0034205      9.3899e+06          9685.8          88.772
v  TurbVisc            2.4854e-11         0.64999       0.0027288        0.037655
v  total_pressure     -2.3734e+05      9.2268e+05      7.2506e+05      7.0207e+05


 TIME FOR THE TIME STEP              523:        0.74636E+02

===============================================================


 INSTANT    0.524000000E+03   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         0.878641357E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969710E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10797E+03 0.10439E+02
   Friction velocity        uet   :  0.39771E-01 0.74108E+01
   Friction velocity        uk    :  0.48122E-01 0.69100E+01
   Dimensionless distance   yplus :  0.33087E-03 0.36102E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15907
   Nb of facc  Velocity[X]                                      0.32540E+03 
c  Velocity[Y]                                      0.30283E+03 
c  Velocity[Z]                                      0.50352E+03 
c  Pressure     0.18565E+00     643   0.78484E-02   0.35305E+00 0.12015E+04 
c  k            0.11409E+01      77   0.50751E-02   0.51584E+01 0.14333E+04 
c  epsilon      0.22775E+05      55   0.58623E-02   0.25413E+11 0.13119E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016502                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.704          48.332          2.7568         0.30838
v  Velocity[Y]            -44.314          37.074          1.0013         0.71415
v  Velocity[Z]             -90.76           65.78         -1.2575      -0.0026401
v  ǁVelocityǁ          0.00092338           103.1           7.868           6.571
v  Pressure           -7.4093e+05      4.2203e+05      2.2523e+05      2.0242e+05
v  k                   2.8898e-06          52.867         0.12511        0.080775
v  epsilon              0.0042097      9.3062e+06            9786          90.828
v  TurbVisc            2.6081e-11         0.84452       0.0027579        0.037695
v  total_pressure     -2.4093e+05      9.2203e+05      7.2523e+05      7.0242e+05


 TIME FOR THE TIME STEP              525:        0.70996E+02

===============================================================


 INSTANT    0.526000000E+03   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.374906175E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         c  Velocity     0.10269E+02     116   0.19090E+00   0.11440E+04 0.87060E+03 
c  Velocity[X]                                      0.31991E+03 
c  Velocity[Y]                                      0.30523E+03 
c  Velocity[Z]                                      0.51885E+03 
c  Pressure     0.17472E+00     654   0.69051E-02   0.33362E+00 0.79134E+03 
c  k            0.10811E+01      74   0.48782E-02   0.33639E+01 0.12149E+04 
c  epsilon      0.22655E+05      53   0.48016E-02   0.16452E+11 0.36021E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.01429                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.842          47.068          2.7577          0.3083
v  Velocity[Y]            -35.074          37.035         0.99021         0.71448
v  Velocity[Z]            -68.141          60.018         -1.2672      -0.0021957
v  ǁVelocityǁ          0.00093825          81.898          7.8878          6.5754
v  Pressure           -7.4805e+05      4.2151e+05      2.2503e+05      2.0249e+05
v  k                   3.3157e-06          52.693         0.12606        0.080967
v  epsilon              0.0050362      9.3559e+06          9864.3           90.68
v  TurbVisc            2.6671e-11         0.70505       0.0027925        0.037725
v  total_pressure     -2.4805e+05      9.2151e+05      7.2503e+05      7.0249e+05


 TIME FOR THE TIME STEP              527:        0.69846E+02

===============================================================


 INSTANT    0.528000000E+03   TIME STEP NUMBER        c  Velocity[X]                                      0.32540E+03 
c  Velocity[Y]                                      0.30283E+03 
c  Velocity[Z]                                      0.50352E+03 
c  Pressure     0.18565E+00     643   0.78484E-02   0.35305E+00 0.12015E+04 
c  k            0.11409E+01      77   0.50751E-02   0.51584E+01 0.14333E+04 
c  epsilon      0.22775E+05      55   0.58623E-02   0.25413E+11 0.13119E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.016502                             4
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.704          48.332          2.7568         0.30838
v  Velocity[Y]            -44.314          37.074          1.0013         0.71415
v  Velocity[Z]             -90.76           65.78         -1.2575      -0.0026401
v  ǁVelocityǁ          0.00092338           103.1           7.868           6.571
v  Pressure           -7.4093e+05      4.2203e+05      2.2523e+05      2.0242e+05
v  k                   2.8898e-06          52.867         0.12511        0.080775
v  epsilon              0.0042097      9.3062e+06            9786          90.828
v  TurbVisc            2.6081e-11         0.84452       0.0027579        0.037695
v  total_pressure     -2.4093e+05      9.2203e+05      7.2523e+05      7.0242e+05


 TIME FOR THE TIME STEP              525:        0.66528E+02

===============================================================


 INSTANT    0.526000000E+03   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.374906175E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13741E+03 0.89976E+01
   Friction velocity        uet   :  0.39790E-01 0.74760E+01
   Friction velocity        uk    :  0.41026E-01 0.68711E+01
   Dimensionless distance   yplus :  0.33682E-03 0.35660E+02
   ---------------------------------------------------c  Velocity     0.10269E+02     116   0.19090E+00   0.11440E+04 0.87060E+03 
c  Velocity[X]                                      0.31991E+03 
c  Velocity[Y]                                      0.30523E+03 
c  Velocity[Z]                                      0.51885E+03 
c  Pressure     0.17472E+00     654   0.69051E-02   0.33362E+00 0.79134E+03 
c  k            0.10811E+01      74   0.48782E-02   0.33639E+01 0.12149E+04 
c  epsilon      0.22655E+05      53   0.48016E-02   0.16452E+11 0.36021E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.01429                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.842          47.068          2.7577          0.3083
v  Velocity[Y]            -35.074          37.035         0.99021         0.71448
v  Velocity[Z]            -68.141          60.018         -1.2672      -0.0021957
v  ǁVelocityǁ          0.00093825          81.898          7.8878          6.5754
v  Pressure           -7.4805e+05      4.2151e+05      2.2503e+05      2.0249e+05
v  k                   3.3157e-06          52.693         0.12606        0.080967
v  epsilon              0.0050362      9.3559e+06          9864.3           90.68
v  TurbVisc            2.6671e-11         0.70505       0.0027925        0.037725
v  total_pressure     -2.4805e+05      9.2151e+05      7.2503e+05      7.0249e+05


 TIME FOR THE TIME STEP              527:        0.70051E+02

===============================================================


 INSTANT    0.528000000E+03   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         0.391878241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11338E+03 0.89903E+01
   Friction velocity        uet   :  0.38389E-01 0.60386E+01
   Friction velocity        uk    :  0.41129E-01 0.68848E+01
   Dimensionless distance   yplus :  0.33987E-03 0.33233E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16019
   Nb of faces within the viscous sub-layer     :       9126
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10261E+02     116   0.18789E+00   0.10334E+04 0.82442E+03 
c  Velocity[X]                                      0.29857E+03 
c  Velocity[Y]                                      0.27611E+03 
c  Velocity[Z]                                      0.45871E+03 
c  Pressure     0.16563E+00     665   0.66525E-02   0.31494E+00 0.10132E+04 
c  k            0.98669E+00      73   0.63858E-02   0.57542E+01 0.14046E+04 
c  epsilon      0.22300E+05      51   0.47770E-02   0.66845E+10 0.10386E+06 
------------------------------------------------c  Velocity     0.10269E+02     116   0.19090E+00   0.11440E+04 0.87060E+03 
c  Velocity[X]                                      0.31991E+03 
c  Velocity[Y]                                      0.30523E+03 
c  Velocity[Z]                                      0.51885E+03 
c  Pressure     0.17472E+00     654   0.69051E-02   0.33362E+00 0.79134E+03 
c  k            0.10811E+01      74   0.48782E-02   0.33639E+01 0.12149E+04 
c  epsilon      0.22655E+05      53   0.48016E-02   0.16452E+11 0.36021E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.01429                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.842          47.068          2.7577          0.3083
v  Velocity[Y]            -35.074          37.035         0.99021         0.71448
v  Velocity[Z]            -68.141          60.018         -1.2672      -0.0021957
v  ǁVelocityǁ          0.00093825          81.898          7.8878          6.5754
v  Pressure           -7.4805e+05      4.2151e+05      2.2503e+05      2.0249e+05
v  k                   3.3157e-06          52.693         0.12606        0.080967
v  epsilon              0.0050362      9.3559e+06          9864.3           90.68
v  TurbVisc            2.6671e-11         0.70505       0.0027925        0.037725
v  total_pressure     -2.4805e+05      9.2151e+05      7.2503e+05      7.0249e+05


 TIME FOR THE TIME STEP              527:        0.60164E+02

===============================================================


 INSTANT    0.528000000E+03   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         0.391878241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11338E+03 0.89903E+01
   Friction velocity        uet   :  0.38389E-01 0.60386E+01
   Friction velocity        uk    :  0.41129E-01 0.68848E+01
   Di   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10263E+02     116   0.18525E+00   0.10474E+04 0.83082E+03 
c  Velocity[X]                                      0.30454E+03 
c  Velocity[Y]                                      0.28875E+03 
c  Velocity[Z]                                      0.45410E+03 
c  Pressure     0.18336E+00     735   0.57944E-02   0.35237E+00 0.19061E+04 
c  k            0.94022E+00      72   0.53420E-02   0.27947E+01 0.11553E+04 
c  epsilon      0.22099E+05      50   0.47776E-02   0.72880E+10 0.15851E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.013877                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.691          50.973          2.7582         0.30777
v  Velocity[Y]            -36.817          37.599         0.98473         0.71497
v  Velocity[Z]            -88.539          62.764         -1.2778      -0.0022017
v  ǁVelocityǁ           0.0009476          102.35          7.9113          6.5771
v  Pressure            -7.496e+05      4.2294e+05       2.255e+05      2.0305e+05
v  k                   3.8087e-06            44.9         0.12663        0.080954
v  epsilon              0.0058512      9.3638e+06          9899.5          89.187
v  TurbVisc            2.6952e-11         0.56748       0.0028256         0.03775
v  total_pressure      -2.496e+05      9.2294e+05       7.255e+05      7.0305e+05


 TIME FOR THE TIME STEP              529:        0.81491E+02

===============================================================


 INSTANT    0.530000000E+03   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         0.569552649E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12273E+03 0.89744E+01
   Friction velocity        uet   :  0.39804E-01 0.72804E+01
   Friction velocity        uk    :  0.57266E-01 0.69282E+01
   Dimensionless distance   yplus :  0.34145E-03 0.32144E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16090
   Nb of faces within the viscous sub-layer     :       9098
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10277E+02     118   0.18866E+00   0.10960E+04 0.83453E+03 
c  Velocity[X]                                      0.31358E+03 
c  Velocity[Y]                                      0.29389E+03 
c  Velocity[Z]                                      0.48850E+03 
c  Pressure     0.17590E+00     642   0.63320E-02   0.33514E+00 0.23761E+04 
c  k            0.94327E+00      72   0.35003E   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10263E+02     116   0.18525E+00   0.10474E+04 0.83082E+03 
c  Velocity[X]                                      0.30454E+03 
c  Velocity[Y]                                      0.28875E+03 
c  Velocity[Z]                                      0.45410E+03 
c  Pressure     0.18336E+00     735   0.57944E-02   0.35237E+00 0.19061E+04 
c  k            0.94022E+00      72   0.53420E-02   0.27947E+01 0.11553E+04 
c  epsilon      0.22099E+05      50   0.47776E-02   0.72880E+10 0.15851E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.013877                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.691          50.973          2.7582         0.30777
v  Velocity[Y]            -36.817          37.599         0.98473         0.71497
v  Velocity[Z]            -88.539          62.764         -1.2778      -0.0022017
v  ǁVelocityǁ           0.0009476          102.35          7.9113          6.5771
v  Pressure            -7.496e+05      4.2294e+05       2.255e+05      2.0305e+05
v  k                   3.8087e-06            44.9         0.12663        0.080954
v  epsilon              0.0058512      9.3638e+06          9899.5          89.187
v  TurbVisc            2.6952e-11         0.56748       0.0028256         0.03775
v  total_pressure      -2.496e+05      9.2294e+05       7.255e+05      7.0305e+05


 TIME FOR THE TIME STEP              529:        0.72470E+02

===============================================================


 INSTANT    0.530000000E+03   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         0.569552649E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12273E+03 0.89744E+01
   Friction velo      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10284E+02     118   0.18854E+00   0.11647E+04 0.86515E+03 
c  Velocity[X]                                      0.34382E+03 
c  Velocity[Y]                                      0.27737E+03 
c  Velocity[Z]                                      0.54346E+03 
c  Pressure     0.17681E+00     629   0.61490E-02   0.34237E+00 0.77418E+03 
c  k            0.88870E+00      73   0.53364E-02   0.25495E+01 0.11817E+04 
c  epsilon      0.22008E+05      52   0.45745E-02   0.10479E+11 0.11226E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.02945                             3
a  epsilon         -489.53                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.703          46.845          2.7594         0.30746
v  Velocity[Y]            -34.598            37.8         0.98437         0.71484
v  Velocity[Z]            -58.578          65.466         -1.2914      -0.0018594
v  ǁVelocityǁ          0.00096942          77.482          7.9409          6.5807
v  Pressure           -7.5442e+05      4.2394e+05      2.2594e+05      2.0354e+05
v  k                   4.3477e-06           43.29         0.12743        0.081081
v  epsilon              0.0066621        9.29e+06          9989.3          88.847
v  TurbVisc            2.7193e-11         0.57357       0.0028507        0.037773
v  total_pressure     -2.5442e+05      9.2394e+05      7.2594e+05      7.0354e+05


 TIME FOR THE TIME STEP              531:        0.69613E+02

===============================================================


 INSTANT    0.532000000E+03   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inle------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10286E+02     118   0.18699E+00   0.11533E+04 0.87370E+03 
c  Velocity[X]                                      0.30145E+03 
c  Velocity[Y]                                      0.33007E+03 
c  Velocity[Z]                                      0.52174E+03 
c  Pressure     0.21707E+00     717   0.59857E-02   0.42096E+00 0.26909E+04 
c  k            0.88218E+00      71   0.35381E-02   0.15668E+01 0.91754E+03 
c  epsilon      0.22056E+05      48   0.34233E-02   0.42748E+10 0.13065E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.017577                             3
a  epsilon        -0.17054                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.736          63.573          2.7646         0.30763
v  Velocity[Y]            -34.375          38.366          0.9872         0.71536
v  Velocity[Z]            -113.77            68.5         -1.3052      -0.0023078
v  ǁVelocityǁ          0.00096924          131.54          7.9732          6.5865
v  Pressure           -7.5754e+05      4.2656e+05      2.2743e+05      2.0469e+05
v  k                   4.9435e-06          41.988         0.12814        0.0      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10284E+02     118   0.18854E+00   0.11647E+04 0.86515E+03 
c  Velocity[X]                                      0.34382E+03 
c  Velocity[Y]                                      0.27737E+03 
c  Velocity[Z]                                      0.54346E+03 
c  Pressure     0.17681E+00     629   0.61490E-02   0.34237E+00 0.77418E+03 
c  k            0.88870E+00      73   0.53364E-02   0.25495E+01 0.11817E+04 
c  epsilon      0.22008E+05      52   0.45745E-02   0.10479E+11 0.11226E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.02945                             3
a  epsilon         -489.53                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.703          46.845          2.7594         0.30746
v  Velocity[Y]            -34.598            37.8         0.98437         0.71484
v  Velocity[Z]            -58.578          65.466         -1.2914      -0.0018594
v  ǁVelocityǁ          0.00096942          77.482          7.9409          6.5807
v  Pressure           -7.5442e+05      4.2394e+05      2.2594e+05      2.0354e+05
v  k                   4.3477e-06           43.29         0.12743        0.081081
v  epsilon              0.0066621        9.29e+06          9989.3          88.847
v  TurbVisc            2.7193e-11         0.57357       0.0028507        0.037773
v  total_pressure     -2.5442e+05      9.2394e+05      7.2594e+05      7.0354e+05


 TIME FOR THE TIME STEP              531:        0.68277E+02

===============================================================


 INSTANT    0.532000000E+03   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.244616364E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Max------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10286E+02     118   0.18699E+00   0.11533E+04 0.87370E+03 
c  Velocity[X]                                      0.30145E+03 
c  Velocity[Y]                                      0.33007E+03 
c  Velocity[Z]                                      0.52174E+03 
c  Pressure     0.21707E+00     717   0.59857E-02   0.42096E+00 0.26909E+04 
c  k            0.88218E+00      71   0.35381E-02   0.15668E+01 0.91754E+03 
c  epsilon      0.22056E+05      48   0.34233E-02   0.42748E+10 0.13065E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.017577                             3
a  epsilon        -0.17054                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.736          63.573          2.7646         0.30763
v  Velocity[Y]            -34.375          38.366          0.9872         0.71536
v  Velocity[Z]            -113.77            68.5         -1.3052      -0.0023078
v  ǁVelocityǁ          0.00096924          131.54          7.9732          6.5865
v  Pressure           -7.5754e+05      4.2656e+05      2.2743e+05      2.0469e+05
v  k                   4.9435e-06          41.988         0.12814        0.081217
v  epsilon              0.0073781      9.3116e+06           10062          88.874
v  TurbVisc            2.7445e-11         0.53799       0.0028701        0.037792
v  total_pressure     -2.5754e+05      9.2656e+05      7.2743e+05      7.0469e+05


 TIME FOR THE TIME STEP              533:        0.72109E+02

===============================================================


 INSTANT    0.534000000E+03   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-------------------------------------------------------   Nb of reversal of the velocity at the wall   :      16275
   Nb of faces within the viscous sub-layer     :       9058
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10296E+02     120   0.18996E+00   0.12569E+04 0.88118E+03 
c  Velocity[X]                                      0.34483E+03 
c  Velocity[Y]                                      0.26929E+03 
c  Velocity[Z]                                      0.64278E+03 
c  Pressure     0.17519E+00     824   0.69598E-02   0.34115E+00 0.15370E+04 
c  k            0.99216E+00      70   0.61119E-02   0.77852E+01 0.16227E+04 
c  epsilon      0.22603E+05      51   0.46236E-02   0.56943E+10 0.37047E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015716                             3
a  epsilon         -1.2033                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.813          47.474           2.772         0.30807
v  Velocity[Y]            -40.083          37.655          0.9926         0.71521
v  Velocity[Z]             -70.12          61.713         -1.3185      -0.0025075
v  ǁVelocityǁ          0.00097433          78.361           8.005          6.5926
v  Pressure           -7.5884e+05        4.29e+05      2.2876e+05      2.0579e+05
v  k                   5.6217e-06          51.818          0.1291        0.081526
v  epsilon              0.0078974      9.3294e+06           10131           90.18
v  TurbVisc            2.7527e-11         0.54241       0.0028978        0.037811
v  total_pressure     -2.5884e+05        9.29e+05      7.2876e+05      7.0579e+05


 TIME FOR THE TIME STEP              535:        0.79965E+02

===============================================================


 INSTANT    0.536000000E+03   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.137359243E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12822E+03 0.99257E+01
   Friction velocity        uet   :  0.37515E-01 0.59978E+01
   Friction velocity        uk    :  0.58999E-01 0.69467E+01
   Dimensionless distance   yplus :  0.34643E-03 0.34348E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16291
   Nb of faces within the viscous sub-layer     :       9041
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10291E+02     119   0.19110E+00   0.98796E+03 0.82173E+03 
c  Velocity[X]                                      0.30381E+03 
c  Velocity[Y]                                      0.27320E+03 
c  Velocity[Z]                                      0.41095E+03 
c  Pressure     0.17375E+00     912   0.62370E-02   0.33505E+00 0.22161E+04 
c  k            0.10826E+01      72   0.95638E-02   0.10096E+02 0.18010E+04 
c  epsilon      0.23055E+05      53   0.64448E-02   0.25269E+11 0.44541E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  -----------   Nb of reversal of the velocity at the wall   :      16275
   Nb of faces within the viscous sub-layer     :       9058
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10296E+02     120   0.18996E+00   0.12569E+04 0.88118E+03 
c  Velocity[X]                                      0.34483E+03 
c  Velocity[Y]                                      0.26929E+03 
c  Velocity[Z]                                      0.64278E+03 
c  Pressure     0.17519E+00     824   0.69598E-02   0.34115E+00 0.15370E+04 
c  k            0.99216E+00      70   0.61119E-02   0.77852E+01 0.16227E+04 
c  epsilon      0.22603E+05      51   0.46236E-02   0.56943E+10 0.37047E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015716                             3
a  epsilon         -1.2033                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.813          47.474           2.772         0.30807
v  Velocity[Y]            -40.083          37.655          0.9926         0.71521
v  Velocity[Z]             -70.12          61.713         -1.3185      -0.0025075
v  ǁVelocityǁ          0.00097433          78.361           8.005          6.5926
v  Pressure           -7.5884e+05        4.29e+05      2.2876e+05      2.0579e+05
v  k                   5.6217e-06          51.818          0.1291        0.081526
v  epsilon              0.0078974      9.3294e+06           10131           90.18
v  TurbVisc            2.7527e-11         0.54241       0.0028978        0.037811
v  total_pressure     -2.5884e+05        9.29e+05      7.2876e+05      7.0579e+05


 TIME FOR THE TIME STEP              535:        0.70569E+02

===============================================================


 INSTANT    0.536000000E+03   TIME STEP NUMBER             536
 =================   Friction velocity        uk    :  0.49185E-01 0.68992E+01
   Dimensionless distance   yplus :  0.34722E-03 0.34982E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16357
   Nb of faces within the viscous sub-layer     :       9036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10298E+02     119   0.18646E+00   0.10487E+04 0.83357E+03 
c  Velocity[X]                                      0.29432E+03 
c  Velocity[Y]                                      0.28424E+03 
c  Velocity[Z]                                      0.47019E+03 
c  Pressure     0.19185E+00     738   0.70654E-02   0.37149E+00 0.93833E+03 
c  k            0.10216E+01      72   0.10343E-01   0.15601E+02 0.21314E+04 
c  epsilon      0.22936E+05      52   0.71350E-02   0.37284E+10 0.25412E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015462                             4
a  epsilon         -1.3428                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.999          54.673          2.7784         0.30886
v  Velocity[Y]            -34.765          37.964          1.0023         0.7147   Nb of reversal of the velocity at the wall   :      16275
   Nb of faces within the viscous sub-layer     :       9058
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10296E+02     120   0.18996E+00   0.12569E+04 0.88118E+03 
c  Velocity[X]                                      0.34483E+03 
c  Velocity[Y]                                      0.26929E+03 
c  Velocity[Z]                                      0.64278E+03 
c  Pressure     0.17519E+00     824   0.69598E-02   0.34115E+00 0.15370E+04 
c  k            0.99216E+00      70   0.61119E-02   0.77852E+01 0.16227E+04 
c  epsilon      0.22603E+05      51   0.46236E-02   0.56943E+10 0.37047E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015716                             3
a  epsilon         -1.2033                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.813          47.474           2.772         0.30807
v  Velocity[Y]            -40.083          37.655          0.9926         0.71521
v  Velocity[Z]             -70.12          61.713         -1.3185      -0.0025075
v  ǁVelocityǁ          0.00097433          78.361           8.005          6.5926
v  Pressure           -7.5884e+05        4.29e+05      2.2876e+05      2.0579e+05
v  k                   5.6217e-06          51.818          0.1291        0.081526
v  epsilon              0.0078974      9.3294e+06           10131           90.18
v  TurbVisc            2.7527e-11         0.54241       0.0028978        0.037811
v  total_pressure     -2.5884e+05        9.29e+05      7.2876e+05      7.0579e+05


 TIME FOR THE TIME STEP              535:        0.78325E+02

===============================================================


 INSTANT    0.536000000E+03   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.137359243E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined          Friction velocity        uk    :  0.49185E-01 0.68992E+01
   Dimensionless distance   yplus :  0.34722E-03 0.34982E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16357
   Nb of faces within the viscous sub-layer     :       9036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10298E+02     119   0.18646E+00   0.10487E+04 0.83357E+03 
c  Velocity[X]                                      0.29432E+03 
c  Velocity[Y]                                      0.28424E+03 
c  Velocity[Z]                                      0.47019E+03 
c  Pressure     0.19185E+00     738   0.70654E-02   0.37149E+00 0.93833E+03 
c  k            0.10216E+01      72   0.10343E-01   0.15601E+02 0.21314E+04 
c  epsilon      0.22936E+05      52   0.71350E-02   0.37284E+10 0.25412E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015462                             4
a  epsilon         -1.3428                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.999          54.673          2.7784         0.30886
v  Velocity[Y]            -34.765          37.964          1.0023         0.71475
v  Velocity[Z]            -97.388          61.361          -1.332      -0.0022615
v  ǁVelocityǁ          0.00098576          112.07          8.0371          6.5999
v  Pressure           -7.6162e+05      4.3207e+05      2.3042e+05      2.0714e+05
v  k                   6.4063e-06          49.555         0.13007        0.081716
v  epsilon              0.0083079      9.3279e+06           10221          91.013
v  TurbVisc            2.7973e-11         0.67426       0.0029332        0.037829
v  total_pressure     -2.6162e+05      9.3207e+05      7.3042e+05      7.0714e+05


 TIME FOR THE TIME STEP   ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23340E+03 0.16817E+02
   Friction velocity        uet   :  0.33181E-01 0.78312E+01
   Friction velocity        uk    :  0.50960E-01 0.69393E+01
   Dimensionless distance   yplus :  0.34982E-03 0.32984E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16404
   Nb of faces within the viscous sub-layer     :       9028
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10330E+02     118   0.18977E+00   0.13134E+04 0.88592E+03 
c  Velocity[X]                                      0.33396E+03 
c  Velocity[Y]                                      0.32030E+03 
c  Velocity[Z]                                      0.65910E+03 
c  Pressure     0.18510E+00     862   0.71242E-02   0.35474E+00 0.11092E+04 
c  k            0.90344E+00      75   0.83878E-02   0.85711E+01 0.19098E+04 
c  epsilon      0.22675E+05      53   0.53587E-02   0.13438E+11 0.56826E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015614                             2
a  epsilon        -0.90261                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  -------------   Friction velocity        uk    :  0.49185E-01 0.68992E+01
   Dimensionless distance   yplus :  0.34722E-03 0.34982E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16357
   Nb of faces within the viscous sub-layer     :       9036
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10298E+02     119   0.18646E+00   0.10487E+04 0.83357E+03 
c  Velocity[X]                                      0.29432E+03 
c  Velocity[Y]                                      0.28424E+03 
c  Velocity[Z]                                      0.47019E+03 
c  Pressure     0.19185E+00     738   0.70654E-02   0.37149E+00 0.93833E+03 
c  k            0.10216E+01      72   0.10343E-01   0.15601E+02 0.21314E+04 
c  epsilon      0.22936E+05      52   0.71350E-02   0.37284E+10 0.25412E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015462                             4
a  epsilon         -1.3428                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.999          54.673          2.7784         0.30886
v  Velocity[Y]            -34.765          37.964          1.0023         0.71475
v  Velocity[Z]            -97.388          61.361          -1.332      -0.0022615
v  ǁVelocityǁ          0.00098576          112.07          8.0371          6.5999
v  Pressure           -7.6162e+05      4.3207e+05      2.3042e+05      2.0714e+05
v  k                   6.4063e-06          49.555         0.13007        0.081716
v  epsilon              0.0083079      9.3279e+06           10221          91.013
v  TurbVisc            2.7973e-11         0.67426       0.0029332        0.037829
v  total_pressure     -2.6162e+05      9.3207e+05      7.3042e+05      7.0714e+05


 TIME FOR THE TIME STEP              537:        0.76538E+02

===============================================================


 INSTANT    0.538000000E+03   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.194241207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23340E+03 0.16817E+02
   Friction velocity        uet   :  0.33181E-01 0.78312E+01
   Friction velocity        uk    :  0.50960E-01 0.69393E+01
   Dimensionless distance   yplus :  0.34982E-03 0.32984E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16404
   Nb of faces within the viscous sub-layer     :       9028
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10330E+02     118   0.18977E+00   0.13134E+04 0.88592E+03 
c  Velocity[X]                                      0.33396E+03 
c  Velocity[Y]                                      0.32030E+03 
c  Velocity[Z]                                      0.65910E+03 
c  Pressure     0.18510E+00     862   0.71242E-02   0.35474E+00 0.11092E+04 
c  k            0.90344E+00      75   0.83878E-02   0.85711E+01 0.19098E+04 
c  epsilon      0.22675E+05      53   0.53587E-02   0.13438E+11 0.56826E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015614                             2
a  epsilon        -0.90261                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.144          46.374          2.7833         0.30852
v  Velocity[Y]             -35.98          37.105          1.0144          0.7143
v  Velocity[Z]            -67.356          67.665          -1.341      -0.0016483
v  ǁVelocityǁ          0.00099325          84.661          8.0682          6.6063
v  Pressure           -7.6352e+05      4.3486e+05      2.3201e+05      2.0846e+05
v  k                   7.2943e-06          36.373         0.13095        0.081626
v  epsilon              0.0087753      9.4148e+06           10338           89.96
v  TurbVisc             2.8   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22895E+03 0.20478E+02
   Friction velocity        uet   :  0.25671E-01 0.74061E+01
   Friction velocity        uk    :  0.25642E-01 0.68978E+01
   Dimensionless distance   yplus :  0.35068E-03 0.36620E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16450
   Nb of faces within the viscous sub-layer     :       9005
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10339E+02     119   0.18933E+00   0.12817E+04 0.89525E+03 
c  Velocity[X]                                      0.36526E+03 
c  Velocity[Y]                                      0.30734E+03 
c  Velocity[Z]                                      0.60909E+03 
c  Pressure     0.18335E+00     771   0.72221E-02   0.35046E+00 0.79545E+03 
c  k            0.94742E+00      75   0.79873E-02   0.56879E+01 0.16152E+04 
c  epsilon      0.23065E+05      54   0.53779E-02   0.10854E+11 0.74792E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014866                             2
a  epsilon        -0.67025                             2


  ** Computed fields on ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23340E+03 0.16817E+02
   Friction velocity        uet   :  0.33181E-01 0.78312E+01
   Friction velocity        uk    :  0.50960E-01 0.69393E+01
   Dimensionless distance   yplus :  0.34982E-03 0.32984E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16404
   Nb of faces within the viscous sub-layer     :       9028
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10330E+02     118   0.18977E+00   0.13134E+04 0.88592E+03 
c  Velocity[X]                                      0.33396E+03 
c  Velocity[Y]                                      0.32030E+03 
c  Velocity[Z]                                      0.65910E+03 
c  Pressure     0.18510E+00     862   0.71242E-02   0.35474E+00 0.11092E+04 
c  k            0.90344E+00      75   0.83878E-02   0.85711E+01 0.19098E+04 
c  epsilon      0.22675E+05      53   0.53587E-02   0.13438E+11 0.56826E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.015614                             2
a  epsilon        -0.90261                             3


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.144          46.374          2.7833         0.30852
v  Velocity[Y]             -35.98          37.105          1.0144          0.7143
v  Velocity[Z]            -67.356          67.665          -1.341      -0.0016483
v  ǁVelocityǁ          0.00099325          84.661          8.0682          6.6063
v  Pressure           -7.6352e+05      4.3486e+05      2.3201e+05      2.0846e+05
v  k                   7.2943e-06          36.373         0.13095        0.081626
v  epsilon              0.0087753      9.4148e+06           10338           89.96
v  TurbVisc             2.831e-11         0.46348       0.0029687        0.037842
v  total_pressure     -2.6352e+05      9.3486e+05      7.3201e+05      7.0846e+05


 TIME FOR THE TIME STEP              539:        0.83192E+02

===============================================================


 INSTANT    0.540000000E+03   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         0.552547977E-17
Rough wall                6           0         0.00   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22895E+03 0.20478E+02
   Friction velocity        uet   :  0.25671E-01 0.74061E+01
   Friction velocity        uk    :  0.25642E-01 0.68978E+01
   Dimensionless distance   yplus :  0.35068E-03 0.36620E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16450
   Nb of faces within the viscous sub-layer     :       9005
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10339E+02     119   0.18933E+00   0.12817E+04 0.89525E+03 
c  Velocity[X]                                      0.36526E+03 
c  Velocity[Y]                                      0.30734E+03 
c  Velocity[Z]                                      0.60909E+03 
c  Pressure     0.18335E+00     771   0.72221E-02   0.35046E+00 0.79545E+03 
c  k            0.94742E+00      75   0.79873E-02   0.56879E+01 0.16152E+04 
c  epsilon      0.23065E+05      54   0.53779E-02   0.10854E+11 0.74792E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014866                             2
a  epsilon        -0.67025                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.086          47.086          2.7878         0.30842
v  Velocity[Y]            -35.356           37.14          1.0279         0.71369
v  Velocity[Z]            -66.771          61.394          -1.347       -0.001597
v  ǁVelocityǁ          0.00098956          78.678          8.0956          6.6125
v  Pressure           -7.6459e+05      4.3724e+05      2.3292e+05      2.0922e+05
v  k              Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17417E+03 0.21086E+02
   Friction velocity        uet   :  0.44680E-01 0.63401E+01
   Friction velocity        uk    :  0.49728E-01 0.69235E+01
   Dimensionless distance   yplus :  0.35168E-03 0.39089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16461
   Nb of faces within the viscous sub-layer     :       8995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10378E+02     119   0.19304E+00   0.12516E+04 0.90836E+03 
c  Velocity[X]                                      0.34879E+03 
c  Velocity[Y]                                      0.32934E+03 
c  Velocity[Z]                                      0.57342E+03 
c  Pressure     0.19320E+00     735   0.73643E-02   0.36580E+00 0.10231E+04 
c  k            0.11234E+01      70   0.90315E-02   0.72577E+01 0.14497E+04 
c  epsilon      0.24094E+05      51   0.75682E-02   0.12835E+11 0.59217E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  --   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22895E+03 0.20478E+02
   Friction velocity        uet   :  0.25671E-01 0.74061E+01
   Friction velocity        uk    :  0.25642E-01 0.68978E+01
   Dimensionless distance   yplus :  0.35068E-03 0.36620E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16450
   Nb of faces within the viscous sub-layer     :       9005
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10339E+02     119   0.18933E+00   0.12817E+04 0.89525E+03 
c  Velocity[X]                                      0.36526E+03 
c  Velocity[Y]                                      0.30734E+03 
c  Velocity[Z]                                      0.60909E+03 
c  Pressure     0.18335E+00     771   0.72221E-02   0.35046E+00 0.79545E+03 
c  k            0.94742E+00      75   0.79873E-02   0.56879E+01 0.16152E+04 
c  epsilon      0.23065E+05      54   0.53779E-02   0.10854E+11 0.74792E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014866                             2
a  epsilon        -0.67025                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.086          47.086          2.7878         0.30842
v  Velocity[Y]            -35.356           37.14          1.0279         0.71369
v  Velocity[Z]            -66.771          61.394          -1.347       -0.001597
v  ǁVelocityǁ          0.00098956          78.678          8.0956          6.6125
v  Pressure           -7.6459e+05      4.3724e+05      2.3292e+05      2.0922e+05
v  k                   8.2641e-06           43.59         0.13209        0.081751
v  epsilon              0.0092179      9.5509e+06           10456          90.195
v  TurbVisc            2.8296e-11         0.41839       0.0030011        0.037856
v  total_pressure     -2.6459e+05      9.3724e+05      7.3292e+05      7.0922e+05


 TIME FOR THE TIME STEP              541:        0.74337E+02

===============================================================


 INSTANT    0.542000000E+03   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet  Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17417E+03 0.21086E+02
   Friction velocity        uet   :  0.44680E-01 0.63401E+01
   Friction velocity        uk    :  0.49728E-01 0.69235E+01
   Dimensionless distance   yplus :  0.35168E-03 0.39089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16461
   Nb of faces within the viscous sub-layer     :       8995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10378E+02     119   0.19304E+00   0.12516E+04 0.90836E+03 
c  Velocity[X]                                      0.34879E+03 
c  Velocity[Y]                                      0.32934E+03 
c  Velocity[Z]                                      0.57342E+03 
c  Pressure     0.19320E+00     735   0.73643E-02   0.36580E+00 0.10231E+04 
c  k            0.11234E+01      70   0.90315E-02   0.72577E+01 0.14497E+04 
c  epsilon      0.24094E+05      51   0.75682E-02   0.12835E+11 0.59217E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014779                             3
a  epsilon        -0.98654                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.182          45.935          2.7922         0.30955
v  Velocity[Y]            -38.622          41.135          1.0364         0.71366
v  Velocity[Z]            -70.417          64.864         -1.3502       -0Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20168E+03 0.21320E+02
   Friction velocity        uet   :  0.34605E-01 0.68904E+01
   Friction velocity        uk    :  0.46815E-01 0.69548E+01
   Dimensionless distance   yplus :  0.35364E-03 0.39250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16517
   Nb of faces within the viscous sub-layer     :       8967
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10395E+02     117   0.19096E+00   0.12508E+04 0.87673E+03 
c  Velocity[X]                                      0.32602E+03 
c  Velocity[Y]                                      0.34234E+03 
c  Velocity[Z]                                      0.58247E+03 
c  Pressure     0.19636E+00     695   0.78396E-02   0.36948E+00 0.61441E+03 
c  k            0.12832E+01      68   0.67169E-02   0.91761E+01 0.13478E+04 
c  epsilon      0.25353E+05      48   0.55170E-02   0.70531E+10 0.15927E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17417E+03 0.21086E+02
   Friction velocity        uet   :  0.44680E-01 0.63401E+01
   Friction velocity        uk    :  0.49728E-01 0.69235E+01
   Dimensionless distance   yplus :  0.35168E-03 0.39089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16461
   Nb of faces within the viscous sub-layer     :       8995
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10378E+02     119   0.19304E+00   0.12516E+04 0.90836E+03 
c  Velocity[X]                                      0.34879E+03 
c  Velocity[Y]                                      0.32934E+03 
c  Velocity[Z]                                      0.57342E+03 
c  Pressure     0.19320E+00     735   0.73643E-02   0.36580E+00 0.10231E+04 
c  k            0.11234E+01      70   0.90315E-02   0.72577E+01 0.14497E+04 
c  epsilon      0.24094E+05      51   0.75682E-02   0.12835E+11 0.59217E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014779                             3
a  epsilon        -0.98654                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.182          45.935          2.7922         0.30955
v  Velocity[Y]            -38.622          41.135          1.0364         0.71366
v  Velocity[Z]            -70.417          64.864         -1.3502       -0.001514
v  ǁVelocityǁ           0.0010056          79.702          8.1195          6.6191
v  Pressure           -7.6512e+05      4.3954e+05      2.3411e+05      2.1015e+05
v  k                   9.2975e-06          47.735          0.1331        0.082142
v  epsilon              0.0093584      9.4315e+06           10487           92.38
v  TurbVisc            2.8468e-11         0.56566       0.0030296        0.037872
v  total_pressure     -2.6512e+05      9.3954e+05      7.3411e+05      7.1015e+05


 TIME FOR THE TIME STEP              543:        0.72632E+02

===============================================================


 INSTANT    0.544000000E+03   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20168E+03 0.21320E+02
   Friction velocity        uet   :  0.34605E-01 0.68904E+01
   Friction velocity        uk    :  0.46815E-01 0.69548E+01
   Dimensionless distance   yplus :  0.35364E-03 0.39250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16517
   Nb of faces within the viscous sub-layer     :       8967
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10395E+02     117   0.19096E+00   0.12508E+04 0.87673E+03 
c  Velocity[X]                                      0.32602E+03 
c  Velocity[Y]                                      0.34234E+03 
c  Velocity[Z]                                      0.58247E+03 
c  Pressure     0.19636E+00     695   0.78396E-02   0.36948E+00 0.61441E+03 
c  k            0.12832E+01      68   0.67169E-02   0.91761E+01 0.13478E+04 
c  epsilon      0.25353E+05      48   0.55170E-02   0.70531E+10 0.15927E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014271                             2
a  epsilon         -0.6098                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.074           46Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20394E+03 0.28613E+02
   Friction velocity        uet   :  0.43472E-01 0.71919E+01
   Friction velocity        uk    :  0.44889E-01 0.68916E+01
   Dimensionless distance   yplus :  0.35269E-03 0.38522E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16547
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10416E+02     116   0.18933E+00   0.11366E+04 0.82667E+03 
c  Velocity[X]                                      0.32306E+03 
c  Velocity[Y]                                      0.28190E+03 
c  Velocity[Z]                                      0.53164E+03 
c  Pressure     0.19218E+00     751   0.60497E-02   0.36402E+00 0.46711E+03 
c  k            0.13692E+01      70   0.99018E-02   0.21914E+0Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20168E+03 0.21320E+02
   Friction velocity        uet   :  0.34605E-01 0.68904E+01
   Friction velocity        uk    :  0.46815E-01 0.69548E+01
   Dimensionless distance   yplus :  0.35364E-03 0.39250E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16517
   Nb of faces within the viscous sub-layer     :       8967
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10395E+02     117   0.19096E+00   0.12508E+04 0.87673E+03 
c  Velocity[X]                                      0.32602E+03 
c  Velocity[Y]                                      0.34234E+03 
c  Velocity[Z]                                      0.58247E+03 
c  Pressure     0.19636E+00     695   0.78396E-02   0.36948E+00 0.61441E+03 
c  k            0.12832E+01      68   0.67169E-02   0.91761E+01 0.13478E+04 
c  epsilon      0.25353E+05      48   0.55170E-02   0.70531E+10 0.15927E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014271                             2
a  epsilon         -0.6098                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.074           46.16          2.7943         0.30881
v  Velocity[Y]            -34.701          37.511           1.039         0.71407
v  Velocity[Z]            -79.827          61.249          -1.355      -0.0014954
v  ǁVelocityǁ           0.0010022          89.279          8.1367          6.6259
v  Pressure           -7.6509e+05       4.404e+05      2.3505e+05       2.108e+05
v  k                   1.0374e-05          53.537         0.13441        0.082646
v  epsilon              0.0090525      9.2942e+06           10546          95.106
v  TurbVisc            2.8557e-11         0.60889       0.0030608        0.037894
v  total_pressure     -2.6509e+05       9.404e+05      7.3505e+05       7.108e+05


 TIME FOR THE TIME STEP              545:        0.71701E+02

===============================================================


 INSTANT    0.546Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20394E+03 0.28613E+02
   Friction velocity        uet   :  0.43472E-01 0.71919E+01
   Friction velocity        uk    :  0.44889E-01 0.68916E+01
   Dimensionless distance   yplus :  0.35269E-03 0.38522E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16547
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10416E+02     116   0.18933E+00   0.11366E+04 0.82667E+03 
c  Velocity[X]                                      0.32306E+03 
c  Velocity[Y]                                      0.28190E+03 
c  Velocity[Z]                                      0.53164E+03 
c  Pressure     0.19218E+00     751   0.60497E-02   0.36402E+00 0.46711E+03 
c  k            0.13692E+01      70   0.99018E-02   0.21914E+02 0.19871E+04 
c  epsilon      0.25974E+05      48   0.85320E-02   0.47424E+11 0.24810E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014053                             3
a  epsilon         -1.5685                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum   Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.435516485E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969746E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13417E+03 0.27549E+02
   Friction velocity        uet   :  0.31309E-01 0.60672E+01
   Friction velocity        uk    :  0.39796E-01 0.69168E+01
   Dimensionless distance   yplus :  0.35367E-03 0.39262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16561
   Nb of faces within the viscous sub-layer     :       8942
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10419E+02     118   0.19302E+00   0.10597E+04 0.81155E+03 
c  Velocity[X]                                      0.31275E+03 
c  Velocity[Y]                                      0.28868E+03 
c  Velocity[Z]                                      0.4582Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20394E+03 0.28613E+02
   Friction velocity        uet   :  0.43472E-01 0.71919E+01
   Friction velocity        uk    :  0.44889E-01 0.68916E+01
   Dimensionless distance   yplus :  0.35269E-03 0.38522E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16547
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10416E+02     116   0.18933E+00   0.11366E+04 0.82667E+03 
c  Velocity[X]                                      0.32306E+03 
c  Velocity[Y]                                      0.28190E+03 
c  Velocity[Z]                                      0.53164E+03 
c  Pressure     0.19218E+00     751   0.60497E-02   0.36402E+00 0.46711E+03 
c  k            0.13692E+01      70   0.99018E-02   0.21914E+02 0.19871E+04 
c  epsilon      0.25974E+05      48   0.85320E-02   0.47424E+11 0.24810E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.014053                             3
a  epsilon         -1.5685                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.178          49.362          2.7941         0.30913
v  Velocity[Y]            -39.245          36.112          1.0372          0.7141
v  Velocity[Z]            -85.855          63.858         -1.3585      -0.0018281
v  ǁVelocityǁ            0.001004          96.979          8.1499          6.6285
v  Pressure           -7.6444e+05      4.4229e+05      2.3552e+05       2.112e+05
v  k                   1.0896e-06          62.336         0.13574        0.083169
v  epsilon              0.0084919      9.4017e+06           10677          97.341
v  TurbVisc            2.8608e-11         0.67842       0.0030953        0.037923
v  total_pressure     -2.6444e+05      9.4229e+05      Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.435516485E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969746E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13417E+03 0.27549E+02
   Friction velocity        uet   :  0.31309E-01 0.60672E+01
   Friction velocity        uk    :  0.39796E-01 0.69168E+01
   Dimensionless distance   yplus :  0.35367E-03 0.39262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16561
   Nb of faces within the viscous sub-layer     :       8942
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10419E+02     118   0.19302E+00   0.10597E+04 0.81155E+03 
c  Velocity[X]                                      0.31275E+03 
c  Velocity[Y]                                      0.28868E+03 
c  Velocity[Z]                                      0.45829E+03 
c  Pressure     0.18503E+00     630   0.66113E-02   0.35298E+00 0.28260E+03 
c  k            0.14132E+01      73   0.52576E-02   0.88795E+01 0.14616E+04 
c  epsilon      0.26294E+05      52   0.52712E-02   0.18277E+11 0.22570E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.01393                             3
a  epsilon       -0.053242      Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.213620214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14276E+03 0.24868E+02
   Friction velocity        uet   :  0.34942E-01 0.60765E+01
   Friction velocity        uk    :  0.40826E-01 0.69792E+01
   Dimensionless distance   yplus :  0.35491E-03 0.38434E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16604
   Nb of faces within the viscous sub-layer     :       8923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10439E+02     118   0.18717E+00   0.11625E+04 0.87186E+03 
c  Velocity[X]                                      0.31214EInlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.435516485E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969746E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13417E+03 0.27549E+02
   Friction velocity        uet   :  0.31309E-01 0.60672E+01
   Friction velocity        uk    :  0.39796E-01 0.69168E+01
   Dimensionless distance   yplus :  0.35367E-03 0.39262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16561
   Nb of faces within the viscous sub-layer     :       8942
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10419E+02     118   0.19302E+00   0.10597E+04 0.81155E+03 
c  Velocity[X]                                      0.31275E+03 
c  Velocity[Y]                                      0.28868E+03 
c  Velocity[Z]                                      0.45829E+03 
c  Pressure     0.18503E+00     630   0.66113E-02   0.35298E+00 0.28260E+03 
c  k            0.14132E+01      73   0.52576E-02   0.88795E+01 0.14616E+04 
c  epsilon      0.26294E+05      52   0.52712E-02   0.18277E+11 0.22570E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.01393                             3
a  epsilon       -0.053242                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.007          47.605          2.7927         0.30923
v  Velocity[Y]            -42.667          37.368          1.0365         0.71394
v  Velocity[Z]            -75.772          61.582         -1.3632      -0.0019536
v  ǁVelocityǁ           0.0010106          91.762          8.1632          6.6326
v  Pressure           -7.6314e+05      4.4436e+05      2.3647e+05        2.12e+05
v  k                   1.0539e-05          60.317         0.13648        0.083675
v  epsilon              0.0079334      9.4597e+06           10671          98.979
v  TurbVisc  Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.213620214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14276E+03 0.24868E+02
   Friction velocity        uet   :  0.34942E-01 0.60765E+01
   Friction velocity        uk    :  0.40826E-01 0.69792E+01
   Dimensionless distance   yplus :  0.35491E-03 0.38434E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16604
   Nb of faces within the viscous sub-layer     :       8923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10439E+02     118   0.18717E+00   0.11625E+04 0.87186E+03 
c  Velocity[X]                                      0.31214E+03 
c  Velocity[Y]                                      0.34158E+03 
c  Velocity[Z]                                      0.50874E+03 
c  Pressure     0.17169E+00     790   0.71548E-02   0.32511E+00 0.18807E+04 
c  k            0.12975E+01      71   0.83219E-02   0.11339E+02 0.16110E+04 
c  epsilon      0.25707E+05      51   0.63846E-02   0.14887E+11 0.18200E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ---------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.490236683E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19118E+03 0.25865E+02
   Friction velocity        uet   :  0.36962E-01 0.72233E+01
   Friction velocity        uk    :  0.40499E-01 0.69062E+01
   Dimensionless distance   yplus :  0.35706E-03 0.38761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16653
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10458E+02     118   0.19330E+00   0.10662Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.213620214E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14276E+03 0.24868E+02
   Friction velocity        uet   :  0.34942E-01 0.60765E+01
   Friction velocity        uk    :  0.40826E-01 0.69792E+01
   Dimensionless distance   yplus :  0.35491E-03 0.38434E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16604
   Nb of faces within the viscous sub-layer     :       8923
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10439E+02     118   0.18717E+00   0.11625E+04 0.87186E+03 
c  Velocity[X]                                      0.31214E+03 
c  Velocity[Y]                                      0.34158E+03 
c  Velocity[Z]                                      0.50874E+03 
c  Pressure     0.17169E+00     790   0.71548E-02   0.32511E+00 0.18807E+04 
c  k            0.12975E+01      71   0.83219E-02   0.11339E+02 0.16110E+04 
c  epsilon      0.25707E+05      51   0.63846E-02   0.14887E+11 0.18200E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024285                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.083          45.915          2.7923         0.30849
v  Velocity[Y]            -35.503          37.814          1.0401         0.71388
v  Velocity[Z]            -77.495          62.881         -1.3681      -0.0020444
v  ǁVelocityǁ           0.0010223          87.369          8.1788          6.6357
v  Pressure           -7.6431e+05      4.4535e+05      2.3783e+05      2.1297e+05
v  k                   1.0183e-05          56.305         0.13714        0.084007
v  epsilon              0.00744---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.490236683E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19118E+03 0.25865E+02
   Friction velocity        uet   :  0.36962E-01 0.72233E+01
   Friction velocity        uk    :  0.40499E-01 0.69062E+01
   Dimensionless distance   yplus :  0.35706E-03 0.38761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16653
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10458E+02     118   0.19330E+00   0.10662E+04 0.80474E+03 
c  Velocity[X]                                      0.31737E+03 
c  Velocity[Y]                                      0.31266E+03 
c  Velocity[Z]                                      0.43618E+03 
c  Pressure     0.17650E+00     664   0.65056E-02   0.33103E+00 0.16425E+04 
c  k            0.11633E+01      68   0.71025E-02   0.58675E+01 0.13371E+04 
c  epsilon      0.25048E+05      48   0.53228E-02   0.77996E+10 0.11371E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  cl   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.635426234E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969712E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16059E+03 0.28414E+02
   Friction velocity        uet   :  0.30916E-01 0.62589E+01
   Friction velocity        uk    :  0.29621E-01 0.69096E+01
   Dimensionless distance   yplus :  0.35860E-03 0.41707E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16719
   Nb of faces within the viscous sub-layer     :       8959
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
----------------------------------------------------------------------------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.490236683E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19118E+03 0.25865E+02
   Friction velocity        uet   :  0.36962E-01 0.72233E+01
   Friction velocity        uk    :  0.40499E-01 0.69062E+01
   Dimensionless distance   yplus :  0.35706E-03 0.38761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16653
   Nb of faces within the viscous sub-layer     :       8934
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10458E+02     118   0.19330E+00   0.10662E+04 0.80474E+03 
c  Velocity[X]                                      0.31737E+03 
c  Velocity[Y]                                      0.31266E+03 
c  Velocity[Z]                                      0.43618E+03 
c  Pressure     0.17650E+00     664   0.65056E-02   0.33103E+00 0.16425E+04 
c  k            0.11633E+01      68   0.71025E-02   0.58675E+01 0.13371E+04 
c  epsilon      0.25048E+05      48   0.53228E-02   0.77996E+10 0.11371E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00027642                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.532          45.868          2.7921         0.30809
v  Velocity[Y]            -38.385          36.938          1.0457         0.71392
v  Velocity[Z]            -64.159          77.236         -1.3734      -0.0018849
v  ǁVelocityǁ           0.0010343           78.94          8.1945          6.6393
v  Pressure           -7.6467e+05      4.4719e+05      2.3853e+05      2.1358e+05
v  k                   9.8646e-06        ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.635426234E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969712E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16059E+03 0.28414E+02
   Friction velocity        uet   :  0.30916E-01 0.62589E+01
   Friction velocity        uk    :  0.29621E-01 0.69096E+01
   Dimensionless distance   yplus :  0.35860E-03 0.41707E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16719
   Nb of faces within the viscous sub-layer     :       8959
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10448E+02     116   0.18943E+00   0.10370E+04 0.80344E+03 
c  Velocity[X]                                      0.28707E+03 
c  Velocity[Y]                                      0.28682E+03 
c  Velocity[Z]                                      0.46314E+03 
c  Pressure     0.17046E+00     664   0.58336E-02   0.32076E+00 0.10479E+04 
c  k            0.10908E+01      71   0.54439E-02   0.38516E+01 0.12022E+04 
c  epsilon      0.24697E+05      47   0.37917E-02   0.33107E+10 0.26534E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     --------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.794496529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96988E+02 0.25493E+02
   Friction velocity        uet   :  0.37392E-01 0.60735E+01
   Friction velocity        uk    :  0.38304E-01 0.69778E+01
   Dimensionless distance   yplus :  0.35900E-03 0.38578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16760
   Nb of faces within the viscous sub-layer     :       8937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residua   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.635426234E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969712E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16059E+03 0.28414E+02
   Friction velocity        uet   :  0.30916E-01 0.62589E+01
   Friction velocity        uk    :  0.29621E-01 0.69096E+01
   Dimensionless distance   yplus :  0.35860E-03 0.41707E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16719
   Nb of faces within the viscous sub-layer     :       8959
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10448E+02     116   0.18943E+00   0.10370E+04 0.80344E+03 
c  Velocity[X]                                      0.28707E+03 
c  Velocity[Y]                                      0.28682E+03 
c  Velocity[Z]                                      0.46314E+03 
c  Pressure     0.17046E+00     664   0.58336E-02   0.32076E+00 0.10479E+04 
c  k            0.10908E+01      71   0.54439E-02   0.38516E+01 0.12022E+04 
c  epsilon      0.24697E+05      47   0.37917E-02   0.33107E+10 0.26534E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0004965                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.675           47.57          2.7908         0.30809
v  Velocity[Y]            -36.552          39.015          1.0536         0.71341
v  Velocity[Z]            -67.584          61.171         -1.3817      -0.0016904
v  ǁVelocityǁ           0.0010362          77.422          8.2112          6.6423
v  Pressure           -7.6695e+05      4.4784e+05    ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.794496529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96988E+02 0.25493E+02
   Friction velocity        uet   :  0.37392E-01 0.60735E+01
   Friction velocity        uk    :  0.38304E-01 0.69778E+01
   Dimensionless distance   yplus :  0.35900E-03 0.38578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16760
   Nb of faces within the viscous sub-layer     :       8937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10459E+02     116   0.18987E+00   0.10041E+04 0.79291E+03 
c  Velocity[X]                                      0.30254E+03 
c  Velocity[Y]                                      0.30008E+03 
c  Velocity[Z]                                      0.40152E+03 
c  Pressure     0.18093E+00     803   0.57570E-02   0.33855E+00 0.31095E+03 
c  k            0.10555E+01      72   0.48663E-02   0.37617E+01 0.12508E+04 
c  epsilon      0.24384E+05      47   0.33733E-02   0.49263E+10 0.12701E+06 
---------------------------------------------------===============================================================


 INSTANT    0.559000000E+03   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.583082440E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27409E+03 0.24937E+02
   Friction velocity        uet   :  0.23232E-01 0.85917E+01
   Friction velocity        uk    :  0.22962E-01 0.69349E+01
   Dimensionless distance   yplus :  0.35835E-03 0.42669E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16764
   Nb of faces within the viscous sub-layer     :       8922
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.794496529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.96988E+02 0.25493E+02
   Friction velocity        uet   :  0.37392E-01 0.60735E+01
   Friction velocity        uk    :  0.38304E-01 0.69778E+01
   Dimensionless distance   yplus :  0.35900E-03 0.38578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16760
   Nb of faces within the viscous sub-layer     :       8937
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10459E+02     116   0.18987E+00   0.10041E+04 0.79291E+03 
c  Velocity[X]                                      0.30254E+03 
c  Velocity[Y]                                      0.30008E+03 
c  Velocity[Z]                                      0.40152E+03 
c  Pressure     0.18093E+00     803   0.57570E-02   0.33855E+00 0.31095E+03 
c  k            0.10555E+01      72   0.48663E-02   0.37617E+01 0.12508E+04 
c  epsilon      0.24384E+05      47   0.33733E-02   0.49263E+10 0.12701E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00030995                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -40.532          45.159          2.7898         0.30763
v  Velocity[Y]            -38.742          37.376          1.0638         0.71449
v  Velocity[Z]            -67.126          61.098         -1.3904       -0.002174
v  ǁVelocityǁ            0.001036          77.204  ===============================================================


 INSTANT    0.559000000E+03   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.583082440E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27409E+03 0.24937E+02
   Friction velocity        uet   :  0.23232E-01 0.85917E+01
   Friction velocity        uk    :  0.22962E-01 0.69349E+01
   Dimensionless distance   yplus :  0.35835E-03 0.42669E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16764
   Nb of faces within the viscous sub-layer     :       8922
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10472E+02     116   0.19525E+00   0.10139E+04 0.78486E+03 
c  Velocity[X]                                      0.28408E+03 
c  Velocity[Y]                                      0.29462E+03 
c  Velocity[Z]                                      0.43517E+03 
c  Pressure     0.19650E+00     626   0.53033E-02   0.37076E+00 0.69074E+03 
c  k            0.10573E+01      70   0.56456E-02   0.35394E+01 0.12148E+04 
c  epsilon      0.24551E+05 v  total_pressure     -2.7833e+05      9.4927e+05      7.3988e+05      7.1462e+05


 TIME FOR THE TIME STEP              560:        0.65383E+02

===============================================================


 INSTANT    0.561000000E+03   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.643585786E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11469E+03 0.24079E+02
   Friction velocity        uet   :  0.34149E-01 0.60685E+01
   Friction velocity        uk    :  0.58000E-01 0.69275E+01
   Dimensionless distance   yplus :  0.35710E-03 0.40839E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16750
   Nb of faces within the viscous sub-layer     :       8896
   Total number of wall faces                   :      4===============================================================


 INSTANT    0.559000000E+03   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.583082440E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969741E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27409E+03 0.24937E+02
   Friction velocity        uet   :  0.23232E-01 0.85917E+01
   Friction velocity        uk    :  0.22962E-01 0.69349E+01
   Dimensionless distance   yplus :  0.35835E-03 0.42669E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16764
   Nb of faces within the viscous sub-layer     :       8922
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10472E+02     116   0.19525E+00   0.10139E+04 0.78486E+03 
c  Velocity[X]                                      0.28408E+03 
c  Velocity[Y]                                      0.29462E+03 
c  Velocity[Z]                                      0.43517E+03 
c  Pressure     0.19650E+00     626   0.53033E-02   0.37076E+00 0.69074E+03 
c  k            0.10573E+01      70   0.56456E-02   0.35394E+01 0.12148E+04 
c  epsilon      0.24551E+05      46   0.42247E-02   0.15233E+11 0.25192E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025585                             2
a  epsilon         -3.6344                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.572          44.393          2.7889         0.30759
v  Velocity[Y]            -51.023          62.927          1.0728      v  total_pressure     -2.7833e+05      9.4927e+05      7.3988e+05      7.1462e+05


 TIME FOR THE TIME STEP              560:        0.78780E+02

===============================================================


 INSTANT    0.561000000E+03   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.643585786E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11469E+03 0.24079E+02
   Friction velocity        uet   :  0.34149E-01 0.60685E+01
   Friction velocity        uk    :  0.58000E-01 0.69275E+01
   Dimensionless distance   yplus :  0.35710E-03 0.40839E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16750
   Nb of faces within the viscous sub-layer     :       8896
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10473E+02     115   0.19200E+00   0.98816E+03 0.79534E+03 
c  Velocity[X]                                      0.28898E+03 
c  Velocity[Y]                                      0.28603E+03 
c  Velocity[Z]                       v  epsilon              0.0047326      9.4002e+06           11022           96.37
v  TurbVisc            2.9132e-11         0.55548       0.0032876        0.038114
v  total_pressure     -2.8558e+05        9.49e+05      7.3976e+05      7.1465e+05


 TIME FOR THE TIME STEP              562:        0.69787E+02

===============================================================


 INSTANT    0.563000000E+03   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.682365147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18480E+03 0.23090E+02
   Friction velocity        uet   :  0.29220E-01 0.67492E+01
   Friction velocity        uk    :  0.47648E-01 0.69582E+01
   Dimensionless distance   yplus :  0.35583E-03 0.42299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16758
   Nb of faces wiv  total_pressure     -2.7833e+05      9.4927e+05      7.3988e+05      7.1462e+05


 TIME FOR THE TIME STEP              560:        0.57190E+02

===============================================================


 INSTANT    0.561000000E+03   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.643585786E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11469E+03 0.24079E+02
   Friction velocity        uet   :  0.34149E-01 0.60685E+01
   Friction velocity        uk    :  0.58000E-01 0.69275E+01
   Dimensionless distance   yplus :  0.35710E-03 0.40839E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16750
   Nb of faces within the viscous sub-layer     :       8896
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10473E+02     115   0.19200E+00   0.98816E+03 0.79534E+03 
c  Velocity[X]                                      0.28898E+03 
c  Velocity[Y]                                      0.28603E+03 
c  Velocity[Z]                                      0.41315E+03 
c  Pressure     0.19192E+00     639   0.58036E-02   0.36104E+00 0.73995E+03 
c  k            0.10220E+01      69   0.42486E-02   0.25781E+01 0.96929E+03 
c  epsilon      0.24360E+05      47   0.41856E-02   0.18040E+10 0.19424E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020096                             2
a  epsilon         -3.4356                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  ------v  epsilon              0.0047326      9.4002e+06           11022           96.37
v  TurbVisc            2.9132e-11         0.55548       0.0032876        0.038114
v  total_pressure     -2.8558e+05        9.49e+05      7.3976e+05      7.1465e+05


 TIME FOR THE TIME STEP              562:        0.71152E+02

===============================================================


 INSTANT    0.563000000E+03   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.682365147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18480E+03 0.23090E+02
   Friction velocity        uet   :  0.29220E-01 0.67492E+01
   Friction velocity        uk    :  0.47648E-01 0.69582E+01
   Dimensionless distance   yplus :  0.35583E-03 0.42299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16758
   Nb of faces within the viscous sub-layer     :       8870
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10488E+02     114   0.19307E+00   0.11607E+04 0.83280E+03 
c  v  Pressure           -7.9042e+05      4.4882e+05      2.3925e+05      2.1441e+05
v  k                   7.4133e-06          52.097         0.13977        0.084544
v  epsilon              0.0048789      9.4206e+06           11065          97.417
v  TurbVisc            2.8646e-11         0.56834       0.0033018         0.03812
v  total_pressure     -2.9042e+05      9.4882e+05      7.3925e+05      7.1441e+05


 TIME FOR THE TIME STEP              564:        0.76686E+02

===============================================================


 INSTANT    0.565000000E+03   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.219130421E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14308E+03 0.20947E+02
   Friction velocity        uet   :  0.32658E-01 0.64202E+01
   Friction velocity        uk    :  0.56184E-01 0.69689E+01
   Dimensionless distance   yplusv  epsilon              0.0047326      9.4002e+06           11022           96.37
v  TurbVisc            2.9132e-11         0.55548       0.0032876        0.038114
v  total_pressure     -2.8558e+05        9.49e+05      7.3976e+05      7.1465e+05


 TIME FOR THE TIME STEP              562:        0.73368E+02

===============================================================


 INSTANT    0.563000000E+03   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.682365147E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18480E+03 0.23090E+02
   Friction velocity        uet   :  0.29220E-01 0.67492E+01
   Friction velocity        uk    :  0.47648E-01 0.69582E+01
   Dimensionless distance   yplus :  0.35583E-03 0.42299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16758
   Nb of faces within the viscous sub-layer     :       8870
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10488E+02     114   0.19307E+00   0.11607E+04 0.83280E+03 
c  Velocity[X]                                      0.30768E+03 
c  Velocity[Y]                                      0.33155E+03 
c  Velocity[Z]                                      0.52146E+03 
c  Pressure     0.18429E+00     614   0.80225E-02   0.34523E+00 0.57595E+03 
c  k            0.10925E+01      70   0.62522E-02   0.44947E+01 0.13949E+04 
c  epsilon      0.24695E+05      49   0.45092E-02   0.25915E+11 0.89107E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.010567                             3
a  epsilon         -7389.5                             5


  **v  Pressure           -7.9042e+05      4.4882e+05      2.3925e+05      2.1441e+05
v  k                   7.4133e-06          52.097         0.13977        0.084544
v  epsilon              0.0048789      9.4206e+06           11065          97.417
v  TurbVisc            2.8646e-11         0.56834       0.0033018         0.03812
v  total_pressure     -2.9042e+05      9.4882e+05      7.3925e+05      7.1441e+05


 TIME FOR THE TIME STEP              564:        0.64341E+02

===============================================================


 INSTANT    0.565000000E+03   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.219130421E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14308E+03 0.20947E+02
   Friction velocity        uet   :  0.32658E-01 0.64202E+01
   Friction velocity        uk    :  0.56184E-01 0.69689E+01
   Dimensionless distance   yplus :  0.35382E-03 0.40908E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16806
   Nb of faces within the viscous sub-layer     :       8853
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time rv  Velocity[Z]            -66.468          106.37         -1.4311      -0.0012965
v  ǁVelocityǁ           0.0010016           118.1          8.2974          6.6576
v  Pressure           -7.9689e+05      4.4743e+05      2.3822e+05       2.138e+05
v  k                   6.6296e-06          62.522         0.14049         0.08481
v  epsilon               0.005392      9.3626e+06           11202          98.973
v  TurbVisc            2.8493e-11         0.64184       0.0033072        0.038128
v  total_pressure     -2.9689e+05      9.4743e+05      7.3822e+05       7.138e+05


 TIME FOR THE TIME STEP              566:        0.75312E+02

===============================================================


 INSTANT    0.567000000E+03   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        -0.401599380E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27505E+03 0.1v  Pressure           -7.9042e+05      4.4882e+05      2.3925e+05      2.1441e+05
v  k                   7.4133e-06          52.097         0.13977        0.084544
v  epsilon              0.0048789      9.4206e+06           11065          97.417
v  TurbVisc            2.8646e-11         0.56834       0.0033018         0.03812
v  total_pressure     -2.9042e+05      9.4882e+05      7.3925e+05      7.1441e+05


 TIME FOR THE TIME STEP              564:        0.72941E+02

===============================================================


 INSTANT    0.565000000E+03   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.219130421E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14308E+03 0.20947E+02
   Friction velocity        uet   :  0.32658E-01 0.64202E+01
   Friction velocity        uk    :  0.56184E-01 0.69689E+01
   Dimensionless distance   yplus :  0.35382E-03 0.40908E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16806
   Nb of faces within the viscous sub-layer     :       8853
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10471E+02     116   0.19162E+00   0.97218E+03 0.78984E+03 
c  Velocity[X]                                      0.29245E+03 
c  Velocity[Y]                                      0.27347E+03 
c  Velocity[Z]                                      0.40626E+03 
c  Pressure     0.19211E+00     878   0.58016E-02   0.35927E+00 0.11006E+04 
c  k            0.11799E+01      69   0.57135E-02   0.60683E+01 0.13185E+04 
c  epsilon      0.25087E+05      50   0.49029E-02   0.69950E+10 0.48776E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  -------------v  Velocity[Z]            -66.468          106.37         -1.4311      -0.0012965
v  ǁVelocityǁ           0.0010016           118.1          8.2974          6.6576
v  Pressure           -7.9689e+05      4.4743e+05      2.3822e+05       2.138e+05
v  k                   6.6296e-06          62.522         0.14049         0.08481
v  epsilon               0.005392      9.3626e+06           11202          98.973
v  TurbVisc            2.8493e-11         0.64184       0.0033072        0.038128
v  total_pressure     -2.9689e+05      9.4743e+05      7.3822e+05       7.138e+05


 TIME FOR THE TIME STEP              566:        0.74412E+02

===============================================================


 INSTANT    0.567000000E+03   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        -0.401599380E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27505E+03 0.17942E+02
   Friction velocity        uet   :  0.37869E-01 0.86073E+01
   Friction velocity        uk    :  0.46502E-01 0.69923E+01
   Dimensionless distance   yplus :  0.35287E-03 0.39919E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16785
   Nb of faces within the viscous sub-layer     :       8824
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------v  Velocity[Y]            -38.717          43.282          1.1141          0.7137
v  Velocity[Z]            -66.926          58.449         -1.4324      -0.0017365
v  ǁVelocityǁ          0.00099078          81.118          8.3045          6.6593
v  Pressure           -7.9865e+05      4.4767e+05      2.3788e+05      2.1366e+05
v  k                   5.8557e-06          69.346         0.14085        0.085091
v  epsilon              0.0046597      9.4342e+06           11202          100.18
v  TurbVisc            2.8364e-11         0.71033       0.0033124        0.038137
v  total_pressure     -2.9865e+05      9.4767e+05      7.3788e+05      7.1366e+05


 TIME FOR THE TIME STEP              568:        0.64260E+02

===============================================================


 INSTANT    0.569000000E+03   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        -0.839778781E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Mv  Velocity[Z]            -66.468          106.37         -1.4311      -0.0012965
v  ǁVelocityǁ           0.0010016           118.1          8.2974          6.6576
v  Pressure           -7.9689e+05      4.4743e+05      2.3822e+05       2.138e+05
v  k                   6.6296e-06          62.522         0.14049         0.08481
v  epsilon               0.005392      9.3626e+06           11202          98.973
v  TurbVisc            2.8493e-11         0.64184       0.0033072        0.038128
v  total_pressure     -2.9689e+05      9.4743e+05      7.3822e+05       7.138e+05


 TIME FOR THE TIME STEP              566:        0.72240E+02

===============================================================


 INSTANT    0.567000000E+03   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        -0.401599380E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969740E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27505E+03 0.17942E+02
   Friction velocity        uet   :  0.37869E-01 0.86073E+01
   Friction velocity        uk    :  0.46502E-01 0.69923E+01
   Dimensionless distance   yplus :  0.35287E-03 0.39919E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16785
   Nb of faces within the viscous sub-layer     :       8824
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10477E+02     118   0.19078E+00   0.97342E+03 0.77749E+03 
c  Velocity[X]                                      0.27157E+03 
c  Velocity[Y]                                      0.27416E+03 
c  Velocity[Z]                                      0.42768E+03 
c  Pressure     0.18206E+00     654   0.54728E-02   0.33701E+00 0.11511E+04 
c  k            0.12781E+01      68   0.62512E-02   0.67863E+01 0.13649E+04 
c  epsilon      0.25745E+05      51   0.60620E-02   0.13278E+11 0.54114E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
    v  Velocity[Y]            -38.717          43.282          1.1141          0.7137
v  Velocity[Z]            -66.926          58.449         -1.4324      -0.0017365
v  ǁVelocityǁ          0.00099078          81.118          8.3045          6.6593
v  Pressure           -7.9865e+05      4.4767e+05      2.3788e+05      2.1366e+05
v  k                   5.8557e-06          69.346         0.14085        0.085091
v  epsilon              0.0046597      9.4342e+06           11202          100.18
v  TurbVisc            2.8364e-11         0.71033       0.0033124        0.038137
v  total_pressure     -2.9865e+05      9.4767e+05      7.3788e+05      7.1366e+05


 TIME FOR THE TIME STEP              568:        0.67070E+02

===============================================================


 INSTANT    0.569000000E+03   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        -0.839778781E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99020E+02 0.16615E+02
   Friction velocity        uet   :  0.17591E-01 0.60737E+01
   Friction velocity        uk    :  0.45804E-01 0.69438E+01
   Dimensionless distance   yplus :  0.35090E-03 0.37491E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16791
   Nb of faces within the viscous sub-layer     :       8801
   Total number of wall faces                   :      41000
---------------------------------  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.572          45.465          2.7732         0.30927
v  Velocity[Y]            -35.564          47.661          1.1214         0.71417
v  Velocity[Z]            -68.569          69.256         -1.4312      -0.0015192
v  ǁVelocityǁ          0.00098265          83.253          8.3086          6.6612
v  Pressure           -8.0545e+05      4.4752e+05       2.374e+05      2.1342e+05
v  k                   5.0649e-06          59.336         0.14094        0.085108
v  epsilon              0.0038999      9.3553e+06           11218          100.06
v  TurbVisc            2.8119e-11         0.73067       0.0033181        0.038144
v  total_pressure     -3.0545e+05      9.4752e+05       7.374e+05      7.1342e+05


 TIME FOR THE TIME STEP              570:        0.73798E+02

===============================================================


 INSTANT    0.571000000E+03   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.378072933E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Y]            -38.717          43.282          1.1141          0.7137
v  Velocity[Z]            -66.926          58.449         -1.4324      -0.0017365
v  ǁVelocityǁ          0.00099078          81.118          8.3045          6.6593
v  Pressure           -7.9865e+05      4.4767e+05      2.3788e+05      2.1366e+05
v  k                   5.8557e-06          69.346         0.14085        0.085091
v  epsilon              0.0046597      9.4342e+06           11202          100.18
v  TurbVisc            2.8364e-11         0.71033       0.0033124        0.038137
v  total_pressure     -2.9865e+05      9.4767e+05      7.3788e+05      7.1366e+05


 TIME FOR THE TIME STEP              568:        0.66861E+02

===============================================================


 INSTANT    0.569000000E+03   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        -0.839778781E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969737E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.99020E+02 0.16615E+02
   Friction velocity        uet   :  0.17591E-01 0.60737E+01
   Friction velocity        uk    :  0.45804E-01 0.69438E+01
   Dimensionless distance   yplus :  0.35090E-03 0.37491E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16791
   Nb of faces within the viscous sub-layer     :       8801
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10469E+02     116   0.18962E+00   0.97690E+03 0.78710E+03 
c  Velocity[X]                                      0.27951E+03 
c  Velocity[Y]                                      0.28236E+03 
c  Velocity[Z]                                      0.41503E+03 
c  Pressure     0.18101E+00     647   0.57281E-02   0.33670E+00 0.11323E+04 
c  k            0.13564E+01      68   0.79690E-02   0.71145E+01 0.12348E+04 
c  epsilon      0.26171E+05      49   0.75274E-02   0.82014E+10 0.39074E+05 
-------  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.572          45.465          2.7732         0.30927
v  Velocity[Y]            -35.564          47.661          1.1214         0.71417
v  Velocity[Z]            -68.569          69.256         -1.4312      -0.0015192
v  ǁVelocityǁ          0.00098265          83.253          8.3086          6.6612
v  Pressure           -8.0545e+05      4.4752e+05       2.374e+05      2.1342e+05
v  k                   5.0649e-06          59.336         0.14094        0.085108
v  epsilon              0.0038999      9.3553e+06           11218          100.06
v  TurbVisc            2.8119e-11         0.73067       0.0033181        0.038144
v  total_pressure     -3.0545e+05      9.4752e+05       7.374e+05      7.1342e+05


 TIME FOR THE TIME STEP              570:        0.68571E+02

===============================================================


 INSTANT    0.571000000E+03   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.378072933E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13694E+03 0.16281E+02
   Friction velocity        uet   :  0.25231E-01 0.60720E+01
   Friction velocity        uk    :  0.35638E-01 0.69872E+01
   Dimensionless distance   yplus :  0.34935E-03 0.35020E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16774
   Nb of faces within the
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.561          44.322          2.7693         0.30924
v  Velocity[Y]            -37.798          42.527          1.1271         0.71444
v  Velocity[Z]            -66.343          57.667          -1.428       -0.001316
v  ǁVelocityǁ          0.00072815          83.867          8.3072          6.6618
v  Pressure           -8.0896e+05      4.4721e+05      2.3681e+05        2.13e+05
v  k                   4.3718e-06          47.534         0.14111        0.084914
v  epsilon               0.003228      9.4756e+06           11258          98.434
v  TurbVisc            2.8247e-11         0.53926        0.003323        0.038144
v  total_pressure     -3.0896e+05      9.4721e+05      7.3681e+05        7.13e+05


 TIME FOR THE TIME STEP              572:        0.72621E+02

===============================================================


 INSTANT    0.573000000E+03   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         0.365521582E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           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]            -17.572          45.465          2.7732         0.30927
v  Velocity[Y]            -35.564          47.661          1.1214         0.71417
v  Velocity[Z]            -68.569          69.256         -1.4312      -0.0015192
v  ǁVelocityǁ          0.00098265          83.253          8.3086          6.6612
v  Pressure           -8.0545e+05      4.4752e+05       2.374e+05      2.1342e+05
v  k                   5.0649e-06          59.336         0.14094        0.085108
v  epsilon              0.0038999      9.3553e+06           11218          100.06
v  TurbVisc            2.8119e-11         0.73067       0.0033181        0.038144
v  total_pressure     -3.0545e+05      9.4752e+05       7.374e+05      7.1342e+05


 TIME FOR THE TIME STEP              570:        0.70420E+02

===============================================================


 INSTANT    0.571000000E+03   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.378072933E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969742E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13694E+03 0.16281E+02
   Friction velocity        uet   :  0.25231E-01 0.60720E+01
   Friction velocity        uk    :  0.35638E-01 0.69872E+01
   Dimensionless distance   yplus :  0.34935E-03 0.35020E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16774
   Nb of faces within the viscous sub-layer     :       8780
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10470E+02     117   0.18937E+00   0.99713E+03 0.78714E+03 
c  Velocity[X]                                      0.28440E+03 
c  Velocity[Y]                                      0.26899E+03 
c  Velocity[Z]                                      0.44374E+03 
c  Pressure     0.17262E+00     681   0.52369E-02   0.31822E+00 0.14636E+04 
c  k            0.11594E+01    
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.561          44.322          2.7693         0.30924
v  Velocity[Y]            -37.798          42.527          1.1271         0.71444
v  Velocity[Z]            -66.343          57.667          -1.428       -0.001316
v  ǁVelocityǁ          0.00072815          83.867          8.3072          6.6618
v  Pressure           -8.0896e+05      4.4721e+05      2.3681e+05        2.13e+05
v  k                   4.3718e-06          47.534         0.14111        0.084914
v  epsilon               0.003228      9.4756e+06           11258          98.434
v  TurbVisc            2.8247e-11         0.53926        0.003323        0.038144
v  total_pressure     -3.0896e+05      9.4721e+05      7.3681e+05        7.13e+05


 TIME FOR THE TIME STEP              572:        0.68812E+02

===============================================================


 INSTANT    0.573000000E+03   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         0.365521582E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84215E+02 0.14384E+02
   Friction velocity        uet   :  0.27751E-01 0.60750E+01
   Friction velocity        uk    :  0.27735E-01 0.69729E+01
   Dimensionless distance   yplus :  0.35256E-03 0.31368E+02
   ------------------------------------------------------
   Nb of revea  epsilon         -5787.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.183          45.116           2.765         0.31013
v  Velocity[Y]            -34.485          59.069          1.1305         0.71536
v  Velocity[Z]             -66.36          99.806         -1.4215     -0.00059432
v  ǁVelocityǁ           0.0010001          108.57          8.3048          6.6632
v  Pressure           -8.1439e+05      4.4659e+05      2.3605e+05      2.1251e+05
v  k                   3.8675e-06          58.023         0.14165        0.085209
v  epsilon              0.0026924      9.3496e+06           11258          100.04
v  TurbVisc            2.8256e-11          0.5593       0.0033346        0.038143
v  total_pressure     -3.1439e+05      9.4659e+05      7.3605e+05      7.1251e+05


 TIME FOR THE TIME STEP              574:        0.73295E+02

===============================================================


 INSTANT    0.575000000E+03   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.365721778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969718E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface        
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.561          44.322          2.7693         0.30924
v  Velocity[Y]            -37.798          42.527          1.1271         0.71444
v  Velocity[Z]            -66.343          57.667          -1.428       -0.001316
v  ǁVelocityǁ          0.00072815          83.867          8.3072          6.6618
v  Pressure           -8.0896e+05      4.4721e+05      2.3681e+05        2.13e+05
v  k                   4.3718e-06          47.534         0.14111        0.084914
v  epsilon               0.003228      9.4756e+06           11258          98.434
v  TurbVisc            2.8247e-11         0.53926        0.003323        0.038144
v  total_pressure     -3.0896e+05      9.4721e+05      7.3681e+05        7.13e+05


 TIME FOR THE TIME STEP              572:        0.73907E+02

===============================================================


 INSTANT    0.573000000E+03   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         0.365521582E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969743E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84215E+02 0.14384E+02
   Friction velocity        uet   :  0.27751E-01 0.60750E+01
   Friction velocity        uk    :  0.27735E-01 0.69729E+01
   Dimensionless distance   yplus :  0.35256E-03 0.31368E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16742
   Nb of faces within the viscous sub-layer     :       8763
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10476E+02     115   0.19044E+00   0.96041E+03 0.79388E+03 
c  Velocity[X]                                      0.28238E+03 
c  Velocity[Y]                                      0.27048E+03 
c  Velocity[Z]                                      0.40755E+03 
c  Pressure     0.17681E+00     913a  epsilon         -5787.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.183          45.116           2.765         0.31013
v  Velocity[Y]            -34.485          59.069          1.1305         0.71536
v  Velocity[Z]             -66.36          99.806         -1.4215     -0.00059432
v  ǁVelocityǁ           0.0010001          108.57          8.3048          6.6632
v  Pressure           -8.1439e+05      4.4659e+05      2.3605e+05      2.1251e+05
v  k                   3.8675e-06          58.023         0.14165        0.085209
v  epsilon              0.0026924      9.3496e+06           11258          100.04
v  TurbVisc            2.8256e-11          0.5593       0.0033346        0.038143
v  total_pressure     -3.1439e+05      9.4659e+05      7.3605e+05      7.1251e+05


 TIME FOR THE TIME STEP              574:        0.65369E+02

===============================================================


 INSTANT    0.575000000E+03   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.365721778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969718E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24355E+03 0.15298E+02
   Friction velocity        uet   :  0.19917E-01 0.79853E+01
   Friction velocity        uk    :  0.19906E-01 0.70181E+01
   D-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027568                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.155          45.971           2.761         0.31063
v  Velocity[Y]            -36.015          36.028          1.1282         0.71508
v  Velocity[Z]            -88.647          59.874         -1.4172      -0.0013353
v  ǁVelocityǁ          0.00085645          92.606          8.2983          6.6648
v  Pressure           -8.1458e+05      4.4618e+05      2.3597e+05      2.1252e+05
v  k                   3.5667e-06          62.856         0.14223        0.085555
v  epsilon              0.0022887      9.4137e+06           11233          102.32
v  TurbVisc            2.8217e-11         0.68037       0.0033598        0.038149
v  total_pressure     -3.1458e+05      9.4618e+05      7.3597e+05      7.1252e+05


 TIME FOR THE TIME STEP              576:        0.67051E+02

===============================================================


 INSTANT    0.577000000E+03   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        -0.248603507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969738E+01
Free inlet               13           0         0.000000000E+00
Convective a  epsilon         -5787.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.183          45.116           2.765         0.31013
v  Velocity[Y]            -34.485          59.069          1.1305         0.71536
v  Velocity[Z]             -66.36          99.806         -1.4215     -0.00059432
v  ǁVelocityǁ           0.0010001          108.57          8.3048          6.6632
v  Pressure           -8.1439e+05      4.4659e+05      2.3605e+05      2.1251e+05
v  k                   3.8675e-06          58.023         0.14165        0.085209
v  epsilon              0.0026924      9.3496e+06           11258          100.04
v  TurbVisc            2.8256e-11          0.5593       0.0033346        0.038143
v  total_pressure     -3.1439e+05      9.4659e+05      7.3605e+05      7.1251e+05


 TIME FOR THE TIME STEP              574:        0.60141E+02

===============================================================


 INSTANT    0.575000000E+03   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.365721778E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969718E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24355E+03 0.15298E+02
   Friction velocity        uet   :  0.19917E-01 0.79853E+01
   Friction velocity        uk    :  0.19906E-01 0.70181E+01
   Dimensionless distance   yplus :  0.35234E-03 0.34782E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16731
   Nb of faces within the viscous sub-layer     :       8751
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10492E+02     115   0.19002E+00   0.11210E+04 0.83347E+03 
c  Velocity[X]                                      0.29480E+03 
c  Velocity[Y]                       -  -------  --------------  --------------  ------------  ------------
a  k            -0.0027568                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.155          45.971           2.761         0.31063
v  Velocity[Y]            -36.015          36.028          1.1282         0.71508
v  Velocity[Z]            -88.647          59.874         -1.4172      -0.0013353
v  ǁVelocityǁ          0.00085645          92.606          8.2983          6.6648
v  Pressure           -8.1458e+05      4.4618e+05      2.3597e+05      2.1252e+05
v  k                   3.5667e-06          62.856         0.14223        0.085555
v  epsilon              0.0022887      9.4137e+06           11233          102.32
v  TurbVisc            2.8217e-11         0.68037       0.0033598        0.038149
v  total_pressure     -3.1458e+05      9.4618e+05      7.3597e+05      7.1252e+05


 TIME FOR THE TIME STEP              576:        0.64907E+02

===============================================================


 INSTANT    0.577000000E+03   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        -0.248603507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23751E+03 0.17447E+02
   Friction velocity        uet   :  0.20838E-01 0.760
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0093665                             3
a  epsilon         -5729.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.678          45.321          2.7572         0.31012
v  Velocity[Y]            -36.299          36.602          1.1192         0.71625
v  Velocity[Z]            -67.489          87.692          -1.414     -0.00093173
v  ǁVelocityǁ          0.00065128          93.784          8.2916          6.6669
v  Pressure           -8.1572e+05      4.4657e+05      2.3612e+05      2.1261e+05
v  k                   3.4284e-06          56.513         0.14281        0.085763
v  epsilon              0.0020002      9.4381e+06           11221          103.05
v  TurbVisc            2.8597e-11         0.64493       0.0033896        0.038153
v  total_pressure     -3.1572e+05      9.4657e+05      7.3612e+05      7.1261e+05


 TIME FOR THE TIME STEP              578:        0.67164E+02

===============================================================


 INSTANT    0.579000000E+03   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        -0.458353144E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027568                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.155          45.971           2.761         0.31063
v  Velocity[Y]            -36.015          36.028          1.1282         0.71508
v  Velocity[Z]            -88.647          59.874         -1.4172      -0.0013353
v  ǁVelocityǁ          0.00085645          92.606          8.2983          6.6648
v  Pressure           -8.1458e+05      4.4618e+05      2.3597e+05      2.1252e+05
v  k                   3.5667e-06          62.856         0.14223        0.085555
v  epsilon              0.0022887      9.4137e+06           11233          102.32
v  TurbVisc            2.8217e-11         0.68037       0.0033598        0.038149
v  total_pressure     -3.1458e+05      9.4618e+05      7.3597e+05      7.1252e+05


 TIME FOR THE TIME STEP              576:        0.63276E+02

===============================================================


 INSTANT    0.577000000E+03   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        -0.248603507E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23751E+03 0.17447E+02
   Friction velocity        uet   :  0.20838E-01 0.76039E+01
   Friction velocity        uk    :  0.24029E-01 0.69526E+01
   Dimensionless distance   yplus :  0.35076E-03 0.37813E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16752
   Nb of faces within the viscous sub-layer     :       8735
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10486E+02     116   0.19018E+00   0.11297E+04 0.83869E+03 
c  Velocity[X]                
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0093665                             3
a  epsilon         -5729.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.678          45.321          2.7572         0.31012
v  Velocity[Y]            -36.299          36.602          1.1192         0.71625
v  Velocity[Z]            -67.489          87.692          -1.414     -0.00093173
v  ǁVelocityǁ          0.00065128          93.784          8.2916          6.6669
v  Pressure           -8.1572e+05      4.4657e+05      2.3612e+05      2.1261e+05
v  k                   3.4284e-06          56.513         0.14281        0.085763
v  epsilon              0.0020002      9.4381e+06           11221          103.05
v  TurbVisc            2.8597e-11         0.64493       0.0033896        0.038153
v  total_pressure     -3.1572e+05      9.4657e+05      7.3612e+05      7.1261e+05


 TIME FOR THE TIME STEP              578:        0.63393E+02

===============================================================


 INSTANT    0.579000000E+03   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        -0.458353144E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
--------------------------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017102                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -28.657          47.223           2.756         0.31001
v  Velocity[Y]            -34.686          43.028          1.1056         0.71637
v  Velocity[Z]            -71.783          57.549         -1.4116      -0.0015583
v  ǁVelocityǁ          0.00031772          85.282           8.282          6.6698
v  Pressure           -8.1553e+05      4.4585e+05      2.3555e+05      2.1214e+05
v  k                   3.1526e-06          50.691         0.14341          0.0859
v  epsilon              0.0018033      9.3412e+06           11223          103.04
v  TurbVisc            2.8819e-11         0.66984       0.0034268        0.038157
v  total_pressure     -3.1553e+05      9.4585e+05      7.3555e+05      7.1214e+05


 TIME FOR THE TIME STEP              580:        0.84640E+02

===============================================================


 INSTANT    0.581000000E+03   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.974280771E-17
Rough wall                6           0         0.000000000E+00
Sym
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0093665                             3
a  epsilon         -5729.6                             5


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.678          45.321          2.7572         0.31012
v  Velocity[Y]            -36.299          36.602          1.1192         0.71625
v  Velocity[Z]            -67.489          87.692          -1.414     -0.00093173
v  ǁVelocityǁ          0.00065128          93.784          8.2916          6.6669
v  Pressure           -8.1572e+05      4.4657e+05      2.3612e+05      2.1261e+05
v  k                   3.4284e-06          56.513         0.14281        0.085763
v  epsilon              0.0020002      9.4381e+06           11221          103.05
v  TurbVisc            2.8597e-11         0.64493       0.0033896        0.038153
v  total_pressure     -3.1572e+05      9.4657e+05      7.3612e+05      7.1261e+05


 TIME FOR THE TIME STEP              578:        0.73883E+02

===============================================================


 INSTANT    0.579000000E+03   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        -0.458353144E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969738E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20003E+03 0.18249E+02
   Friction velocity        uet   :  0.18325E-01 0.70559E+01
   Friction velocity        uk    :  0.18322E-01 0.70005E+01
   Dimensionless distance   yplus :  0.35475E-03 0.36795E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16719
   Nb of faces within the viscous sub-layer     :       8722
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017102                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -28.657          47.223           2.756         0.31001
v  Velocity[Y]            -34.686          43.028          1.1056         0.71637
v  Velocity[Z]            -71.783          57.549         -1.4116      -0.0015583
v  ǁVelocityǁ          0.00031772          85.282           8.282          6.6698
v  Pressure           -8.1553e+05      4.4585e+05      2.3555e+05      2.1214e+05
v  k                   3.1526e-06          50.691         0.14341          0.0859
v  epsilon              0.0018033      9.3412e+06           11223          103.04
v  TurbVisc            2.8819e-11         0.66984       0.0034268        0.038157
v  total_pressure     -3.1553e+05      9.4585e+05      7.3555e+05      7.1214e+05


 TIME FOR THE TIME STEP              580:        0.82771E+02

===============================================================


 INSTANT    0.581000000E+03   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.974280771E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
     c  epsilon      0.25011E+05      50   0.53725E-02   0.56131E+10 0.23428E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00061864                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.893          46.958          2.7551         0.30964
v  Velocity[Y]            -34.971           41.38          1.0917         0.71652
v  Velocity[Z]            -73.563          110.35         -1.4064      -0.0011524
v  ǁVelocityǁ          0.00056787          119.67          8.2733          6.6727
v  Pressure           -8.1542e+05      4.4522e+05      2.3529e+05      2.1192e+05
v  k                   2.7574e-06          52.192         0.14382        0.086058
v  epsilon              0.0016831      9.3607e+06           11231          102.88
v  TurbVisc            2.9284e-11         0.60743       0.0034603        0.038163
v  total_pressure     -3.1542e+05      9.4522e+05      7.3529e+05      7.1192e+05


 TIME FOR THE TIME STEP              582:        0.64655E+02

===============================================================


 INSTANT    0.583000000E+03   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall           -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00017102                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -28.657          47.223           2.756         0.31001
v  Velocity[Y]            -34.686          43.028          1.1056         0.71637
v  Velocity[Z]            -71.783          57.549         -1.4116      -0.0015583
v  ǁVelocityǁ          0.00031772          85.282           8.282          6.6698
v  Pressure           -8.1553e+05      4.4585e+05      2.3555e+05      2.1214e+05
v  k                   3.1526e-06          50.691         0.14341          0.0859
v  epsilon              0.0018033      9.3412e+06           11223          103.04
v  TurbVisc            2.8819e-11         0.66984       0.0034268        0.038157
v  total_pressure     -3.1553e+05      9.4585e+05      7.3555e+05      7.1214e+05


 TIME FOR THE TIME STEP              580:        0.75663E+02

===============================================================


 INSTANT    0.581000000E+03   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.974280771E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969748E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.84977E+02 0.19287E+02
   Friction velocity        uet   :  0.18900E-01 0.60576E+01
   Friction velocity        uk    :  0.18894E-01 0.69966E+01
   Dimensionless distance   yplus :  0.35644E-03 0.40076E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16713
   Nb of faces within the viscous sub-layer     :       8724
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_c  epsilon      0.25011E+05      50   0.53725E-02   0.56131E+10 0.23428E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00061864                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.893          46.958          2.7551         0.30964
v  Velocity[Y]            -34.971           41.38          1.0917         0.71652
v  Velocity[Z]            -73.563          110.35         -1.4064      -0.0011524
v  ǁVelocityǁ          0.00056787          119.67          8.2733          6.6727
v  Pressure           -8.1542e+05      4.4522e+05      2.3529e+05      2.1192e+05
v  k                   2.7574e-06          52.192         0.14382        0.086058
v  epsilon              0.0016831      9.3607e+06           11231          102.88
v  TurbVisc            2.9284e-11         0.60743       0.0034603        0.038163
v  total_pressure     -3.1542e+05      9.4522e+05      7.3529e+05      7.1192e+05


 TIME FOR THE TIME STEP              582:        0.62852E+02

===============================================================


 INSTANT    0.583000000E+03   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         0.267255104E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969716E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   -----------------------------c  k            0.11005E+01      69   0.28380E-02   0.17096E+01 0.77390E+03 
c  epsilon      0.24642E+05      48   0.29152E-02   0.54970E+10 0.34639E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00055094                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.588          44.118          2.7583         0.30914
v  Velocity[Y]             -37.46          55.945          1.0751         0.71711
v  Velocity[Z]            -72.086          60.267         -1.4034      -0.0015992
v  ǁVelocityǁ          0.00023308          84.606            8.26          6.6729
v  Pressure           -8.1338e+05      4.4452e+05      2.3453e+05      2.1132e+05
v  k                    2.851e-06          48.132         0.14395        0.086223
v  epsilon              0.0016286      9.4006e+06           11175          102.47
v  TurbVisc            2.9446e-11         0.55686       0.0034913         0.03818
v  total_pressure     -3.1338e+05      9.4452e+05      7.3453e+05      7.1132e+05


 TIME FOR THE TIME STEP              584:        0.72728E+02

===============================================================


 INSTANT    0.585000000E+03   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet    c  epsilon      0.25011E+05      50   0.53725E-02   0.56131E+10 0.23428E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00061864                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.893          46.958          2.7551         0.30964
v  Velocity[Y]            -34.971           41.38          1.0917         0.71652
v  Velocity[Z]            -73.563          110.35         -1.4064      -0.0011524
v  ǁVelocityǁ          0.00056787          119.67          8.2733          6.6727
v  Pressure           -8.1542e+05      4.4522e+05      2.3529e+05      2.1192e+05
v  k                   2.7574e-06          52.192         0.14382        0.086058
v  epsilon              0.0016831      9.3607e+06           11231          102.88
v  TurbVisc            2.9284e-11         0.60743       0.0034603        0.038163
v  total_pressure     -3.1542e+05      9.4522e+05      7.3529e+05      7.1192e+05


 TIME FOR THE TIME STEP              582:        0.66051E+02

===============================================================


 INSTANT    0.583000000E+03   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         0.267255104E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969716E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28488E+03 0.21551E+02
   Friction velocity        uet   :  0.25935E-01 0.87560E+01
   Friction velocity        uk    :  0.25931E-01 0.70125E+01
   Dimensionless distance   yplus :  0.35911E-03 0.41825E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16722
   Nb of faces within the viscous sub-layer     :       8732
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
--------------------------------c  k            0.11005E+01      69   0.28380E-02   0.17096E+01 0.77390E+03 
c  epsilon      0.24642E+05      48   0.29152E-02   0.54970E+10 0.34639E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00055094                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.588          44.118          2.7583         0.30914
v  Velocity[Y]             -37.46          55.945          1.0751         0.71711
v  Velocity[Z]            -72.086          60.267         -1.4034      -0.0015992
v  ǁVelocityǁ          0.00023308          84.606            8.26          6.6729
v  Pressure           -8.1338e+05      4.4452e+05      2.3453e+05      2.1132e+05
v  k                    2.851e-06          48.132         0.14395        0.086223
v  epsilon              0.0016286      9.4006e+06           11175          102.47
v  TurbVisc            2.9446e-11         0.55686       0.0034913         0.03818
v  total_pressure     -3.1338e+05      9.4452e+05      7.3453e+05      7.1132e+05


 TIME FOR THE TIME STEP              584:        0.77549E+02

===============================================================


 INSTANT    0.585000000E+03   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.298590925E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969708E+01
Free inlet               13           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  Pressure     0.18174E+00     664   0.45619E-02   0.33329E+00 0.13972E+04 
c  k            0.10372E+01      69   0.36820E-02   0.18104E+01 0.80720E+03 
c  epsilon      0.24207E+05      49   0.41335E-02   0.66253E+10 0.33577E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016527                             2
a  epsilon         -0.1146                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -31.165          44.036          2.7673         0.30855
v  Velocity[Y]            -37.233          34.928          1.0572         0.71692
v  Velocity[Z]            -73.005          78.777         -1.4006       -0.001358
v  ǁVelocityǁ          0.00044548          84.711          8.2499          6.6727
v  Pressure           -8.1247e+05      4.4416e+05      2.3431e+05      2.1114e+05
v  k                   2.8409e-06          45.736         0.14376        0.086282
v  epsilon              0.0016224      9.3695e+06           11140           101.5
v  TurbVisc            2.9226e-11         0.53442       0.0035122        0.038196
v  total_pressure     -3.1247e+05      9.4416e+05      7.3431e+05      7.1114e+05


 TIME FOR THE TIME STEP              586:        0.75056E+02

===============================================================


 INSTANT    0.587000000E+03   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary tc  k            0.11005E+01      69   0.28380E-02   0.17096E+01 0.77390E+03 
c  epsilon      0.24642E+05      48   0.29152E-02   0.54970E+10 0.34639E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00055094                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.588          44.118          2.7583         0.30914
v  Velocity[Y]             -37.46          55.945          1.0751         0.71711
v  Velocity[Z]            -72.086          60.267         -1.4034      -0.0015992
v  ǁVelocityǁ          0.00023308          84.606            8.26          6.6729
v  Pressure           -8.1338e+05      4.4452e+05      2.3453e+05      2.1132e+05
v  k                    2.851e-06          48.132         0.14395        0.086223
v  epsilon              0.0016286      9.4006e+06           11175          102.47
v  TurbVisc            2.9446e-11         0.55686       0.0034913         0.03818
v  total_pressure     -3.1338e+05      9.4452e+05      7.3453e+05      7.1132e+05


 TIME FOR THE TIME STEP              584:        0.66776E+02

===============================================================


 INSTANT    0.585000000E+03   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.298590925E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969708E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11502E+03 0.19193E+02
   Friction velocity        uet   :  0.97427E-02 0.61612E+01
   Friction velocity        uk    :  0.97413E-02 0.69583E+01
   Dimensionless distance   yplus :  0.35902E-03 0.39888E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16730
   Nb of faces within the viscous sub-layer     :       8733
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON c  Pressure     0.18174E+00     664   0.45619E-02   0.33329E+00 0.13972E+04 
c  k            0.10372E+01      69   0.36820E-02   0.18104E+01 0.80720E+03 
c  epsilon      0.24207E+05      49   0.41335E-02   0.66253E+10 0.33577E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016527                             2
a  epsilon         -0.1146                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -31.165          44.036          2.7673         0.30855
v  Velocity[Y]            -37.233          34.928          1.0572         0.71692
v  Velocity[Z]            -73.005          78.777         -1.4006       -0.001358
v  ǁVelocityǁ          0.00044548          84.711          8.2499          6.6727
v  Pressure           -8.1247e+05      4.4416e+05      2.3431e+05      2.1114e+05
v  k                   2.8409e-06          45.736         0.14376        0.086282
v  epsilon              0.0016224      9.3695e+06           11140           101.5
v  TurbVisc            2.9226e-11         0.53442       0.0035122        0.038196
v  total_pressure     -3.1247e+05      9.4416e+05      7.3431e+05      7.1114e+05


 TIME FOR THE TIME STEP              586:        0.64531E+02

===============================================================


 INSTANT    0.587000000E+03   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.245908625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+0c  Velocity[Y]                                      0.29736E+03 
c  Velocity[Z]                                      0.32450E+03 
c  Pressure     0.18087E+00     569   0.45424E-02   0.33150E+00 0.61865E+03 
c  k            0.10318E+01      69   0.46161E-02   0.42714E+01 0.10796E+04 
c  epsilon      0.24177E+05      49   0.36535E-02   0.89583E+10 0.28100E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013905                             2
a  epsilon          -399.9                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -36.394          44.386          2.7793         0.30845
v  Velocity[Y]            -36.388          34.974          1.0408         0.71719
v  Velocity[Z]            -72.702          58.885         -1.3989      -0.0013677
v  ǁVelocityǁ           0.0010095          85.261          8.2435          6.6732
v  Pressure           -8.1251e+05      4.4416e+05      2.3436e+05      2.1111e+05
v  k                   2.8738e-06          48.082         0.14371        0.086454
v  epsilon              0.0016444      9.3638e+06           11158          101.13
v  TurbVisc            2.8978e-11         0.53178       0.0035232        0.038214
v  total_pressure     -3.1251e+05      9.4416e+05      7.3436e+05      7.1111e+05


 TIME FOR THE TIME STEP              588:        0.63318E+02

===============================================================


 INSTANT    0.589000000E+03   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW Ic  Pressure     0.18174E+00     664   0.45619E-02   0.33329E+00 0.13972E+04 
c  k            0.10372E+01      69   0.36820E-02   0.18104E+01 0.80720E+03 
c  epsilon      0.24207E+05      49   0.41335E-02   0.66253E+10 0.33577E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016527                             2
a  epsilon         -0.1146                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -31.165          44.036          2.7673         0.30855
v  Velocity[Y]            -37.233          34.928          1.0572         0.71692
v  Velocity[Z]            -73.005          78.777         -1.4006       -0.001358
v  ǁVelocityǁ          0.00044548          84.711          8.2499          6.6727
v  Pressure           -8.1247e+05      4.4416e+05      2.3431e+05      2.1114e+05
v  k                   2.8409e-06          45.736         0.14376        0.086282
v  epsilon              0.0016224      9.3695e+06           11140           101.5
v  TurbVisc            2.9226e-11         0.53442       0.0035122        0.038196
v  total_pressure     -3.1247e+05      9.4416e+05      7.3431e+05      7.1114e+05


 TIME FOR THE TIME STEP              586:        0.70748E+02

===============================================================


 INSTANT    0.587000000E+03   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.245908625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16838E+03 0.17265E+02
   Friction velocity        uet   :  0.22550E-01 0.64035E+01
   Friction velocity        uk    :  0.22544E-01 0.69785E+01
   Dimensionless distance   yplus :  0.35756E-03 0.35682E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16730
   Nb of faces within the viscous sub-layer     :       8727
   Total number c  Velocity[Y]                                      0.29736E+03 
c  Velocity[Z]                                      0.32450E+03 
c  Pressure     0.18087E+00     569   0.45424E-02   0.33150E+00 0.61865E+03 
c  k            0.10318E+01      69   0.46161E-02   0.42714E+01 0.10796E+04 
c  epsilon      0.24177E+05      49   0.36535E-02   0.89583E+10 0.28100E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013905                             2
a  epsilon          -399.9                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -36.394          44.386          2.7793         0.30845
v  Velocity[Y]            -36.388          34.974          1.0408         0.71719
v  Velocity[Z]            -72.702          58.885         -1.3989      -0.0013677
v  ǁVelocityǁ           0.0010095          85.261          8.2435          6.6732
v  Pressure           -8.1251e+05      4.4416e+05      2.3436e+05      2.1111e+05
v  k                   2.8738e-06          48.082         0.14371        0.086454
v  epsilon              0.0016444      9.3638e+06           11158          101.13
v  TurbVisc            2.8978e-11         0.53178       0.0035232        0.038214
v  total_pressure     -3.1251e+05      9.4416e+05      7.3436e+05      7.1111e+05


 TIME FOR THE TIME STEP              588:        0.65421E+02

===============================================================


 INSTANT    0.589000000E+03   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        -0.808355800E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969713E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15   c  Velocity     0.10473E+02     117   0.19145E+00   0.89879E+03 0.76857E+03 
c  Velocity[X]                                      0.27236E+03 
c  Velocity[Y]                                      0.27919E+03 
c  Velocity[Z]                                      0.34725E+03 
c  Pressure     0.19905E+00     662   0.50303E-02   0.36517E+00 0.12404E+04 
c  k            0.10797E+01      71   0.50022E-02   0.49476E+01 0.11859E+04 
c  epsilon      0.24450E+05      52   0.38287E-02   0.77522E+10 0.83724E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011414                             2
a  epsilon      -0.0084602                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.152           43.71          2.7918         0.30838
v  Velocity[Y]            -36.299          35.938          1.0267         0.71769
v  Velocity[Z]            -79.305          100.26         -1.3963     -0.00091928
v  ǁVelocityǁ           0.0010078          106.52          8.2417          6.6745
v  Pressure           -8.2558e+05      4.4351e+05      2.3414e+05      2.1095e+05
v  k                   2.9588e-06          54.191         0.14391        0.086707
v  epsilon              0.0016989      9.3546e+06           11193          101.47
v  TurbVisc            2.8688e-11         0.59934       0.0035364         0.03824
v  total_pressure     -3.2558e+05      9.4351e+05      7.3414e+05      7.1095e+05


 TIME FOR THE TIME STEP              590:        0.74996E+02

===============================================================


 INSTANT    0.591000000E+03   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.234599645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24435E+03 0.20053E+02
   Friction velocity        uet   :  0.17841E-01 0.79323E+01
   Friction velocity        uk    :  0.17833E-01 0.69870E+01
   Dimensionless distance   yplus :  0.35428E-03 0.39022E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16745
   Nb of faces within the viscous sub-layer     :       8737
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10483E+02     117   0.19319E+00   0.13076E+04 0.89399E+03 
c  Velocity[X]                                      0.31952E+03 
c  Velocity[Y]                                      0.35330E+03 
c  Velocity[Z]                                      0.63479E+03 
c  Pressure     0.18354E+00     675   0.51477E-02   0.33741E+00 0.29207E+03 
c  k            0.11090E+01      70   0.58081E-02   0.69378E+01 0.15311E+04 
c  epsilon      0.24622E+05      51   0.49072E-02   0.27148E+11 0.88990E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016122                             2
a  epsilon       -0.054701                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -17.825          51.636          2.7984         0.30806
v  Velocity[Y]            -37.703          35.859          1.0214         0.71701
v  Velocity[Z]            -89.494       c  Velocity     0.10473E+02     117   0.19145E+00   0.89879E+03 0.76857E+03 
c  Velocity[X]                                      0.27236E+03 
c  Velocity[Y]                                      0.27919E+03 
c  Velocity[Z]                                      0.34725E+03 
c  Pressure     0.19905E+00     662   0.50303E-02   0.36517E+00 0.12404E+04 
c  k            0.10797E+01      71   0.50022E-02   0.49476E+01 0.11859E+04 
c  epsilon      0.24450E+05      52   0.38287E-02   0.77522E+10 0.83724E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011414                             2
a  epsilon      -0.0084602                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.152           43.71          2.7918         0.30838
v  Velocity[Y]            -36.299          35.938          1.0267         0.71769
v  Velocity[Z]            -79.305          100.26         -1.3963     -0.00091928
v  ǁVelocityǁ           0.0010078          106.52          8.2417          6.6745
v  Pressure           -8.2558e+05      4.4351e+05      2.3414e+05      2.1095e+05
v  k                   2.9588e-06          54.191         0.14391        0.086707
v  epsilon              0.0016989      9.3546e+06           11193          101.47
v  TurbVisc            2.8688e-11         0.59934       0.0035364         0.03824
v  total_pressure     -3.2558e+05      9.4351e+05      7.3414e+05      7.1095e+05


 TIME FOR THE TIME STEP              590:        0.69069E+02

===============================================================


 INSTANT    0.591000000E+03   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.234599645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10465E+02     116   0.19122E+00   0.11620E+04 0.84839E+03 
c  Velocity[X]                                      0.32811E+03 
c  Velocity[Y]                                      0.28694E+03 
c  Velocity[Z]                                      0.54698E+03 
c  Pressure     0.19034E+00     882   0.71011E-02   0.34992E+00 0.13942E+04 
c  k            0.11625E+01      72   0.83757E-02   0.12635E+02 0.18193E+04 
c  epsilon      0.24918E+05      52   0.66638E-02   0.20582E+11 0.26162E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0012353                             2
a  epsilon       -0.010286                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.266          45.167          2.8039         0.30731
v  Velocity[Y]            -37.982          35.584          1.0191         0.71711
v  Velocity[Z]            -71.809          88.355         -1.3979      -0.0013417
v  ǁVelocityǁ           0.0010032          92.249          8.2435          6.6743
v  Pressure           -8.3457e+05      4.4347e+05      2.3452e+05      2.1119e+05
v  k                   3.1232e-06           53.69         0.14446          0.0871
v  epsilon              0.0017994      9.3249e+06           11301           102.5
v  TurbVisc            2.8495e-11         0.59594       0.0035519         0.03827
v  total_pressure     -3.3457e+05      9.4347e+05  c  Velocity     0.10473E+02     117   0.19145E+00   0.89879E+03 0.76857E+03 
c  Velocity[X]                                      0.27236E+03 
c  Velocity[Y]                                      0.27919E+03 
c  Velocity[Z]                                      0.34725E+03 
c  Pressure     0.19905E+00     662   0.50303E-02   0.36517E+00 0.12404E+04 
c  k            0.10797E+01      71   0.50022E-02   0.49476E+01 0.11859E+04 
c  epsilon      0.24450E+05      52   0.38287E-02   0.77522E+10 0.83724E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011414                             2
a  epsilon      -0.0084602                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.152           43.71          2.7918         0.30838
v  Velocity[Y]            -36.299          35.938          1.0267         0.71769
v  Velocity[Z]            -79.305          100.26         -1.3963     -0.00091928
v  ǁVelocityǁ           0.0010078          106.52          8.2417          6.6745
v  Pressure           -8.2558e+05      4.4351e+05      2.3414e+05      2.1095e+05
v  k                   2.9588e-06          54.191         0.14391        0.086707
v  epsilon              0.0016989      9.3546e+06           11193          101.47
v  TurbVisc            2.8688e-11         0.59934       0.0035364         0.03824
v  total_pressure     -3.2558e+05      9.4351e+05      7.3414e+05      7.1095e+05


 TIME FOR THE TIME STEP              590:        0.64673E+02

===============================================================


 INSTANT    0.591000000E+03   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000         0.234599645E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969715E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24435E+03 0.20053E+02
   Friction velocity        uet   :  0.17841E-01 0.79323E+01
   Friction velocity        uk    :  0.17833E-01 0.69870E+01
   Di   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10465E+02     116   0.19122E+00   0.11620E+04 0.84839E+03 
c  Velocity[X]                                      0.32811E+03 
c  Velocity[Y]                                      0.28694E+03 
c  Velocity[Z]                                      0.54698E+03 
c  Pressure     0.19034E+00     882   0.71011E-02   0.34992E+00 0.13942E+04 
c  k            0.11625E+01      72   0.83757E-02   0.12635E+02 0.18193E+04 
c  epsilon      0.24918E+05      52   0.66638E-02   0.20582E+11 0.26162E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0012353                             2
a  epsilon       -0.010286                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.266          45.167          2.8039         0.30731
v  Velocity[Y]            -37.982          35.584          1.0191         0.71711
v  Velocity[Z]            -71.809          88.355         -1.3979      -0.0013417
v  ǁVelocityǁ           0.0010032          92.249          8.2435          6.6743
v  Pressure           -8.3457e+05      4.4347e+05      2.3452e+05      2.1119e+05
v  k                   3.1232e-06           53.69         0.14446          0.0871
v  epsilon              0.0017994      9.3249e+06           11301           102.5
v  TurbVisc            2.8495e-11         0.59594       0.0035519         0.03827
v  total_pressure     -3.3457e+05      9.4347e+05      7.3452e+05      7.1119e+05


 TIME FOR THE TIME STEP              592:        0.79930E+02

===============================================================


 INSTANT    0.593000000E+03   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10471E+02     118   0.19519E+00   0.97931E+03 0.79030E+03 
c  Velocity[X]                                      0.30487E+03 
c  Velocity[Y]                                      0.27783E+03 
c  Velocity[Z]                                      0.39662E+03 
c  Pressure     0.17486E+00     736   0.55016E-02   0.32287E+00 0.20374E+04 
c  k            0.12436E+01      73   0.10520E-01   0.22193E+02 0.21771E+04 
c  epsilon      0.25450E+05      53   0.85947E-02   0.57190E+10 0.76117E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0014238                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.373          51.091           2.814         0.30703
v  Velocity[Y]            -35.044           36.57          1.0196         0.71683
v  Velocity[Z]            -74.832          80.789          -1.402      -0.0013585
v  ǁVelocityǁ          0.00099462          90.011          8.2512          6.6742
v  Pressure           -8.3936e+05      4.4506e+05      2.3532e+05      2.1181e+05
v  k                   3.3676e-06          54.081         0.14466         0.08747
v  epsilon              0.0019683      9.4718e+06           11265          103.47
v  TurbVisc               Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10465E+02     116   0.19122E+00   0.11620E+04 0.84839E+03 
c  Velocity[X]                                      0.32811E+03 
c  Velocity[Y]                                      0.28694E+03 
c  Velocity[Z]                                      0.54698E+03 
c  Pressure     0.19034E+00     882   0.71011E-02   0.34992E+00 0.13942E+04 
c  k            0.11625E+01      72   0.83757E-02   0.12635E+02 0.18193E+04 
c  epsilon      0.24918E+05      52   0.66638E-02   0.20582E+11 0.26162E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0012353                             2
a  epsilon       -0.010286                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.266          45.167          2.8039         0.30731
v  Velocity[Y]            -37.982          35.584          1.0191         0.71711
v  Velocity[Z]            -71.809          88.355         -1.3979      -0.0013417
v  ǁVelocityǁ           0.0010032          92.249          8.2435          6.6743
v  Pressure           -8.3457e+05      4.4347e+05      2.3452e+05      2.1119e+05
v  k                   3.1232e-06           53.69         0.14446          0.0871
v  epsilon              0.0017994      9.3249e+06           11301           102.5
v  TurbVisc            2.8495e-11         0.59594       0.0035519         0.03827
v  total_pressure     -3.3457e+05      9.4347e+05      7.3452e+05      7.1119e+05


 TIME FOR THE TIME STEP              592:        0.77046E+02

===============================================================


 INSTANT    0.593000000E+03   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.257337372E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969708E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13997E+03 0.19192E+02
   Friction velocity        uet   :  0.11910E-01 0.61034E+01
   Friction velocity        uk    :  0.15371E-01 0.69349E+01
   Dimensionless distance   yplus :  0.35330E-03 0.38096E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16718
   Nb of faces within the viscous sub-layer     :       8728
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10479E+02     117   0.19539E+00   0.11467E+04 0.83589E+03 
c  Velocity[X]                                      0.33830E+03 
c  Velocity[Y]                                      0.29311E+03 
c  Velocity[Z]                                      0.51526E+03 
c  Pressure     0.17498E+00     698   0.73581E-02   0.32537E+00 0.11328E+04 
c  k            0.12185E+01      73   0.11217E-01   0.20881E+02 0.21303E+04 
c  epsilon      0.25132E+05      53   0.86755E-02   0.18665E+11 0.23492E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023341                             2
a  epsilon       -0.011971                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.952          45.505          2.8092         0.30743
v  Velocity[Y]            -38.621          36.232          1.0185         0.71682
v  Velocity[Z]            -83.622          67.028         -1.3997        -0.00113
v  ǁVelocityǁ          0.00099833          95.104          8.2467          6.6745
v  Pressure           -8.3983e+05      4.4513e+05      2.3465e+05      2.1135e+05
v  k                   3.2517e-06          59.563          0.1445         0.08732
v  epsilon              0.0018733      9.4802e+06           11252          103.12
v  TurbVisc            2.8445e-11         0.64715       0.0035637        0.038288
v  total_pressure     -3.3983e+05      9.4513e+05      7.34------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10463E+02     117   0.19026E+00   0.10580E+04 0.80473E+03 
c  Velocity[X]                                      0.31214E+03 
c  Velocity[Y]                                      0.30912E+03 
c  Velocity[Z]                                      0.43672E+03 
c  Pressure     0.18392E+00     836   0.60921E-02   0.33841E+00 0.16707E+04 
c  k            0.11215E+01      76   0.12803E-01   0.26366E+02 0.26515E+04 
c  epsilon      0.25192E+05      54   0.87406E-02   0.53814E+10 0.82846E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018875                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -34.411          54.426          2.8239         0.30681
v  Velocity[Y]            -35.812          36.395          1.0234         0.71623
v  Velocity[Z]            -85.442          75.949          -1.407       -0.002217
v  ǁVelocityǁ          0.00097615          96.718          8.2656          6.6749
v  Pressure           -8.4137e+05      4.4591e+05      2.3596e+05      2.1237e+05
v  k                    3.681e-06          41.898         0.14492        0.087446
v  epsilon              0.0021965      9.4607e+06           11271          102.48
v  TurbVisc            2.8062e-11         0.47347       0.0036038        0.038335
v  total_pressure     -3.4137e+05      9.4591e+05      7.3596e+05      7.1237e+05


 TIME FOR THE TIME STEP              596:        0.79769E+02

===============================================================


 INSTANT    0.597000000E+03   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.775844955E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969711E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17715E+03 0.20402E+02
   Friction velocity        uet   :  0.34537E-01 0.67943E+01
   Friction velocity        uk    :  0.40093E-01 0.69980E+01
   Dimensionless distance   yplus :  0.34862E-03 0.36886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16712
   Nb of faces within the viscous sub-layer     :       8739
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10472E+02     118   0.19009E+00   0.11447E+04 0.83480E+03 
c  Velocity[X]                                      0.33552E+03 
c  Velocity[Y]                                      0.32186E+03 
c  Velocity[Z]                                      0.48732E+03 
c  Pressure     0.18232E+00     458   0.60957E-02   0.33815E+00 0.10119E+04 
c  k            0.10455E+01      78   0.12176E-01   0.18164E+02 0.23241E+04 
c  epsilon      0.24694E+05      56   0.86089E-02   0.67148E+10 0.29633E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018414                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  -----------------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10463E+02     117   0.19026E+00   0.10580E+04 0.80473E+03 
c  Velocity[X]                                      0.31214E+03 
c  Velocity[Y]                                      0.30912E+03 
c  Velocity[Z]                                      0.43672E+03 
c  Pressure     0.18392E+00     836   0.60921E-02   0.33841E+00 0.16707E+04 
c  k            0.11215E+01      76   0.12803E-01   0.26366E+02 0.26515E+04 
c  epsilon      0.25192E+05      54   0.87406E-02   0.53814E+10 0.82846E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018875                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -34.411          54.426          2.8239         0.30681
v  Velocity[Y]            -35.812          36.395          1.0234         0.71623
v  Velocity[Z]            -85.442          75.949          -1.407       -0.002217
v  ǁVelocityǁ          0.00097615          96.718          8.2656          6.6749
v  Pressure           -8.4137e+05      4.4591e+05      2.3596e+05      2.1237e+05
v  k                    3.681e-06          41.898         0.14492        0.087446
v  epsilon              0.0021965      9.4607e+06           11271          102.48
v  TurbVisc            2.8062e-11         0.47347       0.0036038        0.038335
v  total_pressure     -3.4137e+05      9.4591e+05      7.3596e+05      7.1237e+05


 TIME FOR THE TIME STEP              596:        0.70102E+02

===============================================================


 INSTANT    0.597000000E+03   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10480E+02     117   0.19094E+00   0.91193E+03 0.76755E+03 
c  Velocity[X]                                      0.27470E+03 
c  Velocity[Y]                                      0.28888E+03 
c  Velocity[Z]                                      0.34836E+03 
c  Pressure     0.18390E+00     590   0.59436E-02   0.34185E+00 0.37837E+03 
c  k            0.99798E+00      78   0.90297E-02   0.10707E+02 0.18726E+04 
c  epsilon      0.24392E+05      57   0.65696E-02   0.48307E+10 0.26165E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0019646                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.345          48.057          2.8315         0.30694
v  Velocity[Y]            -38.866           36.88          1.0303         0.71589
v  Velocity[Z]            -76.946          71.569         -1.4073      -0.0016248
v  ǁVelocityǁ          0.00097641          90.871          8.2791           6.675
v  Pressure           -8.4445e+05      4.4754e+05      2.3622e+05      2.1267e+05
v  k                   4.1306e-06          43.481         0.14483        0.087225
v  epsilon              0.0024597      9.5486e+06           11264          100.67
v  TurbVisc            2.7818e-11         0.50095       0.0036218        0.038353
v  total_pressure     -3.4445e+05      9.4754e+05      7.3622e+05      7.1267e+05


 TIME FOR THE TIME STEP              598:        0.76246E+02

===============================================================


 INSTANT    0.599000000E+03   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        -0.195649637E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969714E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11787E+03 0.27890E+02
   Friction velocity        uet   :  0.37866E-01 0.65956E+01
   Friction velocity        uk    :  0.47296E-01 0.69392E+01
   Dimensionless distance   yplus :  0.34833E-03 0.34412E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16717
   Nb of faces within the viscous sub-layer     :       8746
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10471E+02     117   0.19010E+00   0.87472E+03 0.77356E+03 
c  Velocity[X]                                      0.26947E+03 
c  Velocity[Y]                                      0.28938E+03 
c  Velocity[Z]                                      0.31587E+03 
c  Pressure     0.18114E+00     735   0.60732E-02   0.33426E+00 0.33669E+03 
c  k            0.99619E+00      78   0.50576E-02   0.50812E+01 0.14448E+04 
c  epsilon      0.24297E+05      56   0.41384E-02   0.37006E+10 0.27606E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001949                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum     Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10480E+02     117   0.19094E+00   0.91193E+03 0.76755E+03 
c  Velocity[X]                                      0.27470E+03 
c  Velocity[Y]                                      0.28888E+03 
c  Velocity[Z]                                      0.34836E+03 
c  Pressure     0.18390E+00     590   0.59436E-02   0.34185E+00 0.37837E+03 
c  k            0.99798E+00      78   0.90297E-02   0.10707E+02 0.18726E+04 
c  epsilon      0.24392E+05      57   0.65696E-02   0.48307E+10 0.26165E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0019646                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.345          48.057          2.8315         0.30694
v  Velocity[Y]            -38.866           36.88          1.0303         0.71589
v  Velocity[Z]            -76.946          71.569         -1.4073      -0.0016248
v  ǁVelocityǁ          0.00097641          90.871          8.2791           6.675
v  Pressure           -8.4445e+05      4.4754e+05      2.3622e+05      2.1267e+05
v  k                   4.1306e-06          43.481         0.14483        0.087225
v  epsilon              0.0024597      9.5486e+06           11264          100.67
v  TurbVisc            2.7818e-11         0.50095       0.0036218        0.038353
v  total_pressure     -3.4445e+05      9.4754e+05      7.3622e+05      7.1267e+05


 TIME FOR THE TIME STEP              598:        0.69999E+02

===============================================================


 INSTANT    0.599000000E+03   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Bounda   Nb of faces within the viscous sub-layer     :       8738
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        600, Physical time    0.60000E+03


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.60215E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10478E+02     116   0.19162E+00   0.88002E+03 0.76732E+03 
c  Velocity[X]                                      0.26686E+03 
c  Velocity[Y]                                      0.26727E+03 
c  Velocity[Z]                                      0.34590E+03 
c  Pressure     0.17511E+00     590   0.58438E-02   0.32351E+00 0.37920E+03 
c  k            0.96747E+00      77   0.51132E-02   0.28972E+01 0.10981E+04 
c  epsilon      0.24210E+05      55   0.42100E-02   0.26081E+10 0.30680E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018509                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.231          45.723          2.8382         0.30632
v  Velocity[Y]            -38.998          36.804           1.038         0.71573
v  Velocity[Z]             -73.05          59.234         -1.4074       -0.001715
v  ǁVelocityǁ          0.00097884          83.422          8.2956          6.6765
v  Pressure           -8.4331e+05      4.4891e+05       2.371e+05      2.1344e+05
v  k                   4.7237e-06          41.472         0.14483           0.087
v  epsilon              0.0027219      9.4568e+06           11281          99.517
v  TurbVisc            2.7988e-11         0.46076         0.00363        0.038364
v  total_pressure     -3.4331e+05      9.4891e+05       7.371e+05      7.1344e+05


 TIME FOR THE TIME STEP              600:        0.64302E+02

===============================================================


 INSTANT    0.601000000E+03   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.270969726E+01
Smooth wall               5       41000        -0.137322434E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.270969736E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11859E+03 0.35872E+02
   Friction velocity        uet   :  0.30678E-01 0.62013E+01
   Friction velocity        uk    :  0.30644E-01 0.69591E+01
   Dimensionless distance   yplus :  0.34860E-03 0.32949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16748
   Nb of faces within the viscous sub-layer     :       8723
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10632E+02     126   0.19083E+00   0.78457E+04 0.15297E+04 
c  Velocity[X]                                    Nb of faces within the viscous sub-layer     :       8738
   Total number of wall faces                   :      41000
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        600, Physical time    0.60000E+03


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.56923E-01



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10478E+02     116   0.19162E+00   0.88002E+03 0.76732E+03 
c  Velocity[X]                                      0.26686E+03 
c  Velocity[Y]                                      0.26727E+03 
c  Velocity[Z]                                      0.34590E+03 
c  Pressure     0.17511E+00     590   0.58438E-02   0.32351E+00 0.37920E+03 
c  k            0.96747E+00      77   0.51132E-02   0.28972E+01 0.10981E+04 
c  epsilon      0.24210E+05      55   0.42100E-02   0.26081E+10 0.30680E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018509                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.231          45.723          2.8382         0.30632
v  Velocity[Y]            -38.998          36.804           1.038         0.71573
v  Velocity[Z]             -73.05          59.234         -1.4074       -0.001715
v  ǁVelocConvective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21725E+03 0.22012E+02
   Friction velocity        uet   :  0.12748E-01 0.81230E+01
   Friction velocity        uk    :  0.29826E-01 0.70163E+01
   Dimensionless distance   yplus :  0.35017E-03 0.30624E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17360
   Nb of faces within the viscous sub-layer     :       8551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13130E+02     143   0.17504E+00   0.49685E+04 0.15553E+04 
c  Velocity[X]                                      0.11228E+04 
c  Velocity[Y]                                      0.15689E+04 
c  Velocity[Z]                                      0.22769E+04 
c  Pressure     0.24968E+00    1134   0.56146E-01   0.43731E+00 0.12619E+06 
c  k            0.99818E+00     107   0.12643E-01   0.22724E+02 0.30670E+04 
c  epsilon      0.24868E+05      68   0.14987E-01   0.13704E+11 0.30674E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018046                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -33.566          109.66          2.9844         0.35576
v  Velocity[Y]            -56.676          72.286          1.2131         0.82845
v  Velocity[Z]            -120.43          148.16         -1.4273      -0.0046974
v  ǁVelocityǁ          0.00098529          197.99          8.6076          7.4573
v  Pressure           -8.4702e+05      5.4891e+05      3.2453e+05      2.8399e+05
v  k                   5.6086e-06          32.549         0.14686        0.099837
v  epsilon              0.0032484      9.6976e+06           11435          104.63
v  TurbVisc            2.8042e-11         0.48463       0.0037499        0.041076
v  total_pressure     -3.4702e+05      1.0489e+06      8.2453e+05      7.8399e+05


 TIME FOR THE TIME STEP              602:        0.91552E+02

===============================================================


 INSTANT    0.603000000E+03   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.215330586E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888873E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30880E+03 0.49686E+02
   Friction velocity        uet   :  0.32325E-01 0.12158E+02
   Friction velocity        uk    :  0.32312E-01 0.71207E+01
   Dimensionless distance   yplus :  0.35005E-03 0.33274E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17391
   Nb of faces within the viscous sub-layer     :       8488
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21725E+03 0.22012E+02
   Friction velocity        uet   :  0.12748E-01 0.81230E+01
   Friction velocity        uk    :  0.29826E-01 0.70163E+01
   Dimensionless distance   yplus :  0.35017E-03 0.30624E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17360
   Nb of faces within the viscous sub-layer     :       8551
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13130E+02     143   0.17504E+00   0.49685E+04 0.15553E+04 
c  Velocity[X]                                      0.11228E+04 
c  Velocity[Y]                                      0.15689E+04 
c  Velocity[Z]                                      0.22769E+04 
c  Pressure     0.24968E+00    1134   0.56146E-01   0.43731E+00 0.12619E+06 
c  k            0.99818E+00     107   0.12643E-01   0.22724E+02 0.30670E+04 
c  epsilon      0.24868E+05      68   0.14987E-01   0.13704E+11 0.30674E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018046                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -33.566          109.66          2.9844         0.35576
v  Velocity[Y]            -56.676          72.286          1.2131         0.82845
v  Velocity[Z]            -1Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43966E+03 0.23416E+02
   Friction velocity        uet   :  0.41752E-01 0.11474E+02
   Friction velocity        uk    :  0.44718E-01 0.71426E+01
   Dimensionless distance   yplus :  0.35060E-03 0.36611E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17413
   Nb of faces within the viscous sub-layer     :       8471
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12889E+02     129   0.17831E+00   0.30712E+04 0.12924E+04 
c  Velocity[X]                                      0.74290E+03 
c  Velocity[Y]                                      0.86226E+03 
c  Velocity[Z]                                      0.14660E+04 
c  Pressure     0.24784E+00     873   0.19644E-01   0.42004E+00 0.61516E+04 
c  k            0.98300E+00      98   0.14055E-01   0.31063E+02 0.35150E+04 
c  epsilon      0.25412E+05      60   0.14634E-01   0.70505E+11 0.99374E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0019363                             2
a  epsilon        -0.53485                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.304           57.72          3.0296         0.35528
v  Velocity[Y]            -61.306          47.976          1.2198         0.82883
v  Velocity[Z]            -119.54          92.176         -1.4494     -0.00098846
v  ǁVelocityǁ          0.00099748          127.78          8.7414          7.5058
v  Pressure           -8.9338e+05      5.4206e+05      3.0984e+05      2.7473e+05
v  k                    6.462e-06          57.348         0.14852         0.10551
v  epsilon              0.0037044      1.0722e+07           11654           105.2
v  TurbVisc            2.8101e-11         0.49467       0.0038318        0.043504
v  total_pressure     -3.9338e+05      1.0421e+06      8.0984e+05      7.7473e+05


 TIME FOR THE TIME STEP              604:        0.77302E+02

===============================================================


 INSTANT    0.605000000E+03   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.111184684E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29005E+03 0.22652E+02
   Friction velocity        uet   :  0.16946E-01 0.89937E+01
   Friction velocity        uk    :  0.39244E-01 0.72582E+01
   Dimensionless distance   yplus :  0.35227E-03 0.44235E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17387
   Nb of faces within the viscous sub-layer     :       8409
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derivFree inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43966E+03 0.23416E+02
   Friction velocity        uet   :  0.41752E-01 0.11474E+02
   Friction velocity        uk    :  0.44718E-01 0.71426E+01
   Dimensionless distance   yplus :  0.35060E-03 0.36611E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17413
   Nb of faces within the viscous sub-layer     :       8471
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.12889E+02     129   0.17831E+00   0.30712E+04 0.12924E+04 
c  Velocity[X]                                      0.74290E+03 
c  Velocity[Y]                                      0.86226E+03 
c  Velocity[Z]                                      0.14660E+04 
c  Pressure     0.24784E+00     873   0.19644E-01   0.42004E+00 0.61516E+04 
c  k            0.98300E+00      98   0.14055E-01   0.31063E+02 0.35150E+04 
c  epsilon      0.25412E+05      60   0.14634E-01   0.70505E+11 0.99374E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0019363                             2
a  epsilon        -0.53485                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.304           57.72          3.029Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19502E+03 0.35410E+02
   Friction velocity        uet   :  0.34220E-01 0.74421E+01
   Friction velocity        uk    :  0.34196E-01 0.72659E+01
   Dimensionless distance   yplus :  0.35445E-03 0.35971E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17409
   Nb of faces within the viscous sub-layer     :       8407
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13140E+02     126   0.17823E+00   0.20066E+04 0.10873E+04 
c  Velocity[X]                                      0.57669E+03 
c  Velocity[Y]                                      0.59536E+03 
c  Velocity[Z]                                      0.83457E+03 
c  Pressure     0.22017E+00     906   0.10545E-01   0.36786E+00 0.13542E+04 
c  k            0.85403E+00      94   0.91985E-02   0.94495E+01 0.23094E+04 
c  epsilon      0.25342E+05      55   0.61579E-02   0.93866E+10 0.12030E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0017706                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -18.401          92.886          3.0653         0.35368
v  Velocity[Y]            -54.363          44.433          1.2153         0.82874
v  Velocity[Z]             -87.93          88.201         -1.4723       -0.001685
v  ǁVelocityǁ           0.0010259           131.9          8.8582          7.5314
v  Pressure           -8.9949e+05      5.5612e+05      3.1118e+05      2.7689e+05
v  k                   6.5907e-06          32.402         0.14933         0.10807
v  epsilon              0.0036967      1.0945e+07           11870          104.11
v  TurbVisc            2.8488e-11         0.49488       0.0038796        0.045063
v  total_pressure     -3.9949e+05      1.0561e+06      8.1118e+05      7.7689e+05


 TIME FOR THE TIME STEP              606:        0.84864E+02

===============================================================


 INSTANT    0.607000000E+03   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.817265868E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888873E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15655E+03 0.26208E+02
   Friction velocity        uet   :  0.33649E-01 0.75853E+01
   Friction velocity        uk    :  0.33628E-01 0.73679E+01
   Dimensionless distance   yplus :  0.35701E-03 0.33201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17484
   Nb of faces within the viscous sub-layer     :       8384
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------------------------------------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19502E+03 0.35410E+02
   Friction velocity        uet   :  0.34220E-01 0.74421E+01
   Friction velocity        uk    :  0.34196E-01 0.72659E+01
   Dimensionless distance   yplus :  0.35445E-03 0.35971E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17409
   Nb of faces within the viscous sub-layer     :       8407
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13140E+02     126   0.17823E+00   0.20066E+04 0.10873E+04 
c  Velocity[X]                                      0.57669E+03 
c  Velocity[Y]                                      0.59536E+03 
c  Velocity[Z]                                      0.83457E+03 
c  Pressure     0.22017E+00     906   0.10545E-01   0.36786E+00 0.13542E+04 
c  k            0.85403E+00      94   0.91985E-02   0.94495E+01 0.23094E+04 
c  epsilon      0.25342E+05      55   0.61579E-02   0.93866E+10 0.12030E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0017706                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15491E+03 0.35892E+02
   Friction velocity        uet   :  0.22765E-01 0.67752E+01
   Friction velocity        uk    :  0.22748E-01 0.73730E+01
   Dimensionless distance   yplus :  0.35998E-03 0.31216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17533
   Nb of faces within the viscous sub-layer     :       8396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13326E+02     125   0.18535E+00   0.18924E+04 0.10638E+04 
c  Velocity[X]                                      0.53035E+03 
c  Velocity[Y]                                      0.58613E+03 
c  Velocity[Z]                                      0.77589E+03 
c  Pressure     0.22118E+00     697   0.83283E-02   0.37125E+00 0.16397E+04 
c  k            0.82367E+00      90   0.91844E-02   0.84314E+01 0.22600E+04 
c  epsilon      0.25542E+05      53   0.70339E-02   0.41170E+11 0.98346E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016169                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.044          60.629           3.099         0.35262
v  Velocity[Y]            -48.249          65.234          1.2145         0.82865
v  Velocity[Z]            -77.912          79.807         -1.4871      -0.0017313
v  ǁVelocityǁ           0.0010664          102.73          8.9699          7.5525
v  Pressure           -9.1149e+05      5.6537e+05      3.1169e+05      2.7787e+05
v  k                   5.6691e-06          32.595         0.15006         0.10963
v  epsilon              0.0033052      1.1215e+07           12190          104.35
v  TurbVisc            2.9347e-11         0.49488        0.003876        0.046133
v  total_pressure     -4.1149e+05      1.0654e+06      8.1169e+05      7.7787e+05


 TIME FOR THE TIME STEP              608:        0.72845E+02

===============================================================


 INSTANT    0.609000000E+03   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         0.171189238E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888875E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14628E+03 0.27385E+02
   Friction velocity        uet   :  0.24362E-01 0.66579E+01
   Friction velocity        uk    :  0.24343E-01 0.73670E+01
   Dimensionless distance   yplus :  0.36353E-03 0.33300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17609
   Nb of faces within the viscous sub-layer     :       8350
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      ---------------------Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15491E+03 0.35892E+02
   Friction velocity        uet   :  0.22765E-01 0.67752E+01
   Friction velocity        uk    :  0.22748E-01 0.73730E+01
   Dimensionless distance   yplus :  0.35998E-03 0.31216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17533
   Nb of faces within the viscous sub-layer     :       8396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13326E+02     125   0.18535E+00   0.18924E+04 0.10638E+04 
c  Velocity[X]                                      0.53035E+03 
c  Velocity[Y]                                      0.58613E+03 
c  Velocity[Z]                                      0.77589E+03 
c  Pressure     0.22118E+00     697   0.83283E-02   0.37125E+00 0.16397E+04 
c  k            0.82367E+00      90   0.91844E-02   0.84314E+01 0.22600E+04 
c  epsilon      0.25542E+05      53   0.70339E-02   0.41170E+11 0.98346E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016169                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  -------------- Smooth wall               5       41000         0.121588350E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23163E+03 0.42194E+02
   Friction velocity        uet   :  0.21629E-01 0.80354E+01
   Friction velocity        uk    :  0.21616E-01 0.74019E+01
   Dimensionless distance   yplus :  0.36820E-03 0.38588E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17669
   Nb of faces within the viscous sub-layer     :       8313
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13472E+02     122   0.19017E+00   0.19375E+04 0.10537E+04 
c  Velocity[X]                                      0.52036E+03 
c  Velocity[Y]                                      0.57678E+03 
c  Velocity[Z]                                      0.84040E+03 
c  Pressure     0.22010E+00     858   0.81488E-02   0.36771E+00 0.23700E+04 
c  k            0.96658E+00      87   0.11626E-01   0.20817E+02 0.26391E+04 
c  epsilon      0.26950E+05      52   0.65854E-02   0.21301E+11 0.73357E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001554                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.062          55.824          3.1331         0.35341
v  Velocity[Y]            -42.628          71.208          1.2092         0.82711
v  Velocity[Z]            -72.334          77.954         -1.4852      -0.0015067
v  ǁVelocityǁ           0.0011264          98.167           9.064          7.5706
v  Pressure           -9.3305e+05       5.715e+05      3.0994e+05      2.7709e+05
v  k                   5.0047e-06          53.449          0.1517         0.11098
v  epsilon              0.0030581      1.1325e+07           12638          107.17
v  TurbVisc            3.0757e-11         0.49488       0.0038468        0.046837
v  total_pressure     -4.3305e+05      1.0715e+06      8.0994e+05      7.7709e+05


 TIME FOR THE TIME STEP              610:        0.68904E+02

===============================================================


 INSTANT    0.611000000E+03   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         0.106451939E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888873E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15445E+03 0.24167E+02
   Friction velocity        uet   :  0.39610E-01 0.69390E+01
   Friction velocity        uk    :  0.42114E-01 0.73737E+01
   Dimensionless distance   yplus :  0.37329E-03 0.42701E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17723
   Nb of faces within the viscous sub-layer     :       8293
   Total number of wall faces                   :      41000
------------------------------------------------------------Smooth wall               5       41000         0.121588350E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23163E+03 0.42194E+02
   Friction velocity        uet   :  0.21629E-01 0.80354E+01
   Friction velocity        uk    :  0.21616E-01 0.74019E+01
   Dimensionless distance   yplus :  0.36820E-03 0.38588E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17669
   Nb of faces within the viscous sub-layer     :       8313
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13472E+02     122   0.19017E+00   0.19375E+04 0.10537E+04 
c  Velocity[X]                                      0.52036E+03 
c  Velocity[Y]                                      0.57678E+03 
c  Velocity[Z]                                      0.84040E+03 
c  Pressure     0.22010E+00     858   0.81488E-02   0.36771E+00 0.23700E+04 
c  k            0.96658E+00      87   0.11626E-01   0.20817E+02 0.26391E+04 
c  epsilon      0.26950E+05      52   0.65854E-02   0.21301E+11 0.73357E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001554                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum   Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.145104397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15124E+03 0.22767E+02
   Friction velocity        uet   :  0.19822E-01 0.80295E+01
   Friction velocity        uk    :  0.19815E-01 0.74341E+01
   Dimensionless distance   yplus :  0.37755E-03 0.48548E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17771
   Nb of faces within the viscous sub-layer     :       8275
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13556E+02     123   0.18487E+00   0.17733E+04 0.10165E+04 
c  Velocity[X]                                      0.51120E+03 
c  Velocity[Y]                                      0.53342E+03 
c  Velocity[Z]                          Smooth wall               5       41000         0.121588350E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23163E+03 0.42194E+02
   Friction velocity        uet   :  0.21629E-01 0.80354E+01
   Friction velocity        uk    :  0.21616E-01 0.74019E+01
   Dimensionless distance   yplus :  0.36820E-03 0.38588E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17669
   Nb of faces within the viscous sub-layer     :       8313
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13472E+02     122   0.19017E+00   0.19375E+04 0.10537E+04 
c  Velocity[X]                                      0.52036E+03 
c  Velocity[Y]                                      0.57678E+03 
c  Velocity[Z]                                      0.84040E+03 
c  Pressure     0.22010E+00     858   0.81488E-02   0.36771E+00 0.23700E+04 
c  k            0.96658E+00      87   0.11626E-01   0.20817E+02 0.26391E+04 
c  epsilon      0.26950E+05      52   0.65854E-02   0.21301E+11 0.73357E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001554                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.062          55.824          3.1331         0.35341
v  Velocity[Y]            -42.628          71.208          1.2092         0.82711
v  Velocity[Z]            -72.334          77.954         -1.4852      -0.0015067
v  ǁVelocityǁ           0.0011264          98.167           9.064          7.5706
v  Pressure           -9.3305e+05       5.715e+05      3.0994e+05      2.7709e+05
v  k                   5.0047e-06          53.449          0.1517         0.11098
v  epsilon              0.0030581      1.1325e+07           12638          107.17
v  TurbVisc            3.0757e-11         0.49488       0.0038468        0.046837
v  total_pressure     -4.3305e+05      1.0715e+06      Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.145104397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15124E+03 0.22767E+02
   Friction velocity        uet   :  0.19822E-01 0.80295E+01
   Friction velocity        uk    :  0.19815E-01 0.74341E+01
   Dimensionless distance   yplus :  0.37755E-03 0.48548E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17771
   Nb of faces within the viscous sub-layer     :       8275
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13556E+02     123   0.18487E+00   0.17733E+04 0.10165E+04 
c  Velocity[X]                                      0.51120E+03 
c  Velocity[Y]                                      0.53342E+03 
c  Velocity[Z]                                      0.72868E+03 
c  Pressure     0.22041E+00     553   0.88240E-02   0.36497E+00 0.13177E+04 
c  k            0.12825E+01      82   0.14548E-01   0.50061E+02 0.33425E+04 
c  epsilon      0.29326E+05      54   0.90887E-02   0.71487E+11 0.19288E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013898                             2
a  epsilon


  ** Computed fields on cells
   ---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.796818021E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12700E+03 0.23127E+02
   Friction velocity        uet   :  0.21587E-01 0.99892E+01
   Friction velocity        uk    :  0.21570E-01 0.74367E+01
   Dimensionless distance   yplus :  0.38805E-03 0.41655E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17869
   Nb of faces within the viscous sub-layer     :       8258
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13652E+02     122   0.18979E+00   0.18325E+04 0.10096E+04 
c  Velocity[X]                                      0.51022E+03 
c  Velocity[Y]                           Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.145104397E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15124E+03 0.22767E+02
   Friction velocity        uet   :  0.19822E-01 0.80295E+01
   Friction velocity        uk    :  0.19815E-01 0.74341E+01
   Dimensionless distance   yplus :  0.37755E-03 0.48548E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17771
   Nb of faces within the viscous sub-layer     :       8275
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13556E+02     123   0.18487E+00   0.17733E+04 0.10165E+04 
c  Velocity[X]                                      0.51120E+03 
c  Velocity[Y]                                      0.53342E+03 
c  Velocity[Z]                                      0.72868E+03 
c  Pressure     0.22041E+00     553   0.88240E-02   0.36497E+00 0.13177E+04 
c  k            0.12825E+01      82   0.14548E-01   0.50061E+02 0.33425E+04 
c  epsilon      0.29326E+05      54   0.90887E-02   0.71487E+11 0.19288E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0013898                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.215          58.008          3.1624          0.3524
v  Velocity[Y]            -50.287          62.706          1.1989         0.82687
v  Velocity[Z]            -70.268          81.102         -1.4777      -0.0018294
v  ǁVelocityǁ           0.0011831            98.6           9.136          7.5884
v  Pressure            -9.541e+05      5.7652e+05      3.0889e+05      2.7664e+05
v  k                   4.6975e-06          60.002         0.15468         0.11253
v  epsilon              0.0030546      1.1466e+07           13235          113.71
v  TurbVisc            3.2476e-11         0.55898       0.0038357        ---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.796818021E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12700E+03 0.23127E+02
   Friction velocity        uet   :  0.21587E-01 0.99892E+01
   Friction velocity        uk    :  0.21570E-01 0.74367E+01
   Dimensionless distance   yplus :  0.38805E-03 0.41655E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17869
   Nb of faces within the viscous sub-layer     :       8258
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13652E+02     122   0.18979E+00   0.18325E+04 0.10096E+04 
c  Velocity[X]                                      0.51022E+03 
c  Velocity[Y]                                      0.51384E+03 
c  Velocity[Z]                                      0.80840E+03 
c  Pressure     0.23451E+00     694   0.82855E-02   0.38590E+00 0.19438E+04 
c  k            0.17232E+01      79   0.11075E-01   0.32537E+02 0.23123E+04 
c  epsilon      0.32559E+05      56   0.13771E-01   0.42750E+11 0.10977E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ----------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.694574896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13349E+03 0.15439E+02
   Friction velocity        uet   :  0.39485E-01 0.65761E+01
   Friction velocity        uk    :  0.42938E-01 0.74364E+01
   Dimensionless distance   yplus :  0.40143E-03 0.42152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17975
   Nb of faces within the viscous sub-layer     :       8216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13696E+02     119   0.19152E+00   0.18277E+04 0.10329E+04 
c  Velocity[X]                                      0.54123E+03 
c  Velocity[Y]         ---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.796818021E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12700E+03 0.23127E+02
   Friction velocity        uet   :  0.21587E-01 0.99892E+01
   Friction velocity        uk    :  0.21570E-01 0.74367E+01
   Dimensionless distance   yplus :  0.38805E-03 0.41655E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17869
   Nb of faces within the viscous sub-layer     :       8258
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13652E+02     122   0.18979E+00   0.18325E+04 0.10096E+04 
c  Velocity[X]                                      0.51022E+03 
c  Velocity[Y]                                      0.51384E+03 
c  Velocity[Z]                                      0.80840E+03 
c  Pressure     0.23451E+00     694   0.82855E-02   0.38590E+00 0.19438E+04 
c  k            0.17232E+01      79   0.11075E-01   0.32537E+02 0.23123E+04 
c  epsilon      0.32559E+05      56   0.13771E-01   0.42750E+11 0.10977E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011574                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.155          55.672          3.1859         0.35248
v  Velocity[Y]            -73.989          46.298          1.1891         0.82721
v  Velocity[Z]             -76.89          76.864         -1.4791      -0.0018333
v  ǁVelocityǁ           0.0012655          97.317          9.1978          7.6054
v  Pressure           -9.7591e+05      5.7856e+05      3.0769e+05      2.7595e+05
v  k                   4.7146e-06          62.714         0.15718         0.11369
v  epsilon              0.0033272      1.1507e+07Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.694574896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13349E+03 0.15439E+02
   Friction velocity        uet   :  0.39485E-01 0.65761E+01
   Friction velocity        uk    :  0.42938E-01 0.74364E+01
   Dimensionless distance   yplus :  0.40143E-03 0.42152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17975
   Nb of faces within the viscous sub-layer     :       8216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13696E+02     119   0.19152E+00   0.18277E+04 0.10329E+04 
c  Velocity[X]                                      0.54123E+03 
c  Velocity[Y]                                      0.54796E+03 
c  Velocity[Z]                                      0.73849E+03 
c  Pressure     0.22374E+00     573   0.78396E-02   0.36621E+00 0.15087E+04 
c  k            0.19823E+01      77   0.37213E-02   0.72312E+01 0.13427E+04 
c  epsilon      0.37057E+05      55   0.39547E-02   0.39195E+11 0.38655E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  ----------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.132937031E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14412E+03 0.19712E+02
   Friction velocity        uet   :  0.67667E-02 0.10348E+02
   Friction velocity        uk    :  0.50825E-01 0.74596E+01
   Dimensionless distance   yplus :  0.41821E-03 0.39981E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18051
   Nb of faces within the viscous sub-layer     :       8160
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13728E+02     119   0.19198E+00   0.18062E+04 0.97699E+03 
c  Velocity[X]              Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.694574896E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13349E+03 0.15439E+02
   Friction velocity        uet   :  0.39485E-01 0.65761E+01
   Friction velocity        uk    :  0.42938E-01 0.74364E+01
   Dimensionless distance   yplus :  0.40143E-03 0.42152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17975
   Nb of faces within the viscous sub-layer     :       8216
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13696E+02     119   0.19152E+00   0.18277E+04 0.10329E+04 
c  Velocity[X]                                      0.54123E+03 
c  Velocity[Y]                                      0.54796E+03 
c  Velocity[Z]                                      0.73849E+03 
c  Pressure     0.22374E+00     573   0.78396E-02   0.36621E+00 0.15087E+04 
c  k            0.19823E+01      77   0.37213E-02   0.72312E+01 0.13427E+04 
c  epsilon      0.37057E+05      55   0.39547E-02   0.39195E+11 0.38655E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011053                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.707          53.743          3.2008         0.35288
v  Velocity[Y]            -39.054          42.874          1.1811         0.82839
v  Velocity[Z]            -80.593          77.812         -1.4888      -0.0020113
v  ǁVelocityǁ           0.0013532          95.526          9.2554          7.6197
v  Pressure           -9.9847e+05      5.7961e+05      3.0702e+05       2.756e+05
v  k                    5.485e-06          65.521         0.15896  ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.132937031E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14412E+03 0.19712E+02
   Friction velocity        uet   :  0.67667E-02 0.10348E+02
   Friction velocity        uk    :  0.50825E-01 0.74596E+01
   Dimensionless distance   yplus :  0.41821E-03 0.39981E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18051
   Nb of faces within the viscous sub-layer     :       8160
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13728E+02     119   0.19198E+00   0.18062E+04 0.97699E+03 
c  Velocity[X]                                      0.51256E+03 
c  Velocity[Y]                                      0.45856E+03 
c  Velocity[Z]                                      0.83504E+03 
c  Pressure     0.23848E+00     731   0.99273E-02   0.38628E+00 0.16661E+04 
c  k            0.17515E+01      76   0.78840E-02   0.14700E+02 0.23225E+04 
c  epsilon      0.35858E+05      52   0.12272E-01   0.20471E+12 0.32509E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  cl   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.161260928E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13551E+03 0.21209E+02
   Friction velocity        uet   :  0.36910E-01 0.66448E+01
   Friction velocity        uk    :  0.37864E-01 0.74338E+01
   Dimensionless distance   yplus :  0.43592E-03 0.41815E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18138
   Nb of faces within the viscous sub-layer     :       8083
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
----------------------------------------------------------------------------------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.132937031E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14412E+03 0.19712E+02
   Friction velocity        uet   :  0.67667E-02 0.10348E+02
   Friction velocity        uk    :  0.50825E-01 0.74596E+01
   Dimensionless distance   yplus :  0.41821E-03 0.39981E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18051
   Nb of faces within the viscous sub-layer     :       8160
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13728E+02     119   0.19198E+00   0.18062E+04 0.97699E+03 
c  Velocity[X]                                      0.51256E+03 
c  Velocity[Y]                                      0.45856E+03 
c  Velocity[Z]                                      0.83504E+03 
c  Pressure     0.23848E+00     731   0.99273E-02   0.38628E+00 0.16661E+04 
c  k            0.17515E+01      76   0.78840E-02   0.14700E+02 0.23225E+04 
c  epsilon      0.35858E+05      52   0.12272E-01   0.20471E+12 0.32509E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0074378                             4
a  epsilon         -9255.2                             7


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.848          53.105          3.2135         0.35396
v  Velocity[Y]            -46.081          74.878          1.1739         0.82866
v  Velocity[Z]            -85.036           73.26         -1.5032       -0.001908
v  ǁVelocityǁ           0.0014032          98.688           9.308          7.6325
v  Pressure           -1.0141e+06      5.8142e+05      3.0718e+05      2.7591e+05
v  k                   6.6235e-06           55.55         0.16037         0.11422
v  epsilon              0.0047217      1.2534e+07           14848          123.83
v  TurbVisc            3.7292e-11         0.61102       0.0038271        0.047816
v  total_pressure     -5.1414e+05      1.0814e+06      8.0718e+05      7.7591e+05


 TIME FOR THE TIME STEP              618:        0.70894E+02

===============================================================


 INSTANT    0.619000000E+03   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        -0.717385689E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+03 0.21941E+02
   Friction velocity        uet   :  0.30591E-01 0.75726E+01
   Friction velocity        uk    :  0.32358E-01 0.73963E+01
   Dimensionless distance   yplus :  0.42722E-03 0.38811E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18101
   Nb of faces within the viscous sub-layer     :       8129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13740E+02     118   0. ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.284852791E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14675E+03 0.37559E+02
   Friction velocity        uet   :  0.37550E-01 0.10186E+02
   Friction velocity        uk    :  0.58592E-01 0.74553E+01
   Dimensionless distance   yplus :  0.45190E-03 0.46297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18194
   Nb of faces within the viscous sub-layer     :       8025
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residua   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.161260928E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13551E+03 0.21209E+02
   Friction velocity        uet   :  0.36910E-01 0.66448E+01
   Friction velocity        uk    :  0.37864E-01 0.74338E+01
   Dimensionless distance   yplus :  0.43592E-03 0.41815E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18138
   Nb of faces within the viscous sub-layer     :       8083
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13759E+02     117   0.19254E+00   0.16629E+04 0.97495E+03 
c  Velocity[X]                                      0.51329E+03 
c  Velocity[Y]                                      0.46449E+03 
c  Velocity[Z]                                      0.68515E+03 
c  Pressure     0.22154E+00     592   0.78466E-02   0.35706E+00 0.18562E+04 
c  k            0.16364E+01      77   0.49137E-02   0.10739E+02 0.19756E+04 
c  epsilon      0.35041E+05      51   0.79891E-02   0.13950E+12 0.79094E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0011858                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -33.109           57.16          3.2236         0.35332
v  Velocity[Y]            -38.922          58.146          1.1669          0.8287
v  Velocity[Z]            -91.107          72.947         -1.5201      -0.0020734
v  ǁVelocityǁ           0.0015994          107.36          9.3536           7.642
v  Pressure           -1.0184e+06      5.8096e+05      3.0738e+05      2.7618e+05
v  k                   5.6876e-06          53.674         0.16193         0.11456
v  epsilon               0.005545      1.1545e+07           15294          124.45
v  TurbVisc            3.1264e-11         0.53363       0.0038334        0.047881
v  total_pressure     -5.1843e+05       1.081e+06      8.0738e+05      7.7618e+05


 TIME FOR THE TIME STEP              620:        0.68192E+02

===============================================================


 INSTANT    0.621000000E+03   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         0.299725454E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11571E+03 0.22057E+02
   Friction velocity        uet   :  0.46279E-01 0.76305E+01
   Friction velocity        uk    :  0.65906E-01 0.74202E+01
   Dimensionless distance   yplus :  0.44490E-03 0.42791E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18158
   Nb of faces within the viscous sub-layer     :       8063
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13763 INSTANT    0.624000000E+03   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.154905043E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26577E+03 0.23193E+02
   Friction velocity        uet   :  0.35482E-01 0.81080E+01
   Friction velocity        uk    :  0.35187E-01 0.74737E+01
   Dimensionless distance   yplus :  0.46082E-03 0.47303E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18208
   Nb of faces within the viscous sub-layer     :       7971
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Varia ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.284852791E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14675E+03 0.37559E+02
   Friction velocity        uet   :  0.37550E-01 0.10186E+02
   Friction velocity        uk    :  0.58592E-01 0.74553E+01
   Dimensionless distance   yplus :  0.45190E-03 0.46297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18194
   Nb of faces within the viscous sub-layer     :       8025
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13795E+02     118   0.18964E+00   0.21862E+04 0.11146E+04 
c  Velocity[X]                                      0.54559E+03 
c  Velocity[Y]                                      0.67047E+03 
c  Velocity[Z]                                      0.97018E+03 
c  Pressure     0.21934E+00     749   0.68452E-02   0.35449E+00 0.31873E+04 
c  k            0.15808E+01      78   0.54148E-02   0.11736E+02 0.18745E+04 
c  epsilon      0.35034E+05      51   0.49583E-02   0.45370E+11 0.11864E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026057                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -27.695          53.848          3.2274           0.353
v  Velocity[Y]            -40.418          51.879          1.1629         0.82781
v  Velocity[Z]            -83.461          73.305         -1.5375      -0.0019128
v  ǁVelocityǁ           0.0016966          96.615          9.3915          7.6511
v  Pressure           -1.0182e+06      5.8043e+05      3.0844e+05      2.7713e+05
v  k                   6.3985e-06          64.653         0.16379         0.11484
v  epsilon               0.006111      1.1529e+07           15644          125.83
v  TurbVisc            3.3854e-11         0.51526       0.0038584        0.047911
v  total_pressure     -5.1819e+05      1.0804e+06      8.0844e+05      7.7713e+05


 TIME FOR THE TIME STEP              622:        0.74807E+02

===============================================================


 INSTANT    0.623000000E+03   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.656458336E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11354E+03 0.22222E+02
   Friction velocity        uet   :  0.40464E-01 0.68729E+01
   Friction velocity        uk    :  0.48808E-01 0.74438E+01
   Dimensionless distance   yplus :  0.45862E-03 0.46973E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18195
   Nb of faces within the viscous sub-layer     :       7992
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------===============================================================


 INSTANT    0.626000000E+03   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         0.225493749E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888876E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13106E+03 0.22541E+02
   Friction velocity        uet   :  0.40301E-01 0.74906E+01
   Friction velocity        uk    :  0.57523E-01 0.74731E+01
   Dimensionless distance   yplus :  0.46134E-03 0.49746E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18223
   Nb of faces within the viscous sub-layer     :       7945
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
----------------------- INSTANT    0.624000000E+03   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.154905043E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26577E+03 0.23193E+02
   Friction velocity        uet   :  0.35482E-01 0.81080E+01
   Friction velocity        uk    :  0.35187E-01 0.74737E+01
   Dimensionless distance   yplus :  0.46082E-03 0.47303E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18208
   Nb of faces within the viscous sub-layer     :       7971
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13817E+02     118   0.18927E+00   0.18071E+04 0.99161E+03 
c  Velocity[X]                                      0.53409E+03 
c  Velocity[Y]                                      0.51955E+03 
c  Velocity[Z]                                      0.75350E+03 
c  Pressure     0.21907E+00     860   0.73192E-02   0.35334E+00 0.51465E+03 
c  k            0.15382E+01      76   0.50677E-02   0.87546E+01 0.17373E+04 
c  epsilon      0.35300E+05      51   0.55769E-02   0.70511E+11 0.19266E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002591                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -27.781          54.001           3.226         0.35307
v  Velocity[Y]            -41.129          52.023          1.1671         0.82636
v  Velocity[Z]            -77.212          75.549         -1.5549      -0.0016793
v  ǁVelocityǁ           0.0017219           93.49          9.4242          7.6607
v  Pressure           -1.0097e+06      5.8147e+05      3.0833e+05      2.7742e+05
v  k                   6.5072e-06          67.799         0.16512         0.11502
v  epsilon              0.0066137       1.235e+07           15765          126.26
v  TurbVisc            3.8139e-11         0.53416       0.0039015        0.047927
v  total_pressure     -5.0966e+05      1.0815e+06      8.0833e+05      7.7742e+05


 TIME FOR THE TIME STEP              624:        0.69542E+02

===============================================================


 INSTANT    0.625000000E+03   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.443931372E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888865E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13506E+03 0.22994E+02
   Friction velocity        uet   :  0.13930E-01 0.65534E+01
   Friction velocity        uk    :  0.54368E-01 0.74153E+01
   Dimensionless distance   yplus :  0.46231E-03 0.48103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18211
   Nb of faces within the viscous sub-layer     :       7948
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual TIME FOR THE TIME STEP              627:        0.70802E+02

===============================================================


 INSTANT    0.628000000E+03   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.236296602E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+03 0.22577E+02
   Friction velocity        uet   :  0.38038E-01 0.69482E+01
   Friction velocity        uk    :  0.37887E-01 0.74839E+01
   Dimensionless distance   yplus :  0.45966E-03 0.53192E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18300
   Nb of faces within the viscous sub-layer     :       7930
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CO===============================================================


 INSTANT    0.626000000E+03   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         0.225493749E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888876E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13106E+03 0.22541E+02
   Friction velocity        uet   :  0.40301E-01 0.74906E+01
   Friction velocity        uk    :  0.57523E-01 0.74731E+01
   Dimensionless distance   yplus :  0.46134E-03 0.49746E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18223
   Nb of faces within the viscous sub-layer     :       7945
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13831E+02     119   0.19264E+00   0.15941E+04 0.93564E+03 
c  Velocity[X]                                      0.48603E+03 
c  Velocity[Y]                                      0.52502E+03 
c  Velocity[Z]                                      0.58304E+03 
c  Pressure     0.22803E+00     678   0.67825E-02   0.37075E+00 0.12519E+04 
c  k            0.15533E+01      74   0.42782E-02   0.66253E+01 0.13650E+04 
c  epsilon      0.35874E+05      52   0.49902E-02   0.11432E+11 0.14964E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024594                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.422          53.902          3.2209           0.353
v  Velocity[Y]            -41.281          60.935          1.1725         0.82585
v  Velocity[Z]            -83.806          78.549         -1.5791      -0.0017646
v  ǁVelocityǁ           0.0017152          97.956          9.4586          7.6679
v  Pressure           -1.0067e+06      5.8403e+05      3.1034e+05      2.7909e+05
v  k                   6.2353e-06          77.959          0.1664         0.11514
v  epsilon              0.0067234      1.1685e+07           15837          126.43
v  TurbVisc            3.8928e-11         0.56074       0.0039524         0.04794
v  total_pressure     -5.0674e+05       1.084e+06      8.1034e+05      7.7909e+05


 TIME FOR THE TIME STEP              626:        0.72587E+02

===============================================================


 INSTANT    0.627000000E+03   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.157810995E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888877E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14348E+03 0.21534E+02
   Friction velocity        uet   :  0.38136E-01 0.71051E+01
   Friction velocity        uk    :  0.38424E-01 0.74257E+01
   Dimensionless distance   yplus :  0.46089E-03 0.51586E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18273
   Nb of faces within the viscous sub-layer     :       7954
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------v  total_pressure     -5.1685e+05      1.0859e+06      8.1167e+05      7.8048e+05


 TIME FOR THE TIME STEP              629:        0.67244E+02

===============================================================


 INSTANT    0.630000000E+03   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.283161901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888876E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16834E+03 0.23435E+02
   Friction velocity        uet   :  0.43313E-01 0.67440E+01
   Friction velocity        uk    :  0.60352E-01 0.74772E+01
   Dimensionless distance   yplus :  0.45715E-03 0.48847E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18309
   Nb of faces within the viscous sub-layer     :       7972
   Total number of wall faces                   :      41000
------------------------- TIME FOR THE TIME STEP              627:        0.75185E+02

===============================================================


 INSTANT    0.628000000E+03   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.236296602E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+03 0.22577E+02
   Friction velocity        uet   :  0.38038E-01 0.69482E+01
   Friction velocity        uk    :  0.37887E-01 0.74839E+01
   Dimensionless distance   yplus :  0.45966E-03 0.53192E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18300
   Nb of faces within the viscous sub-layer     :       7930
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13879E+02     119   0.19242E+00   0.17868E+04 0.99225E+03 
c  Velocity[X]                                      0.48267E+03 
c  Velocity[Y]                                      0.57618E+03 
c  Velocity[Z]                                      0.72795E+03 
c  Pressure     0.23145E+00     625   0.72628E-02   0.37800E+00 0.11100E+04 
c  k            0.15699E+01      72   0.44189E-02   0.57031E+01 0.13851E+04 
c  epsilon      0.36210E+05      51   0.63970E-02   0.38159E+11 0.83976E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025303                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.335           55.72          3.2132         0.35388
v  Velocity[Y]            -41.049          43.006          1.1763          0.8243
v  Velocity[Z]            -79.415          74.438         -1.5981      -0.0013416
v  ǁVelocityǁ           0.0017002          98.157          9.4905          7.6742
v  Pressure           -1.0138e+06      5.8507e+05      3.1066e+05      2.7952e+05
v  k                   6.7435e-06          74.642         0.16721         0.11529
v  epsilon              0.0069192      1.1484e+07           15918          126.68
v  TurbVisc            3.8499e-11         0.57669       0.0040003        0.047955
v  total_pressure     -5.1383e+05      1.0851e+06      8.1066e+05      7.7952e+05


 TIME FOR THE TIME STEP              628:        0.67620E+02

===============================================================


 INSTANT    0.629000000E+03   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.813654045E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12388E+03 0.23142E+02
   Friction velocity        uet   :  0.34160E-01 0.67742E+01
   Friction velocity        uk    :  0.59416E-01 0.74598E+01
   Dimensionless distance   yplus :  0.45974E-03 0.50475E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18294
   Nb of faces within the viscous sub-layer     :       7958
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGEv  TurbVisc             3.766e-11         0.62183        0.004063        0.047985
v  total_pressure     -5.2137e+05      1.0866e+06      8.1196e+05      7.8079e+05


 TIME FOR THE TIME STEP              631:        0.71388E+02

===============================================================


 INSTANT    0.632000000E+03   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        -0.594620459E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18807E+03 0.20318E+02
   Friction velocity        uet   :  0.44390E-01 0.70482E+01
   Friction velocity        uk    :  0.61329E-01 0.74749E+01
   Dimensionless distance   yplus :  0.45396E-03 0.47708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18306
   Nb of faces within the viscous sub-layer     :       7984
  v  total_pressure     -5.1685e+05      1.0859e+06      8.1167e+05      7.8048e+05


 TIME FOR THE TIME STEP              629:        0.77823E+02

===============================================================


 INSTANT    0.630000000E+03   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.283161901E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888876E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16834E+03 0.23435E+02
   Friction velocity        uet   :  0.43313E-01 0.67440E+01
   Friction velocity        uk    :  0.60352E-01 0.74772E+01
   Dimensionless distance   yplus :  0.45715E-03 0.48847E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18309
   Nb of faces within the viscous sub-layer     :       7972
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13906E+02     119   0.19321E+00   0.14993E+04 0.91958E+03 
c  Velocity[X]                                      0.45375E+03 
c  Velocity[Y]                                      0.48318E+03 
c  Velocity[Z]                                      0.56238E+03 
c  Pressure     0.25180E+00     590   0.69363E-02   0.41395E+00 0.13058E+04 
c  k            0.16049E+01      72   0.34579E-02   0.38058E+01 0.11118E+04 
c  epsilon      0.36297E+05      50   0.39986E-02   0.14709E+11 0.49167E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023425                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.594          55.699          3.2068         0.35479
v  Velocity[Y]            -48.976          43.237          1.1867         0.82449
v  Velocity[Z]            -84.559           73.33         -1.6064      -0.0011334
v  ǁVelocityǁ           0.0016695          102.23          9.5204          7.6793
v  Pressure           -1.0196e+06      5.8722e+05      3.1223e+05       2.809e+05
v  k                   7.4691e-06          66.747         0.16817         0.11545
v  epsilon              0.0068495      1.1461e+07           16061          126.94
v  TurbVisc            3.8006e-11         0.61073       0.0040439        0.047975
v  total_pressure     -5.1958e+05      1.0872e+06      8.1223e+05       7.809e+05


 TIME FOR THE TIME STEP              630:        0.59740E+02

===============================================================


 INSTANT    0.631000000E+03   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        -0.321361788E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888906E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21281E+03 0.21456E+02
   Friction velocity        uet   :  0.27279E-01 0.72651E+01
   Friction velocity        uk    :  0.61559E-01 0.74528E+01
   Dimensionless distance   yplus :  0.45564E-03 0.47157E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18296
   Nb of faces within the viscous sub-layer     :       7999
   Total number of wall faces                   :      41000
-----------v  epsilon               0.006976      1.1607e+07           16103          130.28
v  TurbVisc            3.7315e-11         0.70437       0.0040992        0.048004
v  total_pressure     -5.2723e+05      1.0876e+06      8.1182e+05      7.8068e+05


 TIME FOR THE TIME STEP              633:        0.62223E+02

===============================================================


 INSTANT    0.634000000E+03   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.447653333E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12574E+03 0.23885E+02
   Friction velocity        uet   :  0.43867E-01 0.72253E+01
   Friction velocity        uk    :  0.58228E-01 0.75023E+01
   Dimensionless distance   yplus :  0.45118E-03 0.53377E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wv  TurbVisc             3.766e-11         0.62183        0.004063        0.047985
v  total_pressure     -5.2137e+05      1.0866e+06      8.1196e+05      7.8079e+05


 TIME FOR THE TIME STEP              631:        0.76135E+02

===============================================================


 INSTANT    0.632000000E+03   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        -0.594620459E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18807E+03 0.20318E+02
   Friction velocity        uet   :  0.44390E-01 0.70482E+01
   Friction velocity        uk    :  0.61329E-01 0.74749E+01
   Dimensionless distance   yplus :  0.45396E-03 0.47708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18306
   Nb of faces within the viscous sub-layer     :       7984
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13924E+02     119   0.19285E+00   0.15297E+04 0.92755E+03 
c  Velocity[X]                                      0.47099E+03 
c  Velocity[Y]                                      0.48874E+03 
c  Velocity[Z]                                      0.57002E+03 
c  Pressure     0.26287E+00     716   0.76765E-02   0.43674E+00 0.76986E+03 
c  k            0.17825E+01      73   0.64374E-02   0.10129E+02 0.13044E+04 
c  epsilon      0.37657E+05      48   0.64304E-02   0.96239E+10 0.27446E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022114                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.585          55.614          3.2017         0.35484
v  Velocity[Y]            -43.608          42.768             1.2         0.82428
v  Velocity[Z]            -80.998          118.12         -1.6057     -0.00076896
v  ǁVelocityǁ           0.0016493          132.64          9.5487          7.6831
v  Pressure           -1.0233e+06      5.8747e+05      3.1255e+05      2.8127e+05
v  k                   8.6582e-06          76.885         0.16912         0.11575
v  epsilon              0.0068666      1.1536e+07           16092           128.6
v  TurbVisc            3.7338e-11         0.66159       0.0040818        0.047995
v  total_pressure     -5.2327e+05      1.0875e+06      8.1255e+05      7.8127e+05


 TIME FOR THE TIME STEP              632:        0.69044E+02

===============================================================


 INSTANT    0.633000000E+03   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.234747440E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30708E+03 0.19329E+02
   Friction velocity        uet   :  0.37038E-01 0.95060E+01
   Friction velocity        uk    :  0.63780E-01 0.74486E+01
   Dimensionless distance   yplus :  0.45293E-03 0.50642E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18339
   Nb of faces within the viscous sub-layer     :  v  k                   9.5437e-06          85.304          0.1713          0.1165
v  epsilon              0.0072027      1.1685e+07           16141          133.66
v  TurbVisc            3.7547e-11         0.76778       0.0041375        0.048021
v  total_pressure     -5.2819e+05      1.0886e+06      8.1165e+05      7.8055e+05


 TIME FOR THE TIME STEP              635:        0.82063E+02

===============================================================


 INSTANT    0.636000000E+03   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        -0.430261852E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11103E+03 0.23218E+02
   Friction velocity        uet   :  0.35488E-01 0.67409E+01
   Friction velocity        uk    :  0.65372E-01 0.74905E+01
   Dimensionless distance   yplus :  0.45263E-03 0.50834E+02
   ---------------v  epsilon               0.006976      1.1607e+07           16103          130.28
v  TurbVisc            3.7315e-11         0.70437       0.0040992        0.048004
v  total_pressure     -5.2723e+05      1.0876e+06      8.1182e+05      7.8068e+05


 TIME FOR THE TIME STEP              633:        0.71599E+02

===============================================================


 INSTANT    0.634000000E+03   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.447653333E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12574E+03 0.23885E+02
   Friction velocity        uet   :  0.43867E-01 0.72253E+01
   Friction velocity        uk    :  0.58228E-01 0.75023E+01
   Dimensionless distance   yplus :  0.45118E-03 0.53377E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18338
   Nb of faces within the viscous sub-layer     :       7938
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13954E+02     121   0.19281E+00   0.16673E+04 0.96076E+03 
c  Velocity[X]                                      0.46709E+03 
c  Velocity[Y]                                      0.51651E+03 
c  Velocity[Z]                                      0.68369E+03 
c  Pressure     0.25926E+00     934   0.76677E-02   0.42656E+00 0.22161E+04 
c  k            0.20725E+01      72   0.50434E-02   0.13910E+02 0.14510E+04 
c  epsilon      0.40801E+05      51   0.52556E-02   0.41403E+10 0.37435E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0019276                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.321          53.569          3.1999         0.35583
v  Velocity[Y]             -41.55          54.966          1.2142         0.82383
v  Velocity[Z]            -78.593          74.097         -1.6043      -0.0006719
v  ǁVelocityǁ           0.0016481           98.13          9.5755          7.6876
v  Pressure           -1.0268e+06      5.8974e+05      3.1294e+05      2.8145e+05
v  k                   9.2993e-06          85.596         0.17061         0.11623
v  epsilon              0.0069977      1.1519e+07           16140          132.04
v  TurbVisc            2.8179e-11         0.76594       0.0041181        0.048013
v  total_pressure     -5.2675e+05      1.0897e+06      8.1294e+05      7.8145e+05


 TIME FOR THE TIME STEP              634:        0.76722E+02

===============================================================


 INSTANT    0.635000000E+03   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.313698625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888911E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14734E+03 0.21635E+02
   Friction velocity        uet   :  0.40667E-01 0.68751E+01
   Friction velocity        uk    :  0.62148E-01 0.74646E+01
   Dimensionless distance   yplus :  0.45311E-03 0.51945E+02
   ------------------------------------------------------
   Nb of reversal of the velocv  Pressure           -1.0339e+06      5.8783e+05      3.1092e+05      2.8004e+05
v  k                   8.6864e-06          73.744         0.17264         0.11688
v  epsilon              0.0073135      1.1689e+07           16215          135.42
v  TurbVisc            3.7803e-11          0.7138       0.0041764        0.048041
v  total_pressure      -5.339e+05      1.0878e+06      8.1092e+05      7.8004e+05


 TIME FOR THE TIME STEP              637:        0.82008E+02

===============================================================


 INSTANT    0.638000000E+03   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        -0.980092125E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14872E+03 0.23645E+02
   Friction velocity        uet   :  0.36995E-01 0.67528E+01
   Friction velocity        uk    :  0.63813E-01 0.74883E+v  k                   9.5437e-06          85.304          0.1713          0.1165
v  epsilon              0.0072027      1.1685e+07           16141          133.66
v  TurbVisc            3.7547e-11         0.76778       0.0041375        0.048021
v  total_pressure     -5.2819e+05      1.0886e+06      8.1165e+05      7.8055e+05


 TIME FOR THE TIME STEP              635:        0.83572E+02

===============================================================


 INSTANT    0.636000000E+03   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        -0.430261852E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11103E+03 0.23218E+02
   Friction velocity        uet   :  0.35488E-01 0.67409E+01
   Friction velocity        uk    :  0.65372E-01 0.74905E+01
   Dimensionless distance   yplus :  0.45263E-03 0.50834E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18353
   Nb of faces within the viscous sub-layer     :       7882
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13973E+02     120   0.19288E+00   0.15026E+04 0.91811E+03 
c  Velocity[X]                                      0.47790E+03 
c  Velocity[Y]                                      0.45904E+03 
c  Velocity[Z]                                      0.56569E+03 
c  Pressure     0.25570E+00     680   0.72812E-02   0.41954E+00 0.48716E+03 
c  k            0.21023E+01      72   0.49680E-02   0.20737E+02 0.16913E+04 
c  epsilon      0.41399E+05      52   0.44474E-02   0.49527E+10 0.61820E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022115                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.988          56.426          3.1991         0.35677
v  Velocity[Y]            -44.422          42.458          1.2246         0.82358
v  Velocity[Z]            -83.125          68.617         -1.6012     -0.00086182
v  ǁVelocityǁ           0.0016558          104.34          9.5952          7.6899
v  Pressure           -1.0313e+06      5.8934e+05      3.1172e+05      2.8058e+05
v  k                   9.5675e-06          79.181         0.17208         0.11669
v  epsilon              0.0072486      1.1489e+07           16189          134.69
v  TurbVisc            3.7707e-11         0.76487       0.0041581        0.048031
v  total_pressure     -5.3125e+05      1.0893e+06      8.1172e+05      7.8058e+05


 TIME FOR THE TIME STEP              636:        0.65920E+02

===============================================================


 INSTANT    0.637000000E+03   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         0.392479302E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888905E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11207E+03 0.23510E+02
   Friction velocity        uet   :  0.33858E-01 0.73178E+01
   Friction velocity        uk    :  0.49865E-01 0.74644E+01
   Dimensionless distance   yv  Velocity[Z]            -72.942          89.935         -1.6038     -0.00024693
v  ǁVelocityǁ           0.0016537          92.709          9.6126          7.6921
v  Pressure           -1.0414e+06      5.8724e+05      3.1009e+05      2.7955e+05
v  k                   3.8157e-06          72.796         0.17371         0.11722
v  epsilon              0.0066908      1.1689e+07           16266          136.67
v  TurbVisc            3.7682e-11         0.73494       0.0042088        0.048061
v  total_pressure     -5.4135e+05      1.0872e+06      8.1009e+05      7.7955e+05


 TIME FOR THE TIME STEP              639:        0.69069E+02

===============================================================


 INSTANT    0.640000000E+03   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.422152341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888901E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16698E+03 0.2v  Pressure           -1.0339e+06      5.8783e+05      3.1092e+05      2.8004e+05
v  k                   8.6864e-06          73.744         0.17264         0.11688
v  epsilon              0.0073135      1.1689e+07           16215          135.42
v  TurbVisc            3.7803e-11          0.7138       0.0041764        0.048041
v  total_pressure      -5.339e+05      1.0878e+06      8.1092e+05      7.8004e+05


 TIME FOR THE TIME STEP              637:        0.82310E+02

===============================================================


 INSTANT    0.638000000E+03   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        -0.980092125E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14872E+03 0.23645E+02
   Friction velocity        uet   :  0.36995E-01 0.67528E+01
   Friction velocity        uk    :  0.63813E-01 0.74883E+01
   Dimensionless distance   yplus :  0.45343E-03 0.45850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18375
   Nb of faces within the viscous sub-layer     :       7845
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13996E+02     119   0.19513E+00   0.17991E+04 0.97192E+03 
c  Velocity[X]                                      0.50034E+03 
c  Velocity[Y]                                      0.53652E+03 
c  Velocity[Z]                                      0.76221E+03 
c  Pressure     0.27733E+00     770   0.78012E-02   0.45269E+00 0.30632E+03 
c  k            0.20675E+01      72   0.66788E-02   0.29587E+02 0.19019E+04 
c  epsilon      0.40456E+05      52   0.54461E-02   0.16766E+11 0.42737E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020578                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.498          57.157           3.197         0.35697
v  Velocity[Y]            -43.487          46.693          1.2301         0.82365
v  Velocity[Z]            -105.67          94.316         -1.6014     -0.00014556
v  ǁVelocityǁ           0.0016569          120.39          9.6077          7.6923
v  Pressure           -1.0376e+06      5.8977e+05      3.1121e+05      2.8033e+05
v  k                   7.8814e-06          70.776         0.17324         0.11703
v  epsilon              0.0070992      1.1535e+07           16254          136.04
v  TurbVisc            3.7706e-11         0.70446       0.0041944        0.048051
v  total_pressure     -5.3761e+05      1.0898e+06      8.1121e+05      7.8033e+05


 TIME FOR THE TIME STEP              638:        0.68396E+02

===============================================================


 INSTANT    0.639000000E+03   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.261891769E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22019E+03 0.22441E+02
   Friction velocity        uet   :  0.35782E-01 0.85871E+01
   Friction velociv  Velocity[X]              -21.2          54.272          3.1972         0.35643
v  Velocity[Y]            -43.386           40.09          1.2266         0.82382
v  Velocity[Z]            -84.843          79.004         -1.6097     -0.00046001
v  ǁVelocityǁ           0.0016419          100.85          9.6205          7.6925
v  Pressure           -1.0436e+06      5.8753e+05      3.1047e+05      2.7997e+05
v  k                   6.1892e-06          79.184         0.17478         0.11773
v  epsilon               0.005961      1.1669e+07           16302          139.39
v  TurbVisc            3.5611e-11         0.92383       0.0042352        0.048085
v  total_pressure     -5.4361e+05      1.0875e+06      8.1047e+05      7.7997e+05


 TIME FOR THE TIME STEP              641:        0.72626E+02

===============================================================


 INSTANT    0.642000000E+03   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        -0.423876351E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Z]            -72.942          89.935         -1.6038     -0.00024693
v  ǁVelocityǁ           0.0016537          92.709          9.6126          7.6921
v  Pressure           -1.0414e+06      5.8724e+05      3.1009e+05      2.7955e+05
v  k                   3.8157e-06          72.796         0.17371         0.11722
v  epsilon              0.0066908      1.1689e+07           16266          136.67
v  TurbVisc            3.7682e-11         0.73494       0.0042088        0.048061
v  total_pressure     -5.4135e+05      1.0872e+06      8.1009e+05      7.7955e+05


 TIME FOR THE TIME STEP              639:        0.82840E+02

===============================================================


 INSTANT    0.640000000E+03   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.422152341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888901E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16698E+03 0.24609E+02
   Friction velocity        uet   :  0.16926E-01 0.70296E+01
   Friction velocity        uk    :  0.55893E-01 0.74910E+01
   Dimensionless distance   yplus :  0.45327E-03 0.45976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18398
   Nb of faces within the viscous sub-layer     :       7811
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13986E+02     118   0.19421E+00   0.20638E+04 0.11566E+04 
c  Velocity[X]                                      0.52721E+03 
c  Velocity[Y]                                      0.66263E+03 
c  Velocity[Z]                                      0.87392E+03 
c  Pressure     0.24821E+00     790   0.74279E-02   0.40667E+00 0.14367E+04 
c  k            0.20914E+01      74   0.80691E-02   0.35461E+02 0.19104E+04 
c  epsilon      0.40223E+05      54   0.72563E-02   0.50361E+10 0.19940E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021893                             3
a  epsilon         -53.545                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.222          58.521          3.1966         0.35627
v  Velocity[Y]            -43.267          48.613          1.2296         0.82353
v  Velocity[Z]             -96.01          83.105         -1.6063     -6.7362e-05
v  ǁVelocityǁ           0.0016513          112.54          9.6162          7.6923
v  Pressure           -1.0388e+06      5.8894e+05      3.1097e+05      2.8026e+05
v  k                   4.9067e-06          75.372         0.17438         0.11747
v  epsilon               0.006276      1.1705e+07           16292          137.98
v  TurbVisc            4.8123e-12         0.79753       0.0042225        0.048073
v  total_pressure     -5.3876e+05      1.0889e+06      8.1097e+05      7.8026e+05


 TIME FOR THE TIME STEP              640:        0.78025E+02

===============================================================


 INSTANT    0.641000000E+03   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         0.415753970E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888909E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.318          51.609          3.1962         0.35644
v  Velocity[Y]            -44.129          49.615          1.2247         0.82394
v  Velocity[Z]            -89.551          76.356         -1.6197      -0.0012488
v  ǁVelocityǁ           0.0016463          97.452          9.6274           7.691
v  Pressure           -1.0465e+06      5.8893e+05      3.1148e+05      2.8068e+05
v  k                   5.6478e-06          74.396         0.17517         0.11793
v  epsilon              0.0055924      1.1784e+07           16284          139.86
v  TurbVisc            3.7698e-11         0.91824       0.0042538        0.048108
v  total_pressure     -5.4652e+05      1.0889e+06      8.1148e+05      7.8068e+05


 TIME FOR THE TIME STEP              643:        0.68793E+02

===============================================================


 INSTANT    0.644000000E+03   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.190998889E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           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]              -21.2          54.272          3.1972         0.35643
v  Velocity[Y]            -43.386           40.09          1.2266         0.82382
v  Velocity[Z]            -84.843          79.004         -1.6097     -0.00046001
v  ǁVelocityǁ           0.0016419          100.85          9.6205          7.6925
v  Pressure           -1.0436e+06      5.8753e+05      3.1047e+05      2.7997e+05
v  k                   6.1892e-06          79.184         0.17478         0.11773
v  epsilon               0.005961      1.1669e+07           16302          139.39
v  TurbVisc            3.5611e-11         0.92383       0.0042352        0.048085
v  total_pressure     -5.4361e+05      1.0875e+06      8.1047e+05      7.7997e+05


 TIME FOR THE TIME STEP              641:        0.80497E+02

===============================================================


 INSTANT    0.642000000E+03   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        -0.423876351E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14549E+03 0.25918E+02
   Friction velocity        uet   :  0.35672E-01 0.70673E+01
   Friction velocity        uk    :  0.61497E-01 0.75139E+01
   Dimensionless distance   yplus :  0.45196E-03 0.51674E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18412
   Nb of faces within the viscous sub-layer     :       7800
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13977E+02     119   0.19199E+00   0.18473E+04 0.99920E+03 
c  Velocity[X]                                      0.50034E+03 
c  Velocity[Y]                                      0.50651E+03 
c  Velocity[Z]                                      0.84046E+03 
c  Pressure     0.24881E+00     691   0.85402E-02   0.40728E+00 0.19751E+04 
c  k            0.21055E+01      74   0.66049E-02   0.17027E+02 0.13101E+04 
c  epsilon      0.39942E+05      54   0.72629E-02   0.54358E+10 0.55968E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020545                             3
a  epsilon         -229.89                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.758          52.342          3.1961         0.35594
v  Velocity[Y]            -47.716          48.663          1.2252         0.82328
v  Velocity[Z]            -82.985          88.279         -1.6138      -0.0004957
v  ǁVelocityǁ           0.0016492          95.472          9.6229          7.6911
v  Pressure           -1.0432e+06      5.8864e+05      3.1105e+05      2.8035e+05
v  k                   5.8485e-06          82.564          0.1751         0.11788
v  epsilon              0.0057356      1.1591e+07           16307          140.11
v  TurbVisc            3.7603e-11          0.9557       0.0042457        0.048097
v  total_pressure     -5.4318e+05      1.0886e+06      8.1105e+05      7.8035e+05


 TIME FOR THE TIME STEP              642:        0.65355E+02

===============================================================


 INSTANT    0.643000000E+03   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         0.753816185E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective 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            -0.0023862                             3
a  epsilon         -653.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.141          51.408          3.1945         0.35619
v  Velocity[Y]            -45.645          41.626           1.225         0.82317
v  Velocity[Z]            -80.906          82.335         -1.6268     -0.00065376
v  ǁVelocityǁ           0.0016559          98.164          9.6354          7.6923
v  Pressure           -1.0515e+06       5.898e+05      3.1193e+05      2.8112e+05
v  k                    5.484e-06          71.055         0.17519         0.11797
v  epsilon              0.0055308      1.1558e+07           16294          138.02
v  TurbVisc            3.7827e-11         0.72463       0.0042656        0.048134
v  total_pressure     -5.5153e+05      1.0898e+06      8.1193e+05      7.8112e+05


 TIME FOR THE TIME STEP              645:        0.68443E+02

===============================================================


 INSTANT    0.646000000E+03   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         0.106484343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888901E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.318          51.609          3.1962         0.35644
v  Velocity[Y]            -44.129          49.615          1.2247         0.82394
v  Velocity[Z]            -89.551          76.356         -1.6197      -0.0012488
v  ǁVelocityǁ           0.0016463          97.452          9.6274           7.691
v  Pressure           -1.0465e+06      5.8893e+05      3.1148e+05      2.8068e+05
v  k                   5.6478e-06          74.396         0.17517         0.11793
v  epsilon              0.0055924      1.1784e+07           16284          139.86
v  TurbVisc            3.7698e-11         0.91824       0.0042538        0.048108
v  total_pressure     -5.4652e+05      1.0889e+06      8.1148e+05      7.8068e+05


 TIME FOR THE TIME STEP              643:        0.77762E+02

===============================================================


 INSTANT    0.644000000E+03   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.190998889E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19154E+03 0.29534E+02
   Friction velocity        uet   :  0.38427E-01 0.69996E+01
   Friction velocity        uk    :  0.61555E-01 0.75174E+01
   Dimensionless distance   yplus :  0.45244E-03 0.47461E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18429
   Nb of faces within the viscous sub-layer     :       7775
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13970E+02     119   0.19567E+00   0.16448E+04 0.94784E+03 
c  Velocity[X]                                      0.48797E+03 
c  Velocity[Y]                                      0.44055E+03 
c  Velocity[Z]                                      0.71632E+03 
c  Pressure     0.23507E+00     592   0.86417E-02   0.38382E+00 0.54449E+03 
c  k            0.18961E+01      71   0.57157E-02   0.10703E+02 0.11346E+04 
c  epsilon      0.38304E+05      51   0.56443E-02   0.61146E+10 0.51957E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021968                             3
a  epsilon         -341.46                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -31.004          50.259          3.1949         0.35547
v  Velocity[Y]            -40.488          43.122          1.2243         0.82265
v  Velocity[Z]            -83.086          69.709         -1.6229     -0.00063941
v  ǁVelocityǁ           0.0016571          93.625          9.6296          7.6901
v  Pressure           -1.0522e+06      5.8923e+05      3.1139e+05      2.8069e+05
v  k                   5.5158e-06          70.811         0.17516         0.11789
v  epsilon              0.0055276      1.1678e+07           16317          138.64
v  TurbVisc            3.7686e-11         0.78155       0.0042606        0.048121
v  total_pressure     -5.5223e+05      1.0892e+06      8.1139e+05      7.8069e+05


 TIME FOR THE TIME STEP              644:        0.70414E+02

===============================================================


 INSTANT    0.645000000E+03   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.654954533E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.00000
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020901                             4
a  epsilon         -600.72                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.179          52.898          3.1973         0.35535
v  Velocity[Y]            -49.404          41.935          1.2312         0.82345
v  Velocity[Z]            -81.163           70.75         -1.6366     -0.00079131
v  ǁVelocityǁ           0.0016726          95.313          9.6493          7.6931
v  Pressure           -1.0552e+06      5.9169e+05      3.1313e+05      2.8215e+05
v  k                   5.5966e-06          66.842         0.17502         0.11792
v  epsilon              0.0057161      1.1702e+07           16268          136.07
v  TurbVisc            3.8003e-11          0.6535       0.0042774        0.048163
v  total_pressure     -5.5521e+05      1.0917e+06      8.1313e+05      7.8215e+05


 TIME FOR THE TIME STEP              647:        0.69250E+02

===============================================================


 INSTANT    0.648000000E+03   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         0.302044621E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.0000a  k            -0.0023862                             3
a  epsilon         -653.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.141          51.408          3.1945         0.35619
v  Velocity[Y]            -45.645          41.626           1.225         0.82317
v  Velocity[Z]            -80.906          82.335         -1.6268     -0.00065376
v  ǁVelocityǁ           0.0016559          98.164          9.6354          7.6923
v  Pressure           -1.0515e+06       5.898e+05      3.1193e+05      2.8112e+05
v  k                    5.484e-06          71.055         0.17519         0.11797
v  epsilon              0.0055308      1.1558e+07           16294          138.02
v  TurbVisc            3.7827e-11         0.72463       0.0042656        0.048134
v  total_pressure     -5.5153e+05      1.0898e+06      8.1193e+05      7.8112e+05


 TIME FOR THE TIME STEP              645:        0.72568E+02

===============================================================


 INSTANT    0.646000000E+03   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         0.106484343E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888901E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11596E+03 0.24886E+02
   Friction velocity        uet   :  0.39188E-01 0.70702E+01
   Friction velocity        uk    :  0.69756E-01 0.75294E+01
   Dimensionless distance   yplus :  0.45326E-03 0.42845E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18485
   Nb of faces within the viscous sub-layer     :       7778
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13974E+02     117   0.19530E+00   0.17722E+04 0.97988E+03 
c  Velocity[X]                                      0.47001E+03 
c  Velocity[Y]                                      0.51007E+03 
c  Velocity[Z]                                      0.79216E+03 
c  Pressure     0.24246E+00     593   0.65186E-02   0.39609E+00 0.25680E+04 
c  k            0.17687E+01      70   0.44336E-02   0.69771E+01 0.95666E+03 
c  epsilon      0.36971E+05      49   0.40027E-02   0.26947E+10 0.53740E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002131                             3
a  epsilon         -408.69                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.113          51.814           3.194         0.35516
v  Velocity[Y]            -43.348          66.502          1.2278         0.82341
v  Velocity[Z]            -82.468          127.84         -1.6304     -0.00023359
v  ǁVelocityǁ           0.0016632          140.93          9.6409           7.692
v  Pressure           -1.0518e+06      5.9153e+05      3.1272e+05      2.8168e+05
v  k                    5.504e-06          65.166         0.17505         0.11793
v  epsilon              0.0055974      1.1867e+07           16287          136.95
v  TurbVisc            2.5181e-11         0.71221        0.004273         0.04815
v  total_pressure     -5.5178e+05      1.0915e+06      8.1272e+05      7.8168e+05


 TIME FOR THE TIME STEP              646:        0.61241E+02

===============================================================


 INSTANT    0.647000000E+03   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         0.928581662E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15 -----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020555                             3
a  epsilon         -504.26                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -29.778          59.895          3.2024         0.35491
v  Velocity[Y]            -48.113          41.817          1.2404         0.82361
v  Velocity[Z]            -90.573          69.833         -1.6457     -0.00035731
v  ǁVelocityǁ           0.0016786          106.09          9.6706          7.6959
v  Pressure           -1.0573e+06       5.917e+05      3.1343e+05      2.8238e+05
v  k                   5.9143e-06          66.893         0.17506         0.11775
v  epsilon              0.0060875      1.1608e+07           16302          133.87
v  TurbVisc            3.8326e-11         0.70827       0.0042898        0.048185
v  total_pressure      -5.573e+05      1.0917e+06      8.1343e+05      7.8238e+05


 TIME FOR THE TIME STEP              649:        0.72294E+02

===============================================================


 INSTANT    0.650000000E+03   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020901                             4
a  epsilon         -600.72                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.179          52.898          3.1973         0.35535
v  Velocity[Y]            -49.404          41.935          1.2312         0.82345
v  Velocity[Z]            -81.163           70.75         -1.6366     -0.00079131
v  ǁVelocityǁ           0.0016726          95.313          9.6493          7.6931
v  Pressure           -1.0552e+06      5.9169e+05      3.1313e+05      2.8215e+05
v  k                   5.5966e-06          66.842         0.17502         0.11792
v  epsilon              0.0057161      1.1702e+07           16268          136.07
v  TurbVisc            3.8003e-11          0.6535       0.0042774        0.048163
v  total_pressure     -5.5521e+05      1.0917e+06      8.1313e+05      7.8215e+05


 TIME FOR THE TIME STEP              647:        0.62586E+02

===============================================================


 INSTANT    0.648000000E+03   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         0.302044621E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888910E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10543E+03 0.26166E+02
   Friction velocity        uet   :  0.41692E-01 0.68494E+01
   Friction velocity        uk    :  0.48952E-01 0.75423E+01
   Dimensionless distance   yplus :  0.45599E-03 0.42689E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18508
   Nb of faces within the viscous sub-layer     :       7787
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13940E+02     116   0.19222E+00   0.16365E+04 0.94585E+03 
c  Velocity[X]                                      0.45929E+03 
c  Velocity[Y]                                      0.45171E+03 
c  Velocity[Z]                                      0.72547E+03 
c  Pressure     0.22013E+00     582   0.61003E-02   0.35581E+00 0.21639E+04 
c  k            0.16834E+01      70   0.57391E-02   0.72879E+01 0.10564E+04 
c  epsilon      0.35938E+05      48   0.58121E-02   0.14396E+11 0.43677E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022665                             3
a  epsilon         -672.78                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.157          52.814          3.1987         0.35453
v  Velocity[Y]            -42.908          41.073          1.2361         0.82326
v  Velocity[Z]            -88.016          73.303         -1.6404     -0.00049134
v  ǁVelocityǁ           0.0016756           101.2          9.6592          7.6941
v  Pressure           -1.0539e+06      5.9201e+05      3.1363e+05      2.8248e+05
v  k                   5.7358e-06          70.815         0.17502         0.11785
v  epsilon              0.0058809       1.194e+07           16302          134.99
v  TurbVisc            2.4924e-12           0.676        0.004284        0.048175
v  total_pressure     -5.5388e+05       1.092e+06      8.1363e+05      7.8248e+05


 TIME FOR THE TIME STEP              648:        0.66493E+02

===============================================================


 INSTANT    0.649000000E+03   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.225334668E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Frc  k            0.15896E+01      70   0.54243E-02   0.72035E+01 0.12348E+04 
c  epsilon      0.35152E+05      49   0.35206E-02   0.36383E+10 0.34310E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002246                             3
a  epsilon         -614.93                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.073          56.774          3.2096         0.35479
v  Velocity[Y]             -44.25           42.21          1.2499         0.82414
v  Velocity[Z]            -109.16          70.841         -1.6543     -0.00037976
v  ǁVelocityǁ           0.0016813          111.24          9.6942          7.7005
v  Pressure           -1.0626e+06      5.9378e+05      3.1408e+05      2.8303e+05
v  k                   6.3745e-06          66.653         0.17551         0.11781
v  epsilon              0.0066057      1.1895e+07           16346          133.52
v  TurbVisc            3.8503e-11         0.69778       0.0043068        0.048201
v  total_pressure     -5.6264e+05      1.0938e+06      8.1408e+05      7.8303e+05


 TIME FOR THE TIME STEP              651:        0.66241E+02

===============================================================


 INSTANT    0.652000000E+03   TIME STEP NUMBER             652
 ============================================================= 




   ** 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            -0.0020555                             3
a  epsilon         -504.26                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -29.778          59.895          3.2024         0.35491
v  Velocity[Y]            -48.113          41.817          1.2404         0.82361
v  Velocity[Z]            -90.573          69.833         -1.6457     -0.00035731
v  ǁVelocityǁ           0.0016786          106.09          9.6706          7.6959
v  Pressure           -1.0573e+06       5.917e+05      3.1343e+05      2.8238e+05
v  k                   5.9143e-06          66.893         0.17506         0.11775
v  epsilon              0.0060875      1.1608e+07           16302          133.87
v  TurbVisc            3.8326e-11         0.70827       0.0042898        0.048185
v  total_pressure      -5.573e+05      1.0917e+06      8.1343e+05      7.8238e+05


 TIME FOR THE TIME STEP              649:        0.65791E+02

===============================================================


 INSTANT    0.650000000E+03   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.250189806E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888904E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19299E+03 0.27386E+02
   Friction velocity        uet   :  0.15933E-01 0.76198E+01
   Friction velocity        uk    :  0.40691E-01 0.75392E+01
   Dimensionless distance   yplus :  0.45696E-03 0.38826E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18543
   Nb of faces within the viscous sub-layer     :       7771
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13945E+02     116   0.18961E+00   0.15469E+04 0.92546E+03 
c  Velocity[X]                                      0.47920E+03 
c  Velocity[Y]                                      0.43318E+03 
c  Velocity[Z]                                      0.63457E+03 
c  Pressure     0.21800E+00     788   0.58765E-02   0.35015E+00 0.10739E+04 
c  k            0.16089E+01      69   0.61186E-02   0.75994E+01 0.10634E+04 
c  epsilon      0.35252E+05      47   0.45429E-02   0.43078E+10 0.95570E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022081                             3
a  epsilon         -646.91                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.238          50.704          3.2052         0.35449
v  Velocity[Y]             -43.84          43.782          1.2449         0.82356
v  Velocity[Z]            -75.057          115.45         -1.6494      -0.0002701
v  ǁVelocityǁ           0.0016812          123.58          9.6819          7.6981
v  Pressure           -1.0624e+06       5.937e+05      3.1406e+05      2.8296e+05
v  k                    6.111e-06          70.028         0.17532          0.1178
v  epsilon               0.006321      1.1834e+07           16329          133.79
v  TurbVisc            3.8429e-11          0.6715       0.0042965        0.048192
v  total_pressure     -5.6241e+05      1.0937e+06      8.1406e+05      7.8296e+05


 TIME FOR THE TIME STEP              650:        0.71744E+02

===============================================================


 INSTANT    0.651000000E+03   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.28c  Velocity[Z]                                      0.64966E+03 
c  Pressure     0.21105E+00     651   0.69951E-02   0.33399E+00 0.13570E+04 
c  k            0.17427E+01      69   0.67144E-02   0.13159E+02 0.14818E+04 
c  epsilon      0.36297E+05      50   0.53762E-02   0.76495E+10 0.41945E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022065                             4
a  epsilon         -838.14                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.817          54.396           3.217         0.35454
v  Velocity[Y]            -45.428          76.982          1.2606         0.82441
v  Velocity[Z]             -79.78           74.58         -1.6604       -0.000629
v  ǁVelocityǁ           0.0016747          93.323          9.7141          7.7059
v  Pressure           -1.0666e+06      5.9527e+05      3.1444e+05      2.8346e+05
v  k                   6.9394e-06          67.526         0.17656         0.11819
v  epsilon               0.007145      1.1664e+07           16417          135.74
v  TurbVisc            3.8337e-11         0.71281       0.0043322        0.048213
v  total_pressure     -5.6656e+05      1.0953e+06      8.1444e+05      7.8346e+05


 TIME FOR THE TIME STEP              653:        0.69835E+02

===============================================================


 INSTANT    0.654000000E+03   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      --------------c  k            0.15896E+01      70   0.54243E-02   0.72035E+01 0.12348E+04 
c  epsilon      0.35152E+05      49   0.35206E-02   0.36383E+10 0.34310E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002246                             3
a  epsilon         -614.93                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.073          56.774          3.2096         0.35479
v  Velocity[Y]             -44.25           42.21          1.2499         0.82414
v  Velocity[Z]            -109.16          70.841         -1.6543     -0.00037976
v  ǁVelocityǁ           0.0016813          111.24          9.6942          7.7005
v  Pressure           -1.0626e+06      5.9378e+05      3.1408e+05      2.8303e+05
v  k                   6.3745e-06          66.653         0.17551         0.11781
v  epsilon              0.0066057      1.1895e+07           16346          133.52
v  TurbVisc            3.8503e-11         0.69778       0.0043068        0.048201
v  total_pressure     -5.6264e+05      1.0938e+06      8.1408e+05      7.8303e+05


 TIME FOR THE TIME STEP              651:        0.60343E+02

===============================================================


 INSTANT    0.652000000E+03   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.818391733E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888901E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25942E+03 0.32951E+02
   Friction velocity        uet   :  0.37222E-01 0.83043E+01
   Friction velocity        uk    :  0.64240E-01 0.75192E+01
   Dimensionless distance   yplus :  0.45730E-03 0.39337E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18533
   Nb of faces within the viscous sub-layer     :       7734
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13952E+02     116   0.19170E+00   0.16693E+04 0.95593E+03 
c  Velocity[X]                                      0.47735E+03 
c  Velocity[Y]                                      0.46257E+03 
c  Velocity[Z]                                      0.72935E+03 
c  Pressure     0.19988E+00     656   0.56397E-02   0.31755E+00 0.11673E+04 
c  k            0.16828E+01      68   0.75648E-02   0.13839E+02 0.14861E+04 
c  epsilon      0.35796E+05      48   0.56307E-02   0.25240E+11 0.49084E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023931                             3
a  epsilon         -581.59                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -28.113          50.531          3.2126         0.35399
v  Velocity[Y]            -52.758           41.05          1.2554         0.82402
v  Velocity[Z]            -72.339          69.532         -1.6583     -0.00055854
v  ǁVelocityǁ           0.0016751          91.976          9.7035          7.7018
v  Pressure           -1.0651e+06      5.9548e+05      3.1459e+05      2.8349e+05
v  k                   6.6295e-06          71.547         0.17612           0.118
v  epsilon               0.006865      1.1735e+07           16421          134.55
v  TurbVisc            3.8398e-11         0.66778       0.0043169        0.048207
v  total_pressure     -5.6515e+05      1.0955e+06      8.1459e+05      7.8349e+05


 TIME FOR THE TIME STEP              652:        0.67524E+02

===============================================================


 INSTANT    0.653000000E+03   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
----c  Velocity[X]                                      0.47045E+03 
c  Velocity[Y]                                      0.49378E+03 
c  Velocity[Z]                                      0.60426E+03 
c  Pressure     0.20112E+00     571   0.53797E-02   0.31478E+00 0.64410E+03 
c  k            0.19490E+01      70   0.75026E-02   0.25284E+02 0.18251E+04 
c  epsilon      0.38081E+05      53   0.66087E-02   0.83840E+10 0.45294E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023333                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.832          51.411           3.224          0.3536
v  Velocity[Y]            -42.338          41.742          1.2722         0.82505
v  Velocity[Z]            -73.769          111.89          -1.665     -0.00050834
v  ǁVelocityǁ            0.001676          117.99          9.7346          7.7122
v  Pressure           -1.0755e+06      5.9695e+05      3.1549e+05      2.8435e+05
v  k                   7.6083e-06          83.353         0.17781          0.1187
v  epsilon               0.007753      1.1744e+07           16495          138.83
v  TurbVisc            3.8168e-11         0.75415       0.0043642        0.048225
v  total_pressure     -5.7555e+05       1.097e+06      8.1549e+05      7.8435e+05


 TIME FOR THE TIME STEP              655:        0.66388E+02

===============================================================


 INSTANT    0.656000000E+03   TIME STEP NUMBER             656
 ============================================================= 




   ** Bc  Velocity[Z]                                      0.64966E+03 
c  Pressure     0.21105E+00     651   0.69951E-02   0.33399E+00 0.13570E+04 
c  k            0.17427E+01      69   0.67144E-02   0.13159E+02 0.14818E+04 
c  epsilon      0.36297E+05      50   0.53762E-02   0.76495E+10 0.41945E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022065                             4
a  epsilon         -838.14                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -32.817          54.396           3.217         0.35454
v  Velocity[Y]            -45.428          76.982          1.2606         0.82441
v  Velocity[Z]             -79.78           74.58         -1.6604       -0.000629
v  ǁVelocityǁ           0.0016747          93.323          9.7141          7.7059
v  Pressure           -1.0666e+06      5.9527e+05      3.1444e+05      2.8346e+05
v  k                   6.9394e-06          67.526         0.17656         0.11819
v  epsilon               0.007145      1.1664e+07           16417          135.74
v  TurbVisc            3.8337e-11         0.71281       0.0043322        0.048213
v  total_pressure     -5.6656e+05      1.0953e+06      8.1444e+05      7.8346e+05


 TIME FOR THE TIME STEP              653:        0.68612E+02

===============================================================


 INSTANT    0.654000000E+03   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.326351207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888902E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17422E+03 0.36464E+02
   Friction velocity        uet   :  0.34420E-01 0.71515E+01
   Friction velocity        uk    :  0.57392E-01 0.75755E+01
   Dimensionless distance   yplus :  0.45662E-03 0.41024E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18551
   Nb of faces within the viscous sub-layer     :       7720
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13982E+02     115   0.19434E+00   0.15036E+04 0.92951E+03 
c  Velocity[X]                                      0.48310E+03 
c  Velocity[Y]                                      0.48395E+03 
c  Velocity[Z]                                      0.53655E+03 
c  Pressure     0.20354E+00     772   0.55914E-02   0.32253E+00 0.20602E+04 
c  k            0.18818E+01      70   0.78446E-02   0.18027E+02 0.15543E+04 
c  epsilon      0.37374E+05      52   0.63622E-02   0.31045E+10 0.76765E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021119                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.368            51.2          3.2199         0.35386
v  Velocity[Y]            -49.812          50.651          1.2668         0.82468
v  Velocity[Z]            -78.866          79.382         -1.6628     -0.00025091
v  ǁVelocityǁ            0.001685          92.527           9.724          7.7077
v  Pressure           -1.0707e+06      5.9708e+05       3.152e+05      2.8406e+05
v  k                   7.2387e-06           75.28         0.17718         0.11847
v  epsilon              0.0074366      1.1995e+07           16457          137.34
v  TurbVisc            1.7102e-11         0.67248       0.0043467        0.048218
v  total_pressure     -5.7072e+05      1.0971e+06       8.152e+05      7.8406e+05


 TIME FOR THE TIME STEP              654:        0.74241E+02

===============================================================


 INSTANT    0.655000000E+03   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-----c  Velocity     0.13993E+02     117   0.18814E+00   0.14807E+04 0.92241E+03 
c  Velocity[X]                                      0.45184E+03 
c  Velocity[Y]                                      0.42813E+03 
c  Velocity[Z]                                      0.60075E+03 
c  Pressure     0.20566E+00     729   0.60443E-02   0.31996E+00 0.11016E+04 
c  k            0.21824E+01      70   0.81452E-02   0.22184E+02 0.16003E+04 
c  epsilon      0.40412E+05      53   0.84642E-02   0.23679E+11 0.45351E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021961                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.724          59.294          3.2323         0.35355
v  Velocity[Y]            -44.113          42.118          1.2845         0.82497
v  Velocity[Z]            -86.174          107.38         -1.6695     -0.00088576
v  ǁVelocityǁ           0.0016699          118.16          9.7552          7.7188
v  Pressure           -1.0846e+06      5.9797e+05      3.1615e+05      2.8484e+05
v  k                   8.2642e-06          98.083         0.17901         0.11919
v  epsilon              0.0083878      1.1754e+07           16586          141.34
v  TurbVisc            3.8079e-11         0.86644       0.0044017        0.048239
v  total_pressure     -5.8463e+05       1.098e+06      8.1615e+05      7.8484e+05


 TIME FOR THE TIME STEP              657:        0.67041E+02

===============================================================


 INSTANT    0.658000000E+03   TIME STEP NUMBER        c  Velocity[X]                                      0.47045E+03 
c  Velocity[Y]                                      0.49378E+03 
c  Velocity[Z]                                      0.60426E+03 
c  Pressure     0.20112E+00     571   0.53797E-02   0.31478E+00 0.64410E+03 
c  k            0.19490E+01      70   0.75026E-02   0.25284E+02 0.18251E+04 
c  epsilon      0.38081E+05      53   0.66087E-02   0.83840E+10 0.45294E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023333                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.832          51.411           3.224          0.3536
v  Velocity[Y]            -42.338          41.742          1.2722         0.82505
v  Velocity[Z]            -73.769          111.89          -1.665     -0.00050834
v  ǁVelocityǁ            0.001676          117.99          9.7346          7.7122
v  Pressure           -1.0755e+06      5.9695e+05      3.1549e+05      2.8435e+05
v  k                   7.6083e-06          83.353         0.17781          0.1187
v  epsilon               0.007753      1.1744e+07           16495          138.83
v  TurbVisc            3.8168e-11         0.75415       0.0043642        0.048225
v  total_pressure     -5.7555e+05       1.097e+06      8.1549e+05      7.8435e+05


 TIME FOR THE TIME STEP              655:        0.70048E+02

===============================================================


 INSTANT    0.656000000E+03   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.438671366E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22698E+03 0.32602E+02
   Friction velocity        uet   :  0.36231E-01 0.77939E+01
   Friction velocity        uk    :  0.61302E-01 0.75660E+01
   Dimensionless distance   yplus :  0.45678E-03 0.43480E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18579
   Nb of faces within the viscous sub-layer     :       7696
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13995E+02     118   0.18832E+00   0.14564E+04 0.91010E+03 
c  Velocity[X]                                      0.44120E+03 
c  Velocity[Y]                                      0.42071E+03 
c  Velocity[Z]                                      0.59451E+03 
c  Pressure     0.20031E+00     679   0.59959E-02   0.31670E+00 0.15023E+04 
c  k            0.20680E+01      70   0.77791E-02   0.20145E+02 0.15795E+04 
c  epsilon      0.39200E+05      52   0.65770E-02   0.44921E+10 0.37775E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023242                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.923          55.953          3.2282          0.3535
v  Velocity[Y]            -47.619          42.328          1.2793         0.82531
v  Velocity[Z]            -80.709          73.763         -1.6664      0.00011859
v  ǁVelocityǁ           0.0016704          95.251          9.7445          7.7146
v  Pressure           -1.0795e+06      5.9863e+05      3.1602e+05      2.8476e+05
v  k                   7.9204e-06          92.138         0.17841         0.11893
v  epsilon              0.0080627      1.2008e+07           16535          140.04
v  TurbVisc            3.8035e-11         0.80615       0.0043821        0.048231
v  total_pressure     -5.7948e+05      1.0986e+06      8.1602e+05      7.8476e+05


 TIME FOR THE TIME STEP              656:        0.69393E+02

===============================================================


 INSTANT    0.657000000E+03   TIME STEP NUMBER             657
 ============================================================= 




  -----------------------------------------------------------------------------
c  Velocity     0.14022E+02     118   0.19233E+00   0.14378E+04 0.92260E+03 
c  Velocity[X]                                      0.45559E+03 
c  Velocity[Y]                                      0.43385E+03 
c  Velocity[Z]                                      0.54839E+03 
c  Pressure     0.20981E+00     638   0.57922E-02   0.32532E+00 0.10740E+04 
c  k            0.20418E+01      73   0.88776E-02   0.33804E+02 0.20798E+04 
c  epsilon      0.40484E+05      52   0.79980E-02   0.85539E+10 0.34977E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023086                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.602          51.733          3.2375         0.35339
v  Velocity[Y]            -44.199          41.173          1.2955         0.82587
v  Velocity[Z]            -75.264          69.869         -1.6759     -0.00086989
v  ǁVelocityǁ           0.0016635          89.402          9.7718          7.7256
v  Pressure           -1.0936e+06      6.0031e+05      3.1756e+05      2.8591e+05
v  k                   8.2706e-06          71.327          0.1801          0.1194
v  epsilon              0.0090062      1.1997e+07           16681          141.73
v  TurbVisc            3.8226e-11         0.75414       0.0044415        0.048254
v  total_pressure     -5.9359e+05      1.1003e+06      8.1756e+05      7.8591e+05


 TIME FOR THE TIME STEP              659:        0.69739E+02

===========================================c  Velocity     0.13993E+02     117   0.18814E+00   0.14807E+04 0.92241E+03 
c  Velocity[X]                                      0.45184E+03 
c  Velocity[Y]                                      0.42813E+03 
c  Velocity[Z]                                      0.60075E+03 
c  Pressure     0.20566E+00     729   0.60443E-02   0.31996E+00 0.11016E+04 
c  k            0.21824E+01      70   0.81452E-02   0.22184E+02 0.16003E+04 
c  epsilon      0.40412E+05      53   0.84642E-02   0.23679E+11 0.45351E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021961                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.724          59.294          3.2323         0.35355
v  Velocity[Y]            -44.113          42.118          1.2845         0.82497
v  Velocity[Z]            -86.174          107.38         -1.6695     -0.00088576
v  ǁVelocityǁ           0.0016699          118.16          9.7552          7.7188
v  Pressure           -1.0846e+06      5.9797e+05      3.1615e+05      2.8484e+05
v  k                   8.2642e-06          98.083         0.17901         0.11919
v  epsilon              0.0083878      1.1754e+07           16586          141.34
v  TurbVisc            3.8079e-11         0.86644       0.0044017        0.048239
v  total_pressure     -5.8463e+05       1.098e+06      8.1615e+05      7.8484e+05


 TIME FOR THE TIME STEP              657:        0.70568E+02

===============================================================


 INSTANT    0.658000000E+03   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         0.145376082E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888906E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27667E+03 0.35090E+02
   Friction velocity        uet   :  0.34009E-01 0.86655E+01
   Friction velocity        uk    :  0.46140E-01 0.75587E+01
   Dimensionless distance   yplus :  0.45570E-03 0.44052E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18604
   Nb of faces within the viscous sub-layer     :       7646
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14023E+02     117   0.19050E+00   0.16526E+04 0.96158E+03 
c  Velocity[X]                                      0.47102E+03 
c  Velocity[Y]                                      0.49601E+03 
c  Velocity[Z]                                      0.68562E+03 
c  Pressure     0.19318E+00     714   0.57546E-02   0.30318E+00 0.16283E+04 
c  k            0.21573E+01      72   0.84231E-02   0.31617E+02 0.20325E+04 
c  epsilon      0.40926E+05      51   0.90110E-02   0.95142E+10 0.44082E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021248                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.283          55.315          3.2353         0.35333
v  Velocity[Y]            -41.938          45.535          1.2912         0.82609
v  Velocity[Z]             -84.57          71.549         -1.6722      0.00012118
v  ǁVelocityǁ           0.0016723          94.244          9.7636          7.7214
v  Pressure           -1.0886e+06       6.008e+05       3.171e+05      2.8557e+05
v  k                   8.2634e-06          84.751         0.17976         0.11936
v  epsilon              0.0086977      1.1786e+07           16655          142.25
v  TurbVisc            3.8141e-11         0.88563       0.0044222        0.048247
v  total_pressure     -5.8863e+05      1.1008e+06       8.171e+05      7.8557e+05


 TIME FOR THE TIME STEP              658:        0.71760E+02

===============================================================


 INSTANT    0.659000000E+03   TIME STEP NUMBER            Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14039E+02     118   0.19202E+00   0.15145E+04 0.93536E+03 
c  Velocity[X]                                      0.48981E+03 
c  Velocity[Y]                                      0.46321E+03 
c  Velocity[Z]                                      0.56151E+03 
c  Pressure     0.20609E+00     536   0.59971E-02   0.31854E+00 0.56844E+03 
c  k            0.18977E+01      75   0.67317E-02   0.12307E+02 0.13868E+04 
c  epsilon      0.39293E+05      55   0.62105E-02   0.44784E+10 0.34456E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022842                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.464          55.101          3.2392         0.35338
v  Velocity[Y]            -44.967          41.679          1.3049         0.82633
v  Velocity[Z]            -81.386           84.68         -1.6818     -0.00035001
v  ǁVelocityǁ           0.0016579          95.715           9.784          7.7312
v  Pressure           -1.1001e+06      6.0084e+05      3.1873e+05      2.8678e+05
v  k                   8.2943e-06          61.406         0.18097         0.11947
v  epsilon              0.0095595      1.1921e+07           16740           140.9
v  TurbVisc            3.8169e-11          0.6036       0.0044748        0.048266
v  total_pressure      -6.001e+05      1.1008e+06      8.1873e+05      7.8678e+05


 TIME FOR THE TIME STEP    -----------------------------------------------------------------------------
c  Velocity     0.14022E+02     118   0.19233E+00   0.14378E+04 0.92260E+03 
c  Velocity[X]                                      0.45559E+03 
c  Velocity[Y]                                      0.43385E+03 
c  Velocity[Z]                                      0.54839E+03 
c  Pressure     0.20981E+00     638   0.57922E-02   0.32532E+00 0.10740E+04 
c  k            0.20418E+01      73   0.88776E-02   0.33804E+02 0.20798E+04 
c  epsilon      0.40484E+05      52   0.79980E-02   0.85539E+10 0.34977E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023086                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.602          51.733          3.2375         0.35339
v  Velocity[Y]            -44.199          41.173          1.2955         0.82587
v  Velocity[Z]            -75.264          69.869         -1.6759     -0.00086989
v  ǁVelocityǁ           0.0016635          89.402          9.7718          7.7256
v  Pressure           -1.0936e+06      6.0031e+05      3.1756e+05      2.8591e+05
v  k                   8.2706e-06          71.327          0.1801          0.1194
v  epsilon              0.0090062      1.1997e+07           16681          141.73
v  TurbVisc            3.8226e-11         0.75414       0.0044415        0.048254
v  total_pressure     -5.9359e+05      1.1003e+06      8.1756e+05      7.8591e+05


 TIME FOR THE TIME STEP              659:        0.67726E+02

===============================================================


 INSTANT    0.660000000E+03   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        -0.106660733E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888902E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17149E+03 0.33544E+02
   Friction velocity        uet   :  0.16115E-01 0.67195E+01
   Friction velocity        uk    :  0.63195E-01 0.75745E+01
   Dimensionless distance   yplus :  0.45516E-03 0.40493E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18603
   Nb of faces within the viscous sub-layer     :       7626
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14025E+02     117   0.19338E+00   0.15150E+04 0.93135E+03 
c  Velocity[X]                                      0.48865E+03 
c  Velocity[Y]                                      0.44280E+03 
c  Velocity[Z]                                      0.58351E+03 
c  Pressure     0.21030E+00     659   0.59485E-02   0.32773E+00 0.21756E+04 
c  k            0.19512E+01      75   0.69067E-02   0.15462E+02 0.15606E+04 
c  epsilon      0.39893E+05      55   0.64600E-02   0.56474E+10 0.40328E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022234                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.838          57.236          3.2387         0.35333
v  Velocity[Y]            -47.242          48.225          1.3011          0.8262
v  Velocity[Z]            -80.577          73.519         -1.6786     -0.00017987
v  ǁVelocityǁ           0.0016593          96.118          9.7783           7.728
v  Pressure           -1.0946e+06      6.0145e+05      3.1873e+05      2.8681e+05
v  k                   8.2797e-06          64.241         0.18059         0.11942
v  epsilon              0.0092823      1.1745e+07           16730          141.13
v  TurbVisc            3.8243e-11         0.63921       0.0044591        0.048261
v  total_pressure     -5.9462e+05      1.1014e+06      8.1873e+05      7.8681e+05


 TIME FOR THE TIME STEP              660:        0.68598E+02

===========================================-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14055E+02     118   0.19529E+00   0.14540E+04 0.92562E+03 
c  Velocity[X]                                      0.45877E+03 
c  Velocity[Y]                                      0.42443E+03 
c  Velocity[Z]                                      0.57076E+03 
c  Pressure     0.21874E+00     644   0.52255E-02   0.33966E+00 0.16762E+04 
c  k            0.19549E+01      73   0.74543E-02   0.15372E+02 0.13662E+04 
c  epsilon      0.39237E+05      54   0.72749E-02   0.34126E+10 0.53114E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002276                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.554          53.253          3.2381         0.35346
v  Velocity[Y]             -42.44          44.203          1.3118         0.82671
v  Velocity[Z]            -80.712          70.163         -1.6872     -0.00063798
v  ǁVelocityǁ           0.0016679          95.387          9.7929          7.7371
v  Pressure           -1.1056e+06      6.0197e+05      3.1965e+05      2.8742e+05
v  k                   8.3271e-06          68.706          0.1819         0.11977
v  epsilon               0.010081      1.1732e+07           16784          141.97
v  TurbVisc            3.8172e-11         0.63784       0.0045047         0.04828
v  total_pressure     -6.0558e+05   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14039E+02     118   0.19202E+00   0.15145E+04 0.93536E+03 
c  Velocity[X]                                      0.48981E+03 
c  Velocity[Y]                                      0.46321E+03 
c  Velocity[Z]                                      0.56151E+03 
c  Pressure     0.20609E+00     536   0.59971E-02   0.31854E+00 0.56844E+03 
c  k            0.18977E+01      75   0.67317E-02   0.12307E+02 0.13868E+04 
c  epsilon      0.39293E+05      55   0.62105E-02   0.44784E+10 0.34456E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022842                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.464          55.101          3.2392         0.35338
v  Velocity[Y]            -44.967          41.679          1.3049         0.82633
v  Velocity[Z]            -81.386           84.68         -1.6818     -0.00035001
v  ǁVelocityǁ           0.0016579          95.715           9.784          7.7312
v  Pressure           -1.1001e+06      6.0084e+05      3.1873e+05      2.8678e+05
v  k                   8.2943e-06          61.406         0.18097         0.11947
v  epsilon              0.0095595      1.1921e+07           16740           140.9
v  TurbVisc            3.8169e-11          0.6036       0.0044748        0.048266
v  total_pressure      -6.001e+05      1.1008e+06      8.1873e+05      7.8678e+05


 TIME FOR THE TIME STEP              661:        0.60107E+02

===============================================================


 INSTANT    0.662000000E+03   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.241024555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888869E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18693E+03 0.32659E+02
   Friction velocity        uet   :  0.74081E-02 0.69317E+01
   Friction velocity        uk    :  0.69373E-01 0.75752E+01
   Dimensionless distance   yplus :  0.45401E-03 0.39403E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18614
   Nb of faces within the viscous sub-layer     :       7582
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14055E+02     117   0.19250E+00   0.15278E+04 0.92927E+03 
c  Velocity[X]                                      0.47812E+03 
c  Velocity[Y]                                      0.45389E+03 
c  Velocity[Z]                                      0.59578E+03 
c  Pressure     0.20975E+00     681   0.58008E-02   0.32672E+00 0.40730E+03 
c  k            0.19312E+01      75   0.52519E-02   0.93534E+01 0.12411E+04 
c  epsilon      0.39330E+05      55   0.46417E-02   0.32634E+10 0.39849E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020807                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.497           58.27          3.2391         0.35406
v  Velocity[Y]            -46.502           42.57          1.3083         0.82623
v  Velocity[Z]            -79.791          74.046         -1.6848     -0.00046443
v  ǁVelocityǁ           0.0016615            97.1          9.7875          7.7325
v  Pressure           -1.1022e+06      6.0212e+05      3.1951e+05      2.8742e+05
v  k                    8.308e-06           64.31         0.18157         0.11964
v  epsilon              0.0098107      1.1782e+07           16773          141.62
v  TurbVisc             3.821e-11         0.62066       0.0044895        0.048272
v  total_pressure      -6.022e+05      1.1021e+06      8.1951e+05      7.8742e+05


 TIME FOR THE TIME STEP              66   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14076E+02     117   0.19025E+00   0.14616E+04 0.90880E+03 
c  Velocity[X]                                      0.45832E+03 
c  Velocity[Y]                                      0.43501E+03 
c  Velocity[Z]                                      0.56829E+03 
c  Pressure     0.23568E+00     645   0.57089E-02   0.36482E+00 0.27343E+03 
c  k            0.19894E+01      71   0.51269E-02   0.70859E+01 0.98626E+03 
c  epsilon      0.39644E+05      51   0.41160E-02   0.48208E+10 0.56970E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023482                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.313          54.584          3.2354         0.35349
v  Velocity[Y]            -44.016          55.236          1.3182         0.82669
v  Velocity[Z]            -81.764          101.88         -1.6904      -8.728e-05
v  ǁVelocityǁ           0.0016633          109.25          9.8008          7.7428
v  Pressure           -1.1117e+06      6.0304e+05      3.2028e+05      2.8784e+05
v  k                   7.9011e-06          66.292         0.18309         0.12014
v  epsilon               0.010653      1.1996e+07           16857          143.81
v  TurbVisc            3.8221e-11    -----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14055E+02     118   0.19529E+00   0.14540E+04 0.92562E+03 
c  Velocity[X]                                      0.45877E+03 
c  Velocity[Y]                                      0.42443E+03 
c  Velocity[Z]                                      0.57076E+03 
c  Pressure     0.21874E+00     644   0.52255E-02   0.33966E+00 0.16762E+04 
c  k            0.19549E+01      73   0.74543E-02   0.15372E+02 0.13662E+04 
c  epsilon      0.39237E+05      54   0.72749E-02   0.34126E+10 0.53114E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002276                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.554          53.253          3.2381         0.35346
v  Velocity[Y]             -42.44          44.203          1.3118         0.82671
v  Velocity[Z]            -80.712          70.163         -1.6872     -0.00063798
v  ǁVelocityǁ           0.0016679          95.387          9.7929          7.7371
v  Pressure           -1.1056e+06      6.0197e+05      3.1965e+05      2.8742e+05
v  k                   8.3271e-06          68.706          0.1819         0.11977
v  epsilon               0.010081      1.1732e+07           16784          141.97
v  TurbVisc            3.8172e-11         0.63784       0.0045047         0.04828
v  total_pressure     -6.0558e+05       1.102e+06      8.1965e+05      7.8742e+05


 TIME FOR THE TIME STEP              663:        0.66638E+02

===============================================================


 INSTANT    0.664000000E+03   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        -0.792732961E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888907E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13217E+03 0.31727E+02
   Friction velocity        uet   :  0.25464E-01 0.68334E+01
   Friction velocity        uk    :  0.47953E-01 0.75732E+01
   Dimensionless distance   yplus :  0.45530E-03 0.38617E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18618
   Nb of faces within the viscous sub-layer     :       7544
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14059E+02     118   0.19389E+00   0.16097E+04 0.95875E+03 
c  Velocity[X]                                      0.49472E+03 
c  Velocity[Y]                                      0.45301E+03 
c  Velocity[Z]                                      0.66199E+03 
c  Pressure     0.20945E+00     662   0.55717E-02   0.32443E+00 0.90472E+03 
c  k            0.20058E+01      71   0.46152E-02   0.91920E+01 0.11515E+04 
c  epsilon      0.39637E+05      52   0.52242E-02   0.40711E+10 0.36824E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021036                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.411          58.484          3.2374          0.3539
v  Velocity[Y]            -47.758          42.889          1.3154         0.82711
v  Velocity[Z]            -77.117          76.754         -1.6892     -0.00016661
v  ǁVelocityǁ           0.0016676          99.493          9.7972          7.7396
v  Pressure            -1.106e+06      6.0406e+05      3.2085e+05      2.8837e+05
v  k                    8.135e-06          67.459         0.18257         0.11999
v  epsilon               0.010345      1.1923e+07           16826          143.24
v  TurbVisc             3.815e-11         0.66841       0.0045177        0.048287
v  total_pressure     -6.0602e+05      1.1041e+06      8.20------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14119E+02     117   0.19429E+00   0.15975E+04 0.95463E+03 
c  Velocity[X]                                      0.48238E+03 
c  Velocity[Y]                                      0.45962E+03 
c  Velocity[Z]                                      0.65553E+03 
c  Pressure     0.23558E+00     736   0.62897E-02   0.36199E+00 0.12365E+04 
c  k            0.18135E+01      70   0.99512E-02   0.20643E+02 0.17411E+04 
c  epsilon      0.37927E+05      51   0.88598E-02   0.16915E+11 0.57515E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022946                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.176          53.338           3.228          0.3536
v  Velocity[Y]            -42.714           42.66          1.3226         0.82537
v  Velocity[Z]             -79.07          80.659         -1.6906     -0.00065556
v  ǁVelocityǁ           0.0016633          93.523           9.802            7.75
v  Pressure            -1.116e+06      6.0272e+05      3.2046e+05      2.8794e+05
v  k                   7.5946e-06          62.609          0.1838         0.12028
v  epsilon               0.011362      1.1983e+07       ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14076E+02     117   0.19025E+00   0.14616E+04 0.90880E+03 
c  Velocity[X]                                      0.45832E+03 
c  Velocity[Y]                                      0.43501E+03 
c  Velocity[Z]                                      0.56829E+03 
c  Pressure     0.23568E+00     645   0.57089E-02   0.36482E+00 0.27343E+03 
c  k            0.19894E+01      71   0.51269E-02   0.70859E+01 0.98626E+03 
c  epsilon      0.39644E+05      51   0.41160E-02   0.48208E+10 0.56970E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023482                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.313          54.584          3.2354         0.35349
v  Velocity[Y]            -44.016          55.236          1.3182         0.82669
v  Velocity[Z]            -81.764          101.88         -1.6904      -8.728e-05
v  ǁVelocityǁ           0.0016633          109.25          9.8008          7.7428
v  Pressure           -1.1117e+06      6.0304e+05      3.2028e+05      2.8784e+05
v  k                   7.9011e-06          66.292         0.18309         0.12014
v  epsilon               0.010653      1.1996e+07           16857          143.81
v  TurbVisc            3.8221e-11         0.67218       0.0045337        0.048297
v  total_pressure     -6.1169e+05       1.103e+06      8.2028e+05      7.8784e+05


 TIME FOR THE TIME STEP              665:        0.70789E+02

===============================================================


 INSTANT    0.666000000E+03   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.345715709E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888905E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25241E+03 0.32658E+02
   Friction velocity        uet   :  0.41117E-01 0.81025E+01
   Friction velocity        uk    :  0.70683E-01 0.75887E+01
   Dimensionless distance   yplus :  0.45499E-03 0.39943E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18640
   Nb of faces within the viscous sub-layer     :       7522
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14095E+02     116   0.19299E+00   0.16449E+04 0.93441E+03 
c  Velocity[X]                                      0.46955E+03 
c  Velocity[Y]                                      0.46662E+03 
c  Velocity[Z]                                      0.70877E+03 
c  Pressure     0.22090E+00     790   0.57714E-02   0.34208E+00 0.86259E+03 
c  k            0.19209E+01      71   0.96320E-02   0.17379E+02 0.14741E+04 
c  epsilon      0.39138E+05      51   0.71170E-02   0.64734E+10 0.60195E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020515                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.153          60.101          3.2317          0.3531
v  Velocity[Y]            -49.446          42.859          1.3216         0.82645
v  Velocity[Z]            -90.407           76.77         -1.6917     -0.00053602
v  ǁVelocityǁ           0.0016631          100.61          9.8016          7.7462
v  Pressure           -1.1143e+06      6.0376e+05      3.2097e+05      2.8828e+05
v  k                   7.7202e-06          63.743         0.18356         0.12022
v  epsilon               0.010984      1.1831e+07           16901          143.65
v  TurbVisc            3.5629e-12         0.66656       0.0045495        0.04830   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14138E+02     115   0.19262E+00   0.15990E+04 0.95462E+03 
c  Velocity[X]                                      0.48755E+03 
c  Velocity[Y]                                      0.47587E+03 
c  Velocity[Z]                                      0.63562E+03 
c  Pressure     0.26119E+00     640   0.62434E-02   0.40063E+00 0.67629E+03 
c  k            0.16812E+01      72   0.81594E-02   0.22476E+02 0.17134E+04 
c  epsilon      0.36229E+05      50   0.75392E-02   0.33661E+11 0.58460E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020364                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.791          58.491          3.2169         0.35419
v  Velocity[Y]            -49.898           50.68          1.3241         0.82498
v  Velocity[Z]            -86.213          146.26         -1.6876     -0.00091709
v  ǁVelocityǁ           0.0016966          153.19          9.7982          7.7554
v  Pressure           -1.1199e+06      6.0293e+05      3.2057e+05      2.8797e+05
v  k                    7.539e-06          70.739          0.1845      ------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14119E+02     117   0.19429E+00   0.15975E+04 0.95463E+03 
c  Velocity[X]                                      0.48238E+03 
c  Velocity[Y]                                      0.45962E+03 
c  Velocity[Z]                                      0.65553E+03 
c  Pressure     0.23558E+00     736   0.62897E-02   0.36199E+00 0.12365E+04 
c  k            0.18135E+01      70   0.99512E-02   0.20643E+02 0.17411E+04 
c  epsilon      0.37927E+05      51   0.88598E-02   0.16915E+11 0.57515E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022946                             3
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.176          53.338           3.228          0.3536
v  Velocity[Y]            -42.714           42.66          1.3226         0.82537
v  Velocity[Z]             -79.07          80.659         -1.6906     -0.00065556
v  ǁVelocityǁ           0.0016633          93.523           9.802            7.75
v  Pressure            -1.116e+06      6.0272e+05      3.2046e+05      2.8794e+05
v  k                   7.5946e-06          62.609          0.1838         0.12028
v  epsilon               0.011362      1.1983e+07           16894          142.83
v  TurbVisc            3.8207e-11          0.6431       0.0045653         0.04832
v  total_pressure     -6.1597e+05      1.1027e+06      8.2046e+05      7.8794e+05


 TIME FOR THE TIME STEP              667:        0.67646E+02

===============================================================


 INSTANT    0.668000000E+03   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        -0.105520258E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888868E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16493E+03 0.30947E+02
   Friction velocity        uet   :  0.38550E-01 0.67672E+01
   Friction velocity        uk    :  0.71771E-01 0.75841E+01
   Dimensionless distance   yplus :  0.45402E-03 0.39609E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18654
   Nb of faces within the viscous sub-layer     :       7514
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14126E+02     116   0.19668E+00   0.15970E+04 0.94222E+03 
c  Velocity[X]                                      0.48136E+03 
c  Velocity[Y]                                      0.47378E+03 
c  Velocity[Z]                                      0.64187E+03 
c  Pressure     0.22094E+00     792   0.60866E-02   0.34145E+00 0.68393E+03 
c  k            0.17207E+01      70   0.11569E-01   0.33318E+02 0.20823E+04 
c  epsilon      0.36906E+05      50   0.97605E-02   0.70199E+11 0.74375E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020493                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -29.339          58.448          3.2232           0.354
v  Velocity[Y]            -52.417          48.668          1.3242         0.82557
v  Velocity[Z]            -76.545          77.633         -1.6893     -1.5855e-05
v  ǁVelocityǁ           0.0016796          100.11          9.8004          7.7517
v  Pressure           -1.1183e+06      6.0436e+05      3.2107e+05      2.8839e+05
v  k                   7.5357e-06          63.183         0.18421         0.12038
v  epsilon               0.011704      1.1829e+07           16984          142.15
v  TurbVisc           Nb of faces within the viscous sub-layer     :       7493
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14143E+02     115   0.19141E+00   0.16220E+04 0.94742E+03 
c  Velocity[X]                                      0.47436E+03 
c  Velocity[Y]                                      0.44996E+03 
c  Velocity[Z]                                      0.69768E+03 
c  Pressure     0.22207E+00     620   0.57576E-02   0.34168E+00 0.16924E+04 
c  k            0.17046E+01      75   0.72743E-02   0.16260E+02 0.14921E+04 
c  epsilon      0.36449E+05      52   0.60118E-02   0.83701E+10 0.50548E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022361                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.547          51.309          3.2039         0.35503
v  Velocity[Y]            -45.874          41.831          1.3251         0.82511
v  Velocity[Z]            -81.617          71.119         -1.6847      -0.0015389
v  ǁVelocityǁ           0.0017148          96.137          9.7917          7.7597
v  Pressure           -1.1224e+06      6.0171e+05      3.2002e+05      2.8755e+05
v  k         Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14138E+02     115   0.19262E+00   0.15990E+04 0.95462E+03 
c  Velocity[X]                                      0.48755E+03 
c  Velocity[Y]                                      0.47587E+03 
c  Velocity[Z]                                      0.63562E+03 
c  Pressure     0.26119E+00     640   0.62434E-02   0.40063E+00 0.67629E+03 
c  k            0.16812E+01      72   0.81594E-02   0.22476E+02 0.17134E+04 
c  epsilon      0.36229E+05      50   0.75392E-02   0.33661E+11 0.58460E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020364                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.791          58.491          3.2169         0.35419
v  Velocity[Y]            -49.898           50.68          1.3241         0.82498
v  Velocity[Z]            -86.213          146.26         -1.6876     -0.00091709
v  ǁVelocityǁ           0.0016966          153.19          9.7982          7.7554
v  Pressure           -1.1199e+06      6.0293e+05      3.2057e+05      2.8797e+05
v  k                    7.539e-06          70.739          0.1845         0.12054
v  epsilon               0.012116      1.1682e+07           16950           141.9
v  TurbVisc            3.8698e-11         0.73823       0.0045994         0.04835
v  total_pressure     -6.1993e+05      1.1029e+06      8.2057e+05      7.8797e+05


 TIME FOR THE TIME STEP              669:        0.67248E+02

===============================================================


 INSTANT    0.670000000E+03   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         0.754310571E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888875E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34989E+03 0.30863E+02
   Friction velocity        uet   :  0.40957E-01 0.97727E+01
   Friction velocity        uk    :  0.65682E-01 0.75914E+01
   Dimensionless distance   yplus :  0.45863E-03 0.39861E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18666
   Nb of faces within the viscous sub-layer     :       7498
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14142E+02     115   0.19134E+00   0.19585E+04 0.99975E+03 
c  Velocity[X]                                      0.49112E+03 
c  Velocity[Y]                                      0.50227E+03 
c  Velocity[Z]                                      0.96512E+03 
c  Pressure     0.22680E+00     606   0.58577E-02   0.34979E+00 0.44924E+03 
c  k            0.16817E+01      74   0.81492E-02   0.19513E+02 0.15294E+04 
c  epsilon      0.36357E+05      51   0.66518E-02   0.19194E+11 0.11248E+07 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020633                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.664          59.439          3.2104         0.35447
v  Velocity[Y]             -43.65          41.678          1.3253         0.82557
v  Velocity[Z]            -98.508          77.532         -1.6868       -0.001159
v  ǁVelocityǁ           0.0017093          110.32          9.7945           7.757
v  Pressure           -1.1236e+06       6.026e+05      3.2015e+05      2.8759e+05
v  k                   7.6134e-06          69.013         0.18513         0.12087
v  epsilon               0.012536      1   Nb of reversal of the velocity at the wall   :      18642
   Nb of faces within the viscous sub-layer     :       7471
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14184E+02     114   0.19168E+00   0.14998E+04 0.90972E+03 
c  Velocity[X]                                      0.46926E+03 
c  Velocity[Y]                                      0.44521E+03 
c  Velocity[Z]                                      0.58532E+03 
c  Pressure     0.23159E+00     736   0.56414E-02   0.35464E+00 0.30678E+03 
c  k            0.17184E+01      74   0.57147E-02   0.10998E+02 0.11838E+04 
c  epsilon      0.36788E+05      53   0.47685E-02   0.59915E+10 0.72415E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020983                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.537          56.405          3.1917         0.35576
v  Velocity[Y]            -47.469          44.521          1.3242         0.82492
v  Velocity[Z]            -84.699          116.98         -1.6828      -0.0018053
v  ǁVelocityǁ           0.0017216          124.85          9.7888          7.7651
v  Pressure           -1.1284e+   Nb of faces within the viscous sub-layer     :       7493
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14143E+02     115   0.19141E+00   0.16220E+04 0.94742E+03 
c  Velocity[X]                                      0.47436E+03 
c  Velocity[Y]                                      0.44996E+03 
c  Velocity[Z]                                      0.69768E+03 
c  Pressure     0.22207E+00     620   0.57576E-02   0.34168E+00 0.16924E+04 
c  k            0.17046E+01      75   0.72743E-02   0.16260E+02 0.14921E+04 
c  epsilon      0.36449E+05      52   0.60118E-02   0.83701E+10 0.50548E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022361                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.547          51.309          3.2039         0.35503
v  Velocity[Y]            -45.874          41.831          1.3251         0.82511
v  Velocity[Z]            -81.617          71.119         -1.6847      -0.0015389
v  ǁVelocityǁ           0.0017148          96.137          9.7917          7.7597
v  Pressure           -1.1224e+06      6.0171e+05      3.2002e+05      2.8755e+05
v  k                   7.7285e-06          70.491         0.18536         0.12116
v  epsilon               0.012946         1.2e+07           16949          143.93
v  TurbVisc            3.9424e-11          0.7582       0.0046422         0.04839
v  total_pressure     -6.2244e+05      1.1017e+06      8.2002e+05      7.8755e+05


 TIME FOR THE TIME STEP              671:        0.67018E+02

===============================================================


 INSTANT    0.672000000E+03   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.625785814E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10576E+03 0.28782E+02
   Friction velocity        uet   :  0.37193E-01 0.69020E+01
   Friction velocity        uk    :  0.67936E-01 0.75799E+01
   Dimensionless distance   yplus :  0.46172E-03 0.43356E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18656
   Nb of faces within the viscous sub-layer     :       7481
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14174E+02     115   0.19500E+00   0.16226E+04 0.93677E+03 
c  Velocity[X]                                      0.46765E+03 
c  Velocity[Y]                                      0.44489E+03 
c  Velocity[Z]                                      0.71006E+03 
c  Pressure     0.21115E+00     609   0.58542E-02   0.32590E+00 0.79231E+03 
c  k            0.17376E+01      75   0.55834E-02   0.13501E+02 0.12870E+04 
c  epsilon      0.36641E+05      52   0.45322E-02   0.55974E+10 0.31355E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022889                             2
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.074          60.177          3.1974          0.3555
v  Velocity[Y]            -48.121          40.247          1.3257         0.82631
v  Velocity[Z]            -89.007          79.367         -1.6838      -0.0013963
v  ǁVelocityǁ           0.0017193          102.72          9.7898           7.763
v  Pressure           -1.1233e+06      6.0259e+05      3.1998e+05      2.8753e+05
v  k                   7.8006e-06          70.901         0.1859   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18626
   Nb of faces within the viscous sub-layer     :       7444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14187E+02     115   0.19005E+00   0.19400E+04 0.98766E+03 
c  Velocity[X]                                      0.49355E+03 
c  Velocity[Y]                                      0.55469E+03 
c  Velocity[Z]                                      0.89180E+03 
c  Pressure     0.23860E+00     716   0.56375E-02   0.36200E+00 0.61245E+03 
c  k            0.16552E+01      71   0.57821E-02   0.81888E+01 0.13176E+04 
c  epsilon      0.36440E+05      50   0.52911E-02   0.14806E+11 0.11413E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023967                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.121          61.679           3.184         0.35637
v  Velocity[Y]            -45.605          40.145          1.3209         0.82511
v  Velocity[Z]            -115.54          69.078         -1.6815      -0.0023469
v  ǁVelocityǁ           0.0017314          122.71      Nb of reversal of the velocity at the wall   :      18642
   Nb of faces within the viscous sub-layer     :       7471
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14184E+02     114   0.19168E+00   0.14998E+04 0.90972E+03 
c  Velocity[X]                                      0.46926E+03 
c  Velocity[Y]                                      0.44521E+03 
c  Velocity[Z]                                      0.58532E+03 
c  Pressure     0.23159E+00     736   0.56414E-02   0.35464E+00 0.30678E+03 
c  k            0.17184E+01      74   0.57147E-02   0.10998E+02 0.11838E+04 
c  epsilon      0.36788E+05      53   0.47685E-02   0.59915E+10 0.72415E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020983                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.537          56.405          3.1917         0.35576
v  Velocity[Y]            -47.469          44.521          1.3242         0.82492
v  Velocity[Z]            -84.699          116.98         -1.6828      -0.0018053
v  ǁVelocityǁ           0.0017216          124.85          9.7888          7.7651
v  Pressure           -1.1284e+06      6.0167e+05      3.1982e+05      2.8739e+05
v  k                   7.9507e-06          64.734         0.18625         0.12176
v  epsilon               0.014007      1.1878e+07           16929          145.63
v  TurbVisc            3.6457e-11         0.74164       0.0046936        0.048436
v  total_pressure     -6.2836e+05      1.1017e+06      8.1982e+05      7.8739e+05


 TIME FOR THE TIME STEP              673:        0.65287E+02

===============================================================


 INSTANT    0.674000000E+03   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.713563139E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
----------------------------   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18626
   Nb of faces within the viscous sub-layer     :       7444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14187E+02     115   0.19005E+00   0.19400E+04 0.98766E+03 
c  Velocity[X]                                      0.49355E+03 
c  Velocity[Y]                                      0.55469E+03 
c  Velocity[Z]                                      0.89180E+03 
c  Pressure     0.23860E+00     716   0.56375E-02   0.36200E+00 0.61245E+03 
c  k            0.16552E+01      71   0.57821E-02   0.81888E+01 0.13176E+04 
c  epsilon      0.36440E+05      50   0.52911E-02   0.14806E+11 0.11413E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023967                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.121          61.679           3.184         0.35637
v  Velocity[Y]            -45.605          40.145          1.3209         0.82511
v  Velocity[Z]            -115.54          69.078         -1.6815      -0.0023469
v  ǁVelocityǁ           0.0017314          122.71          9.7874          7.7686
v  Pressure           -1.1282e+06      5.9972e+05      3.1891e+05      2.8667e+05
v  k                   8.4113e-06           60.89         0.18698         0.12212
v  epsilon               0.015397      1.1844e+07           16926          145.33
v  TurbVisc            3.9712e-11         0.63692       0.0047581        0.048484
v  total_pressure     -6.2819e+05      1.0997e+06      8.1891e+05      7.8667e+05


 TIME FOR THE TIME STEP              675:        0.68907E+02

===============================================================


 INSTANT    0.676000000E+03   TIME STEP NUMBER             676
 ================================   Dimensionless distance   yplus :  0.46507E-03 0.42910E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18628
   Nb of faces within the viscous sub-layer     :       7419
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14203E+02     113   0.19175E+00   0.14953E+04 0.92601E+03 
c  Velocity[X]                                      0.47211E+03 
c  Velocity[Y]                                      0.43394E+03 
c  Velocity[Z]                                      0.58930E+03 
c  Pressure     0.21953E+00     899   0.53081E-02   0.33741E+00 0.11936E+04 
c  k            0.16236E+01      70   0.49702E-02   0.77001E+01 0.12652E+04 
c  epsilon      0.35927E+05      47   0.50314E-02   0.36583E+11 0.15389E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021912                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.908          58.991          3.1824          0.3575
v  Velocity[Y]            -44.507          56.512          1.3152         0.82446
v  Velocity[Z]            -96.797          78.132         -1.6802      -0.0017   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18626
   Nb of faces within the viscous sub-layer     :       7444
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14187E+02     115   0.19005E+00   0.19400E+04 0.98766E+03 
c  Velocity[X]                                      0.49355E+03 
c  Velocity[Y]                                      0.55469E+03 
c  Velocity[Z]                                      0.89180E+03 
c  Pressure     0.23860E+00     716   0.56375E-02   0.36200E+00 0.61245E+03 
c  k            0.16552E+01      71   0.57821E-02   0.81888E+01 0.13176E+04 
c  epsilon      0.36440E+05      50   0.52911E-02   0.14806E+11 0.11413E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023967                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.121          61.679           3.184         0.35637
v  Velocity[Y]            -45.605          40.145          1.3209         0.82511
v  Velocity[Z]            -115.54          69.078         -1.6815      -0.0023469
v  ǁVelocityǁ           0.0017314          122.71          9.7874          7.7686
v  Pressure           -1.1282e+06      5.9972e+05      3.1891e+05      2.8667e+05
v  k                   8.4113e-06           60.89         0.18698         0.12212
v  epsilon               0.015397      1.1844e+07           16926          145.33
v  TurbVisc            3.9712e-11         0.63692       0.0047581        0.048484
v  total_pressure     -6.2819e+05      1.0997e+06      8.1891e+05      7.8667e+05


 TIME FOR THE TIME STEP              675:        0.72043E+02

===============================================================


 INSTANT    0.676000000E+03   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.432750807E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1       Dimensionless distance   yplus :  0.46507E-03 0.42910E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18628
   Nb of faces within the viscous sub-layer     :       7419
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14203E+02     113   0.19175E+00   0.14953E+04 0.92601E+03 
c  Velocity[X]                                      0.47211E+03 
c  Velocity[Y]                                      0.43394E+03 
c  Velocity[Z]                                      0.58930E+03 
c  Pressure     0.21953E+00     899   0.53081E-02   0.33741E+00 0.11936E+04 
c  k            0.16236E+01      70   0.49702E-02   0.77001E+01 0.12652E+04 
c  epsilon      0.35927E+05      47   0.50314E-02   0.36583E+11 0.15389E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021912                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.908          58.991          3.1824          0.3575
v  Velocity[Y]            -44.507          56.512          1.3152         0.82446
v  Velocity[Z]            -96.797          78.132         -1.6802      -0.0017765
v  ǁVelocityǁ           0.0017367           111.8          9.7883          7.7716
v  Pressure           -1.1316e+06      5.9763e+05      3.1824e+05      2.8622e+05
v  k                   8.9394e-06          60.336         0.18774         0.12235
v  epsilon               0.016835      1.1991e+07           17043           143.9
v  TurbVisc            3.9897e-11         0.62182       0.0048307        0.048532
v  total_pressure     -6.3157e+05      1.0976e+06      8.1824e+05      7.8622e+05


 TIME FOR THE TIME STEP              677:        0.84777E+02

===============================================================


 INSTANT    0.678000000E+03   TIME    Friction velocity        uk    :  0.65577E-01 0.75263E+01
   Dimensionless distance   yplus :  0.46567E-03 0.39518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18636
   Nb of faces within the viscous sub-layer     :       7412
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     113   0.19028E+00   0.16024E+04 0.93425E+03 
c  Velocity[X]                                      0.46759E+03 
c  Velocity[Y]                                      0.48045E+03 
c  Velocity[Z]                                      0.65433E+03 
c  Pressure     0.20174E+00     697   0.54050E-02   0.31171E+00 0.57972E+03 
c  k            0.16395E+01      71   0.59327E-02   0.82228E+01 0.12451E+04 
c  epsilon      0.36036E+05      49   0.50849E-02   0.10460E+11 0.97450E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026424                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.216          50.333           3.189         0.35829
v  Velocity[Y]            -47.211          40.084          1.3091         0.82433
v  Velocity[Z]      Dimensionless distance   yplus :  0.46507E-03 0.42910E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18628
   Nb of faces within the viscous sub-layer     :       7419
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14203E+02     113   0.19175E+00   0.14953E+04 0.92601E+03 
c  Velocity[X]                                      0.47211E+03 
c  Velocity[Y]                                      0.43394E+03 
c  Velocity[Z]                                      0.58930E+03 
c  Pressure     0.21953E+00     899   0.53081E-02   0.33741E+00 0.11936E+04 
c  k            0.16236E+01      70   0.49702E-02   0.77001E+01 0.12652E+04 
c  epsilon      0.35927E+05      47   0.50314E-02   0.36583E+11 0.15389E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021912                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.908          58.991          3.1824          0.3575
v  Velocity[Y]            -44.507          56.512          1.3152         0.82446
v  Velocity[Z]            -96.797          78.132         -1.6802      -0.0017765
v  ǁVelocityǁ           0.0017367           111.8          9.7883          7.7716
v  Pressure           -1.1316e+06      5.9763e+05      3.1824e+05      2.8622e+05
v  k                   8.9394e-06          60.336         0.18774         0.12235
v  epsilon               0.016835      1.1991e+07           17043           143.9
v  TurbVisc            3.9897e-11         0.62182       0.0048307        0.048532
v  total_pressure     -6.3157e+05      1.0976e+06      8.1824e+05      7.8622e+05


 TIME FOR THE TIME STEP              677:        0.71166E+02

===============================================================


 INSTANT    0.678000000E+03   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.696315784E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888863E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14          Friction velocity        uk    :  0.65577E-01 0.75263E+01
   Dimensionless distance   yplus :  0.46567E-03 0.39518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18636
   Nb of faces within the viscous sub-layer     :       7412
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     113   0.19028E+00   0.16024E+04 0.93425E+03 
c  Velocity[X]                                      0.46759E+03 
c  Velocity[Y]                                      0.48045E+03 
c  Velocity[Z]                                      0.65433E+03 
c  Pressure     0.20174E+00     697   0.54050E-02   0.31171E+00 0.57972E+03 
c  k            0.16395E+01      71   0.59327E-02   0.82228E+01 0.12451E+04 
c  epsilon      0.36036E+05      49   0.50849E-02   0.10460E+11 0.97450E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026424                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.216          50.333           3.189         0.35829
v  Velocity[Y]            -47.211          40.084          1.3091         0.82433
v  Velocity[Z]            -79.801          83.666         -1.6772     -0.00077907
v  ǁVelocityǁ           0.0017416          91.841          9.7961          7.7732
v  Pressure           -1.1271e+06      5.9979e+05      3.1725e+05      2.8546e+05
v  k                   9.6021e-06          60.012         0.18884         0.12287
v  epsilon               0.018155      1.1914e+07           17109          144.49
v  TurbVisc            4.0006e-11         0.63891       0.0049135        0.048583
v  total_pressure     -6.2709e+05      1.0998e+06      8.1725e+05      7.8546e+05


 TIME FOR THE TIME STEP              679:        0.67725E+02

========================================   Friction velocity        uet   :  0.40360E-01 0.80597E+01
   Friction velocity        uk    :  0.49757E-01 0.75401E+01
   Dimensionless distance   yplus :  0.46390E-03 0.38518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18642
   Nb of faces within the viscous sub-layer     :       7400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14162E+02     113   0.18806E+00   0.16953E+04 0.94908E+03 
c  Velocity[X]                                      0.45148E+03 
c  Velocity[Y]                                      0.50407E+03 
c  Velocity[Z]                                      0.73976E+03 
c  Pressure     0.20037E+00     663   0.50519E-02   0.30850E+00 0.51580E+03 
c  k            0.16463E+01      74   0.42984E-02   0.75607E+01 0.10001E+04 
c  epsilon      0.35945E+05      53   0.33622E-02   0.32153E+10 0.15928E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023528                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.59           51.23          3.2021         0.35958
v  Velocity[Y]            -43.284        Friction velocity        uk    :  0.65577E-01 0.75263E+01
   Dimensionless distance   yplus :  0.46567E-03 0.39518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18636
   Nb of faces within the viscous sub-layer     :       7412
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     113   0.19028E+00   0.16024E+04 0.93425E+03 
c  Velocity[X]                                      0.46759E+03 
c  Velocity[Y]                                      0.48045E+03 
c  Velocity[Z]                                      0.65433E+03 
c  Pressure     0.20174E+00     697   0.54050E-02   0.31171E+00 0.57972E+03 
c  k            0.16395E+01      71   0.59327E-02   0.82228E+01 0.12451E+04 
c  epsilon      0.36036E+05      49   0.50849E-02   0.10460E+11 0.97450E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026424                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.216          50.333           3.189         0.35829
v  Velocity[Y]            -47.211          40.084          1.3091         0.82433
v  Velocity[Z]            -79.801          83.666         -1.6772     -0.00077907
v  ǁVelocityǁ           0.0017416          91.841          9.7961          7.7732
v  Pressure           -1.1271e+06      5.9979e+05      3.1725e+05      2.8546e+05
v  k                   9.6021e-06          60.012         0.18884         0.12287
v  epsilon               0.018155      1.1914e+07           17109          144.49
v  TurbVisc            4.0006e-11         0.63891       0.0049135        0.048583
v  total_pressure     -6.2709e+05      1.0998e+06      8.1725e+05      7.8546e+05


 TIME FOR THE TIME STEP              679:        0.76911E+02

===============================================================


 INSTANT    0.680000000E+03   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        -0.215729956E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15             Friction velocity        uet   :  0.40360E-01 0.80597E+01
   Friction velocity        uk    :  0.49757E-01 0.75401E+01
   Dimensionless distance   yplus :  0.46390E-03 0.38518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18642
   Nb of faces within the viscous sub-layer     :       7400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14162E+02     113   0.18806E+00   0.16953E+04 0.94908E+03 
c  Velocity[X]                                      0.45148E+03 
c  Velocity[Y]                                      0.50407E+03 
c  Velocity[Z]                                      0.73976E+03 
c  Pressure     0.20037E+00     663   0.50519E-02   0.30850E+00 0.51580E+03 
c  k            0.16463E+01      74   0.42984E-02   0.75607E+01 0.10001E+04 
c  epsilon      0.35945E+05      53   0.33622E-02   0.32153E+10 0.15928E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023528                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.59           51.23          3.2021         0.35958
v  Velocity[Y]            -43.284           46.62          1.3042          0.8243
v  Velocity[Z]            -78.002            80.6          -1.674     -0.00078778
v  ǁVelocityǁ           0.0017401          91.023          9.8082          7.7763
v  Pressure           -1.1277e+06      5.9835e+05      3.1726e+05      2.8547e+05
v  k                   1.0417e-05          62.547         0.19022         0.12349
v  epsilon               0.019893      1.1967e+07           17145          145.35
v  TurbVisc            3.9659e-11         0.63439       0.0050084        0.048639
v  total_pressure     -6.2768e+05      1.0983e+06      8.1726e+05      7.8547e+05


 TIME FOR THE TIME STEP              681:   Rel velocity at the wall uiptn : -0.20761E+03 0.27017E+02
   Friction velocity        uet   :  0.41403E-01 0.73577E+01
   Friction velocity        uk    :  0.68867E-01 0.75584E+01
   Dimensionless distance   yplus :  0.46352E-03 0.39928E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18680
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14182E+02     113   0.19377E+00   0.15573E+04 0.92276E+03 
c  Velocity[X]                                      0.45311E+03 
c  Velocity[Y]                                      0.42813E+03 
c  Velocity[Z]                                      0.67609E+03 
c  Pressure     0.21128E+00     694   0.48010E-02   0.32604E+00 0.54431E+03 
c  k            0.17538E+01      76   0.58197E-02   0.12714E+02 0.13387E+04 
c  epsilon      0.36620E+05      57   0.51547E-02   0.19477E+11 0.11836E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023136                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.191          57.636             Friction velocity        uet   :  0.40360E-01 0.80597E+01
   Friction velocity        uk    :  0.49757E-01 0.75401E+01
   Dimensionless distance   yplus :  0.46390E-03 0.38518E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18642
   Nb of faces within the viscous sub-layer     :       7400
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14162E+02     113   0.18806E+00   0.16953E+04 0.94908E+03 
c  Velocity[X]                                      0.45148E+03 
c  Velocity[Y]                                      0.50407E+03 
c  Velocity[Z]                                      0.73976E+03 
c  Pressure     0.20037E+00     663   0.50519E-02   0.30850E+00 0.51580E+03 
c  k            0.16463E+01      74   0.42984E-02   0.75607E+01 0.10001E+04 
c  epsilon      0.35945E+05      53   0.33622E-02   0.32153E+10 0.15928E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023528                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.59           51.23          3.2021         0.35958
v  Velocity[Y]            -43.284           46.62          1.3042          0.8243
v  Velocity[Z]            -78.002            80.6          -1.674     -0.00078778
v  ǁVelocityǁ           0.0017401          91.023          9.8082          7.7763
v  Pressure           -1.1277e+06      5.9835e+05      3.1726e+05      2.8547e+05
v  k                   1.0417e-05          62.547         0.19022         0.12349
v  epsilon               0.019893      1.1967e+07           17145          145.35
v  TurbVisc            3.9659e-11         0.63439       0.0050084        0.048639
v  total_pressure     -6.2768e+05      1.0983e+06      8.1726e+05      7.8547e+05


 TIME FOR THE TIME STEP              681:        0.62625E+02

===============================================================


 INSTANT    0.682000000E+03   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.283017088E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888873E+01
Free inlet               13           0    Rel velocity at the wall uiptn : -0.20761E+03 0.27017E+02
   Friction velocity        uet   :  0.41403E-01 0.73577E+01
   Friction velocity        uk    :  0.68867E-01 0.75584E+01
   Dimensionless distance   yplus :  0.46352E-03 0.39928E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18680
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14182E+02     113   0.19377E+00   0.15573E+04 0.92276E+03 
c  Velocity[X]                                      0.45311E+03 
c  Velocity[Y]                                      0.42813E+03 
c  Velocity[Z]                                      0.67609E+03 
c  Pressure     0.21128E+00     694   0.48010E-02   0.32604E+00 0.54431E+03 
c  k            0.17538E+01      76   0.58197E-02   0.12714E+02 0.13387E+04 
c  epsilon      0.36620E+05      57   0.51547E-02   0.19477E+11 0.11836E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023136                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.191          57.636          3.2169         0.36015
v  Velocity[Y]            -44.882          48.784          1.3021         0.82476
v  Velocity[Z]            -91.207          74.327         -1.6729     -0.00082403
v  ǁVelocityǁ           0.0016933          106.92          9.8198          7.7777
v  Pressure           -1.1318e+06      5.9868e+05      3.1753e+05      2.8563e+05
v  k                   1.1391e-05            69.7           0.192         0.12456
v  epsilon               0.021887      1.2011e+07           17198          148.24
v  TurbVisc            3.9023e-11         0.68769       0.0051152        0.048707
v  total_pressure     -6.3183e+05      1.0987e+06      8.1753e+0------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14685E+03 0.26476E+02
   Friction velocity        uet   :  0.38345E-01 0.75148E+01
   Friction velocity        uk    :  0.57303E-01 0.75435E+01
   Dimensionless distance   yplus :  0.45764E-03 0.40820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18701
   Nb of faces within the viscous sub-layer     :       7406
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     114   0.19121E+00   0.15161E+04 0.92721E+03 
c  Velocity[X]                                      0.45276E+03 
c  Velocity[Y]                                      0.45749E+03 
c  Velocity[Z]                                      0.60582E+03 
c  Pressure     0.20047E+00     682   0.49601E-02   0.30774E+00 0.84982E+03 
c  k            0.18885E+01      77   0.91459E-02   0.41507E+02 0.21108E+04 
c  epsilon      0.37900E+05      58   0.71648E-02   0.11990E+11 0.99837E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021053                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  -------------   Rel velocity at the wall uiptn : -0.20761E+03 0.27017E+02
   Friction velocity        uet   :  0.41403E-01 0.73577E+01
   Friction velocity        uk    :  0.68867E-01 0.75584E+01
   Dimensionless distance   yplus :  0.46352E-03 0.39928E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18680
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14182E+02     113   0.19377E+00   0.15573E+04 0.92276E+03 
c  Velocity[X]                                      0.45311E+03 
c  Velocity[Y]                                      0.42813E+03 
c  Velocity[Z]                                      0.67609E+03 
c  Pressure     0.21128E+00     694   0.48010E-02   0.32604E+00 0.54431E+03 
c  k            0.17538E+01      76   0.58197E-02   0.12714E+02 0.13387E+04 
c  epsilon      0.36620E+05      57   0.51547E-02   0.19477E+11 0.11836E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023136                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.191          57.636          3.2169         0.36015
v  Velocity[Y]            -44.882          48.784          1.3021         0.82476
v  Velocity[Z]            -91.207          74.327         -1.6729     -0.00082403
v  ǁVelocityǁ           0.0016933          106.92          9.8198          7.7777
v  Pressure           -1.1318e+06      5.9868e+05      3.1753e+05      2.8563e+05
v  k                   1.1391e-05            69.7           0.192         0.12456
v  epsilon               0.021887      1.2011e+07           17198          148.24
v  TurbVisc            3.9023e-11         0.68769       0.0051152        0.048707
v  total_pressure     -6.3183e+05      1.0987e+06      8.1753e+05      7.8563e+05


 TIME FOR THE TIME STEP              683:        0.75016E+02

===============================================================


 INSTANT    0.684000000E+03   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.188674905E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46    ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14685E+03 0.26476E+02
   Friction velocity        uet   :  0.38345E-01 0.75148E+01
   Friction velocity        uk    :  0.57303E-01 0.75435E+01
   Dimensionless distance   yplus :  0.45764E-03 0.40820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18701
   Nb of faces within the viscous sub-layer     :       7406
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     114   0.19121E+00   0.15161E+04 0.92721E+03 
c  Velocity[X]                                      0.45276E+03 
c  Velocity[Y]                                      0.45749E+03 
c  Velocity[Z]                                      0.60582E+03 
c  Pressure     0.20047E+00     682   0.49601E-02   0.30774E+00 0.84982E+03 
c  k            0.18885E+01      77   0.91459E-02   0.41507E+02 0.21108E+04 
c  epsilon      0.37900E+05      58   0.71648E-02   0.11990E+11 0.99837E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021053                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.109          52.463          3.2301         0.36095
v  Velocity[Y]             -45.05          62.646          1.3043         0.82561
v  Velocity[Z]            -95.219          70.524         -1.6737      -0.0013105
v  ǁVelocityǁ           0.0016744          107.77          9.8319            7.78
v  Pressure           -1.1269e+06      6.0023e+05      3.1821e+05      2.8609e+05
v  k                   1.2479e-05          75.505         0.19365          0.1256
v  epsilon               0.024327      1.2073e+07           17253          150.94
v  TurbVisc            3.8538e-11            0.75       0.0052292        0.048791
v                                           Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11115E+03 0.42375E+02
   Friction velocity        uet   :  0.38613E-01 0.77762E+01
   Friction velocity        uk    :  0.67968E-01 0.75441E+01
   Dimensionless distance   yplus :  0.45645E-03 0.40772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14168E+02     114   0.19080E+00   0.14081E+04 0.89549E+03 
c  Velocity[X]                                      0.44113E+03 
c  Velocity[Y]                                      0.43997E+03 
c  Velocity[Z]                                      0.52697E+03 
c  Pressure     0.17677E+00     695   0.50471E-02   0.27168E+00 0.18304E+04 
c  k            0.20794E+01      77   0.11806E-01   0.60280E+02 0.25622E+04 
c  epsilon      0.39831E+05      57   0.95623E-02   0.11556E+11 0.10307E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023815                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  ------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14685E+03 0.26476E+02
   Friction velocity        uet   :  0.38345E-01 0.75148E+01
   Friction velocity        uk    :  0.57303E-01 0.75435E+01
   Dimensionless distance   yplus :  0.45764E-03 0.40820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18701
   Nb of faces within the viscous sub-layer     :       7406
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     114   0.19121E+00   0.15161E+04 0.92721E+03 
c  Velocity[X]                                      0.45276E+03 
c  Velocity[Y]                                      0.45749E+03 
c  Velocity[Z]                                      0.60582E+03 
c  Pressure     0.20047E+00     682   0.49601E-02   0.30774E+00 0.84982E+03 
c  k            0.18885E+01      77   0.91459E-02   0.41507E+02 0.21108E+04 
c  epsilon      0.37900E+05      58   0.71648E-02   0.11990E+11 0.99837E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021053                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.109          52.463          3.2301         0.36095
v  Velocity[Y]             -45.05          62.646          1.3043         0.82561
v  Velocity[Z]            -95.219          70.524         -1.6737      -0.0013105
v  ǁVelocityǁ           0.0016744          107.77          9.8319            7.78
v  Pressure           -1.1269e+06      6.0023e+05      3.1821e+05      2.8609e+05
v  k                   1.2479e-05          75.505         0.19365          0.1256
v  epsilon               0.024327      1.2073e+07           17253          150.94
v  TurbVisc            3.8538e-11            0.75       0.0052292        0.048791
v  total_pressure     -6.2686e+05      1.1002e+06      8.1821e+05      7.8609e+05


 TIME FOR THE TIME STEP              685:        0.77849E+02

===============================================================


 INSTANT    0.686000000E+03   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        -0.526165020E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0                                                Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11115E+03 0.42375E+02
   Friction velocity        uet   :  0.38613E-01 0.77762E+01
   Friction velocity        uk    :  0.67968E-01 0.75441E+01
   Dimensionless distance   yplus :  0.45645E-03 0.40772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14168E+02     114   0.19080E+00   0.14081E+04 0.89549E+03 
c  Velocity[X]                                      0.44113E+03 
c  Velocity[Y]                                      0.43997E+03 
c  Velocity[Z]                                      0.52697E+03 
c  Pressure     0.17677E+00     695   0.50471E-02   0.27168E+00 0.18304E+04 
c  k            0.20794E+01      77   0.11806E-01   0.60280E+02 0.25622E+04 
c  epsilon      0.39831E+05      57   0.95623E-02   0.11556E+11 0.10307E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023815                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.298          54.066           3.241         0.36112
v  Velocity[Y]            -45.806          43.987          1.3072         0.82558
v  Velocity[Z]            -93.964          71.284         -1.6745     -0.00090206
v  ǁVelocityǁ           0.0016699          105.77          9.8436          7.7815
v  Pressure           -1.1234e+06      6.0439e+05       3.196e+05       2.871e+05
v  k                    1.356e-05          79.875         0.19527         0.12645
v  epsilon               0.027112      1.1951e+07           17244          152.84
v  TurbVisc            3------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17607E+03 0.34657E+02
   Friction velocity        uet   :  0.40405E-01 0.72986E+01
   Friction velocity        uk    :  0.67702E-01 0.75517E+01
   Dimensionless distance   yplus :  0.45564E-03 0.42882E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18671
   Nb of faces within the viscous sub-layer     :       7388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     115   0.19046E+00   0.16159E+04 0.93206E+03 
c  Velocity[X]                                      0.47172E+03 
c  Velocity[Y]                                      0.43085E+03 
c  Velocity[Z]                                      0.71330E+03 
c  Pressure     0.18735E+00     605   0.51292E-02   0.28833E+00 0.60036E+03 
c  k            0.19223E+01      79   0.14272E-01   0.94368E+02 0.35535E+04 
c  epsilon      0.39506E+05      55   0.11460E-01   0.95135E+10 0.95122E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022663                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum                                                Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11115E+03 0.42375E+02
   Friction velocity        uet   :  0.38613E-01 0.77762E+01
   Friction velocity        uk    :  0.67968E-01 0.75441E+01
   Dimensionless distance   yplus :  0.45645E-03 0.40772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14168E+02     114   0.19080E+00   0.14081E+04 0.89549E+03 
c  Velocity[X]                                      0.44113E+03 
c  Velocity[Y]                                      0.43997E+03 
c  Velocity[Z]                                      0.52697E+03 
c  Pressure     0.17677E+00     695   0.50471E-02   0.27168E+00 0.18304E+04 
c  k            0.20794E+01      77   0.11806E-01   0.60280E+02 0.25622E+04 
c  epsilon      0.39831E+05      57   0.95623E-02   0.11556E+11 0.10307E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023815                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.298          54.066           3.241         0.36112
v  Velocity[Y]            -45.806          43.987          1.3072         0.82558
v  Velocity[Z]            -93.964          71.284         -1.6745     -0.00090206
v  ǁVelocityǁ           0.0016699          105.77          9.8436          7.7815
v  Pressure           -1.1234e+06      6.0439e+05       3.196e+05       2.871e+05
v  k                    1.356e-05          79.875         0.19527         0.12645
v  epsilon               0.027112      1.1951e+07           17244          152.84
v  TurbVisc            3.8374e-11         0.75995       0.0053431        0.048878
v  total_pressure      -6.234e+05      1.1044e+06       8.196e+05       7.871e+05


 TIME FOR THE TIME STEP              687:        0.66459E+02

===============================================================


 INSTANT    0.688000000E+03   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.224785382E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888868E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10585E+03 0.51818E+02
   Friction velocity        uet   :  0.36964E-01 0.76915E+01
   Friction velocity        uk    :  0.60215E-01 0.75909E+01
   Dimensionless distance   yplus :  0.45559E-03 0.41141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18687
   Nb of faces within the viscous sub-layer     :       7385
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14161E+02     114   0.19094E+00   0.15364E+04 0.92705E+03 
c  Velocity[X]                                      0.44889E+03 
c  Velocity[Y]                                      0.46229E+03 
c  Velocity[Z]                                      0.62525E+03 
c  Pressure     0.17691E+00     790   0.50659E-02   0.27135E+00 0.57292E+03 
c  k            0.20347E+01      78   0.13727E-01   0.91058E+02 0.33470E+04 
c  epsilon      0.39923E+05      56   0.11563E-01   0.19602E+11 0.92774E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023432                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  ----------   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12891E+03 0.31124E+02
   Friction velocity        uet   :  0.29894E-02 0.75259E+01
   Friction velocity        uk    :  0.69207E-01 0.75545E+01
   Dimensionless distance   yplus :  0.45263E-03 0.36538E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18669
   Nb of faces within the viscous sub-layer     :       7365
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     115   0.19088E+00   0.14262E+04 0.90549E+03 
c  Velocity[X]                                      0.42185E+03 
c  Velocity[Y]                                      0.45922E+03 
c  Velocity[Z]                                      0.54509E+03 
c  Pressure     0.18293E+00     603   0.50104E-02   0.27954E+00 0.12088E+04 
c  k            0.17282E+01      81   0.10235E-01   0.32422E+02 0.23533E+04 
c  epsilon      0.38179E+05      58   0.85313E-02   0.11069E+11 0.21693E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024512                             1
a  epsilon


  ** Computed fields on cells
     -----------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17607E+03 0.34657E+02
   Friction velocity        uet   :  0.40405E-01 0.72986E+01
   Friction velocity        uk    :  0.67702E-01 0.75517E+01
   Dimensionless distance   yplus :  0.45564E-03 0.42882E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18671
   Nb of faces within the viscous sub-layer     :       7388
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     115   0.19046E+00   0.16159E+04 0.93206E+03 
c  Velocity[X]                                      0.47172E+03 
c  Velocity[Y]                                      0.43085E+03 
c  Velocity[Z]                                      0.71330E+03 
c  Pressure     0.18735E+00     605   0.51292E-02   0.28833E+00 0.60036E+03 
c  k            0.19223E+01      79   0.14272E-01   0.94368E+02 0.35535E+04 
c  epsilon      0.39506E+05      55   0.11460E-01   0.95135E+10 0.95122E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022663                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.785          52.485          3.2519         0.36176
v  Velocity[Y]            -41.701          46.337          1.3086         0.82588
v  Velocity[Z]            -90.481          68.192         -1.6757     -0.00088054
v  ǁVelocityǁ           0.0016489          103.57          9.8528          7.7845
v  Pressure           -1.1187e+06      6.0569e+05       3.205e+05      2.8784e+05
v  k                   1.4449e-05          59.389         0.19669         0.12685
v  epsilon               0.029868      1.1982e+07           17262          151.56
v  TurbVisc            3.8078e-11         0.63819       0.0054598        0.048965
v  total_pressure     -6.1872e+05      1.1057e+06       8.205e+05      7.8784e+05


 TIME FOR THE TIME STEP              689:        0.74162E+02

===============================================================


 INSTANT    0.690000000E+03   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        -0.134069086E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888903E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.90315E+02 0.32121E+02
   Friction velocity        uet   :  0.23022E-01 0.76220E+01
   Friction velocity        uk    :  0.67386E-01 0.76058E+01
   Dimensionless distance   yplus :  0.45305E-03 0.38810E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18666
   Nb of faces within the viscous sub-layer     :       7380
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14169E+02     115   0.19097E+00   0.14965E+04 0.93125E+03 
c  Velocity[X]                                      0.46642E+03 
c  Velocity[Y]                                      0.44382E+03 
c  Velocity[Z]                                      0.58626E+03 
c  Pressure     0.18480E+00     628   0.49056E-02   0.28211E+00 0.51539E+03 
c  k            0.17846E+01      81   0.13620E-01   0.59397E+02 0.29905E+04 
c  epsilon      0.38508E+05      57   0.11267E-01   0.13717E+11 0.14252E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022672                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35389E+03 0.35100E+02
   Friction velocity        uet   :  0.37561E-01 0.99912E+01
   Friction velocity        uk    :  0.41293E-01 0.75499E+01
   Dimensionless distance   yplus :  0.45380E-03 0.37740E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18676
   Nb of faces within the viscous sub-layer     :       7365
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14188E+02     114   0.19396E+00   0.17682E+04 0.94496E+03 
c  Velocity[X]                                      0.47739E+03 
c  Velocity[Y]                                      0.49398E+03 
c  Velocity[Z]                                      0.79685E+03 
c  Pressure     0.19827E+00     676   0.61571E-02   0.30253E+00 0.91001E+03 
c  k            0.17154E+01      80   0.56142E-02   0.10665E+02 0.13928E+04 
c  epsilon      0.37971E+05      58   0.45405E-02   0.38540E+10 0.95450E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.00219   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12891E+03 0.31124E+02
   Friction velocity        uet   :  0.29894E-02 0.75259E+01
   Friction velocity        uk    :  0.69207E-01 0.75545E+01
   Dimensionless distance   yplus :  0.45263E-03 0.36538E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18669
   Nb of faces within the viscous sub-layer     :       7365
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     115   0.19088E+00   0.14262E+04 0.90549E+03 
c  Velocity[X]                                      0.42185E+03 
c  Velocity[Y]                                      0.45922E+03 
c  Velocity[Z]                                      0.54509E+03 
c  Pressure     0.18293E+00     603   0.50104E-02   0.27954E+00 0.12088E+04 
c  k            0.17282E+01      81   0.10235E-01   0.32422E+02 0.23533E+04 
c  epsilon      0.38179E+05      58   0.85313E-02   0.11069E+11 0.21693E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024512                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.965          51.826           3.261         0.36093
v  Velocity[Y]            -47.144          60.121          1.3054         0.82671
v  Velocity[Z]            -85.993           69.79         -1.6748     -0.00038381
v  ǁVelocityǁ           0.0016508          96.989           9.858          7.7851
v  Pressure           -1.1133e+06      6.0776e+05      3.2057e+05      2.8812e+05
v  k                   1.5032e-05          64.943         0.19796         0.12705
v  epsilon               0.029373      1.2029e+07           17264          148.43
v  TurbVisc            3.7922e-11         0.64873       0.0055693        0.049041
v  total_pressure     -6.1327e+05      1.1078e+06      8.2057e+05      7.8812e+05


 TIME FOR THE TIME STEP              691:        0.67442E+02

===============================================================


 INSTANT    0.692000000E+03   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        -0.382411666E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888874E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11424E+03 0.43495E+02
   Friction velocity        uet   :  0.35377E-01 0.71726E+01
   Friction velocity        uk    :  0.60580E-01 0.75687E+01
   Dimensionless distance   yplus :  0.45285E-03 0.38823E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18644
   Nb of faces within the viscous sub-layer     :       7389
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14175E+02     114   0.19357E+00   0.15709E+04 0.91742E+03 
c  Velocity[X]                                      0.47610E+03 
c  Velocity[Y]                                      0.49684E+03 
c  Velocity[Z]                                      0.59796E+03 
c  Pressure     0.21287E+00     862   0.53155E-02   0.32434E+00 0.59139E+03 
c  k            0.17038E+01      81   0.73896E-02   0.20795E+02 0.19472E+04 
c  epsilon      0.37887E+05      59   0.57797E-02   0.37210E+10 0.13273E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023103                             1
a  epsilon


  ** Computed fields on cells
     -----------------------Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11333E+03 0.35897E+02
   Friction velocity        uet   :  0.39899E-01 0.71146E+01
   Friction velocity        uk    :  0.47410E-01 0.75424E+01
   Dimensionless distance   yplus :  0.45478E-03 0.39183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18621
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14195E+02     114   0.19241E+00   0.14492E+04 0.89969E+03 
c  Velocity[X]                                      0.45979E+03 
c  Velocity[Y]                                      0.44430E+03 
c  Velocity[Z]                                      0.54507E+03 
c  Pressure     0.18517E+00     802   0.57735E-02   0.28601E+00 0.92921E+03 
c  k            0.16625E+01      78   0.61756E-02   0.98073E+01 0.13801E+04 
c  epsilon      0.37513E+05      56   0.45187E-02   0.48956E+10 0.10643E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  ----------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35389E+03 0.35100E+02
   Friction velocity        uet   :  0.37561E-01 0.99912E+01
   Friction velocity        uk    :  0.41293E-01 0.75499E+01
   Dimensionless distance   yplus :  0.45380E-03 0.37740E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18676
   Nb of faces within the viscous sub-layer     :       7365
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14188E+02     114   0.19396E+00   0.17682E+04 0.94496E+03 
c  Velocity[X]                                      0.47739E+03 
c  Velocity[Y]                                      0.49398E+03 
c  Velocity[Z]                                      0.79685E+03 
c  Pressure     0.19827E+00     676   0.61571E-02   0.30253E+00 0.91001E+03 
c  k            0.17154E+01      80   0.56142E-02   0.10665E+02 0.13928E+04 
c  epsilon      0.37971E+05      58   0.45405E-02   0.38540E+10 0.95450E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021992                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.622          51.891          3.2689         0.36255
v  Velocity[Y]            -42.725          69.705          1.2962         0.82628
v  Velocity[Z]            -83.083          72.698         -1.6703     -0.00084912
v  ǁVelocityǁ           0.0016557          95.023          9.8572          7.7855
v  Pressure           -1.1097e+06      6.0882e+05      3.2094e+05      2.8851e+05
v  k                   1.5337e-05          64.849         0.19942         0.12765
v  epsilon               0.028336      1.2038e+07           17260          147.85
v  TurbVisc            3.8007e-11         0.59276       0.0056747        0.049121
v  total_pressure     -6.0966e+05      1.1088e+06      8.2094e+05      7.8851e+05


 TIME FOR THE TIME STEP              693:        0.69389E+02

===============================================================


 INSTANT    0.694000000E+03   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------------------------Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11333E+03 0.35897E+02
   Friction velocity        uet   :  0.39899E-01 0.71146E+01
   Friction velocity        uk    :  0.47410E-01 0.75424E+01
   Dimensionless distance   yplus :  0.45478E-03 0.39183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18621
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14195E+02     114   0.19241E+00   0.14492E+04 0.89969E+03 
c  Velocity[X]                                      0.45979E+03 
c  Velocity[Y]                                      0.44430E+03 
c  Velocity[Z]                                      0.54507E+03 
c  Pressure     0.18517E+00     802   0.57735E-02   0.28601E+00 0.92921E+03 
c  k            0.16625E+01      78   0.61756E-02   0.98073E+01 0.13801E+04 
c  epsilon      0.37513E+05      56   0.45187E-02   0.48956E+10 0.10643E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023876                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.718          53.847          3.2734         0.36249
v  Velocity[Y]            -49.929          60.422          1.2817         0.82668
v  Velocity[Z]            -89.384          67.845          -1.663      -0.0011132
v  ǁVelocityǁ            0.001658          101.79          9.8511       Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20511E+03 0.35552E+02
   Friction velocity        uet   :  0.37545E-01 0.71951E+01
   Friction velocity        uk    :  0.46975E-01 0.75473E+01
   Dimensionless distance   yplus :  0.45543E-03 0.38894E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18591
   Nb of faces within the viscous sub-layer     :       7395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14199E+02     114   0.19097E+00   0.16744E+04 0.95606E+03 
c  Velocity[X]                                      0.49237E+03 
c  Velocity[Y]                                      0.46258E+03 
c  Velocity[Z]                                      0.71950E+03 
c  Pressure     0.17297E+00     641   0.57428E-02   0.26818E+00 0.90205E+03 
c  k            0.16195E+01      76   0.88358E-02   0.25740E+02 0.18271E+04 
c  epsilon      0.37049E+05      54   0.63436E-02   0.44976E+10 0.79666E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initiUndefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11333E+03 0.35897E+02
   Friction velocity        uet   :  0.39899E-01 0.71146E+01
   Friction velocity        uk    :  0.47410E-01 0.75424E+01
   Dimensionless distance   yplus :  0.45478E-03 0.39183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18621
   Nb of faces within the viscous sub-layer     :       7396
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14195E+02     114   0.19241E+00   0.14492E+04 0.89969E+03 
c  Velocity[X]                                      0.45979E+03 
c  Velocity[Y]                                      0.44430E+03 
c  Velocity[Z]                                      0.54507E+03 
c  Pressure     0.18517E+00     802   0.57735E-02   0.28601E+00 0.92921E+03 
c  k            0.16625E+01      78   0.61756E-02   0.98073E+01 0.13801E+04 
c  epsilon      0.37513E+05      56   0.45187E-02   0.48956E+10 0.10643E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023876                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.718          53.847          3.2734         0.36249
v  Velocity[Y]            -49.929          60.422          1.2817         0.82668
v  Velocity[Z]            -89.384          67.845          -1.663      -0.0011132
v  ǁVelocityǁ            0.001658          101.79          9.8511          7.7839
v  Pressure           -1.1066e+06      6.0982e+05      3.2117e+05      2.8884e+05
v  k                   1.5448e-05          59.432         0.20062         0.12839
v  epsilon               0.028239      1.1962e+07           17263          147.79
v  TurbVisc             3.812e-11         0.58638       0.0057771        0.049211
v  total_pressure     -6.0664e+05      1.1098e+06      8.2117e+05      7.8884e+05


 TIME FOR THE TIME STEP              695:        0.73683E+02

===============================================================


 INSTANT    0.696000000E+03   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000         0.178515553E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888870E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13798E+03 0.41485E+02
   Friction velocity        uet   :  0.10502E-01 0.75582E+01
   Friction velocity        uk    :  0.48180E-01 0.75539E+01
   Dimensionless distance   yplus :  0.45424E-03 0.40927E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18617
   Nb of faces within the viscous sub-layer     :       7403
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14183E+02     114   0.19069E+00   0.16371E+04 0.94592E+03 
c  Velocity[X]                                      0.48183E+03 
c  Velocity[Y]                                      0.50857E+03 
c  Velocity[Z]                                      0.64666E+03 
c  Pressure     0.18531E+00     806   0.54227E-02   0.28674E+00 0.97848E+03 
c  k            0.16329E+01      77   0.75998E-02   0.16877E+02 0.18566E+04 
c  epsilon      0.37151E+05      55   0.55669E-02   0.16532E+11 0.16522E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  -------Free outlet               3          46         0.312888872E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12264E+03 0.37920E+02
   Friction velocity        uet   :  0.21580E-01 0.70409E+01
   Friction velocity        uk    :  0.45404E-01 0.75415E+01
   Dimensionless distance   yplus :  0.45835E-03 0.41320E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18605
   Nb of faces within the viscous sub-layer     :       7445
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14201E+02     115   0.19223E+00   0.15436E+04 0.91822E+03 
c  Velocity[X]                                      0.45797E+03 
c  Velocity[Y]                                      0.47500E+03 
c  Velocity[Z]                                      0.61064E+03 
c  Pressure     0.17725E+00     608   0.56611E-02   0.27583E+00 0.13221E+04 
c  k            0.17974E+01      77   0.10347E-01   0.59241E+02 0.23254E+04 
c  epsilon      0.37388E+05      53   0.76073E-02   0.97871E+10 0.81263E+05 
------------------------------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20511E+03 0.35552E+02
   Friction velocity        uet   :  0.37545E-01 0.71951E+01
   Friction velocity        uk    :  0.46975E-01 0.75473E+01
   Dimensionless distance   yplus :  0.45543E-03 0.38894E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18591
   Nb of faces within the viscous sub-layer     :       7395
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14199E+02     114   0.19097E+00   0.16744E+04 0.95606E+03 
c  Velocity[X]                                      0.49237E+03 
c  Velocity[Y]                                      0.46258E+03 
c  Velocity[Z]                                      0.71950E+03 
c  Pressure     0.17297E+00     641   0.57428E-02   0.26818E+00 0.90205E+03 
c  k            0.16195E+01      76   0.88358E-02   0.25740E+02 0.18271E+04 
c  epsilon      0.37049E+05      54   0.63436E-02   0.44976E+10 0.79666E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021689                             2
a  epsilon         -418.36                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.635          50.819          3.2715          0.3628
v  Velocity[Y]            -45.773          58.299          1.2598         0.82671
v  Velocity[Z]             -77.87           67.03         -1.6554     -0.00098393
v  ǁVelocityǁ           0.0016821           89.94          9.8373           7.782
v  Pressure           -1.1056e+06      6.0836e+05      3.2025e+05      2.8813e+05
v  k                   1.5416e-05          53.217         0.20176         0.12948
v  epsilon               0.028209      1.2087e+07           17280          148.58
v  TurbVisc            3.8487e-11         0.51011       0.0058648        0.049316
v  total_pressure     -6.0562e+05      1.1084e+06      8.2025e+05      7.8813e+05


 TIME FOR THE TIME STEP              697:        0.63753E+02

===============================================================


 INSTANT    0.698000000E+03   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.312888889E+01
Smooth wall               5       41000        -0.130858035E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888900E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+03 0.37079E+02
   Friction velocity        uet   :  0.41482E-01 0.67159E+01
   Friction velocity        uk    :  0.42549E-01 0.75898E+01
   Dimensionless distance   yplus :  0.45703E-03 0.42757E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18604
   Nb of faces within the viscous sub-layer     :       7410
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14191E+02     115   0.19113E+00   0.15640E+04 0.94285E+03 
c  Velocity[X]                                      0.49860E+03 
c  Velocity[Y]                                      0.45632E+03 
c  Velocity[Z]                                      0.60911E+03 
c  Pressure     0.18041E+00     715   0.54949E-02   0.27991E+00 0.10074E+04 
c  k            0.16428E+01      76   0.85582E-02   0.28676E+02 0.17588E+04 
c  epsilon      0.36668E+05      52   0.57815E-02   0.37482E+10 0.89997E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fieSmooth wall               5       41000        -0.127187234E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26207E+03 0.36859E+02
   Friction velocity        uet   :  0.41615E-01 0.83117E+01
   Friction velocity        uk    :  0.53090E-01 0.75552E+01
   Dimensionless distance   yplus :  0.46172E-03 0.43578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18547
   Nb of faces within the viscous sub-layer     :       7487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14267E+02     120   0.19112E+00   0.28374E+04 0.10745E+04 
c  Velocity[X]                                      0.62149E+03 
c  Velocity[Y]                                      0.80773E+03 
c  Velocity[Z]                                      0.14081E+04 
c  Pressure     0.17599E+00     918   0.21495E-01   0.27399E+00 0.70825E+05 
c  k            0.20131E+01      99   0.66470E-02   0.28461E+02 0.18163E+04 
c  epsilon      0.38241E+05      60   0.68857E-02   0.15946E+11 0.15446E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022802                             2
a  epsilon         -595.07                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.674          55.555          3.2931         0.38019
v  Velocity[Y]            -55.305          44.487          1.2639         0.86919
v  Velocity[Z]             -92.17          77.214         -1.6475      -0.0018677
v  ǁVelocityǁ           0.0017167          107.22          9.8682          8.0665
v  Pressure           -1.0393e+06      6.8616e+05       3.902e+05      3.5263e+05
v  k                   1.5005e-05           79.06         0.20423         0.13566
v  epsilon                0.01548      1.2063e+07           17148           160.1
v  TurbVisc            3.9326e-11         0.99979       0.0060081        0.049595
v  total_pressure     -5.3933e+05      1.1862e+06       8.902e+05      8.5263e+05


 TIME FOR THE TIME STEP              701:        0.79122E+02

===============================================================


 INSTANT    0.702000000E+03   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        -0.112830904E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160650E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13639E+03 0.27010E+02
   Friction velocity        uet   :  0.39355E-01 0.78909E+01
   Friction velocity        uk    :  0.50806E-01 0.76051E+01
   Dimensionless distance   yplus :  0.46186E-03 0.43875E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18653
   Nb of faces within the viscous sub-layer     :       7487
   Total number of wall faces                   :      41000
--------------Smooth wall               5       41000        -0.127187234E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26207E+03 0.36859E+02
   Friction velocity        uet   :  0.41615E-01 0.83117E+01
   Friction velocity        uk    :  0.53090E-01 0.75552E+01
   Dimensionless distance   yplus :  0.46172E-03 0.43578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18547
   Nb of faces within the viscous sub-layer     :       7487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14267E+02     120   0.19112E+00   0.28374E+04 0.10745E+04 
c  Velocity[X]                                      0.62149E+03 
c  Velocity[Y]                                      0.80773E+03 
c  Velocity[Z]                                      0.14081E+04 
c  Pressure     0.17599E+00     918   0.21495E-01   0.27399E+00 0.70825E+05 
c  k            0.20131E+01      99   0.66470E-02   0.28461E+02 0.18163E+04 
c  epsilon      0.38241E+05      60   0.68857E-02   0.15946E+11 0.15446E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022802                             2
a  epsilon         -595.07                             1


  ** Computed fieldBoundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.794816899E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19176E+03 0.31343E+02
   Friction velocity        uet   :  0.45277E-01 0.10731E+02
   Friction velocity        uk    :  0.72899E-01 0.75847E+01
   Dimensionless distance   yplus :  0.46401E-03 0.43236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18661
   Nb of faces within the viscous sub-layer     :       7441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15115E+02     127   0.18790E+00   0.23754E+04 0.10845E+04 
c  Velocity[X]                                      0.58652E+03 
c  Velocity[YSmooth wall               5       41000        -0.127187234E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.312888871E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26207E+03 0.36859E+02
   Friction velocity        uet   :  0.41615E-01 0.83117E+01
   Friction velocity        uk    :  0.53090E-01 0.75552E+01
   Dimensionless distance   yplus :  0.46172E-03 0.43578E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18547
   Nb of faces within the viscous sub-layer     :       7487
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14267E+02     120   0.19112E+00   0.28374E+04 0.10745E+04 
c  Velocity[X]                                      0.62149E+03 
c  Velocity[Y]                                      0.80773E+03 
c  Velocity[Z]                                      0.14081E+04 
c  Pressure     0.17599E+00     918   0.21495E-01   0.27399E+00 0.70825E+05 
c  k            0.20131E+01      99   0.66470E-02   0.28461E+02 0.18163E+04 
c  epsilon      0.38241E+05      60   0.68857E-02   0.15946E+11 0.15446E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022802                             2
a  epsilon         -595.07                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -19.674          55.555          3.2931         0.38019
v  Velocity[Y]            -55.305          44.487          1.2639         0.86919
v  Velocity[Z]             -92.17          77.214         -1.6475      -0.0018677
v  ǁVelocityǁ           0.0017167          107.22          9.8682          8.0665
v  Pressure           -1.0393e+06      6.8616e+05       3.902e+05      3.5263e+05
v  k                   1.5005e-05           79.06         0.20423         0.13566
v  epsilon                0.01548      1.2063e+07           17148           160.1
v  TurbVisc            3.9326e-11         0.99979       0.0Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.794816899E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19176E+03 0.31343E+02
   Friction velocity        uet   :  0.45277E-01 0.10731E+02
   Friction velocity        uk    :  0.72899E-01 0.75847E+01
   Dimensionless distance   yplus :  0.46401E-03 0.43236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18661
   Nb of faces within the viscous sub-layer     :       7441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15115E+02     127   0.18790E+00   0.23754E+04 0.10845E+04 
c  Velocity[X]                                      0.58652E+03 
c  Velocity[Y]                                      0.81981E+03 
c  Velocity[Z]                                      0.96910E+03 
c  Pressure     0.19966E+00    1112   0.10108E-01   0.30416E+00 0.12709E+05 
c  k            0.20889E+01      91   0.59655E-02   0.14580E+02 0.12443E+04 
c  epsilon      0.39963E+05      58   0.64616E-02   0.14445E+11 0.99542E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  --------
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.948247733E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21615E+03 0.58534E+02
   Friction velocity        uet   :  0.34791E-01 0.96888E+01
   Friction velocity        uk    :  0.68478E-01 0.76270E+01
   Dimensionless distance   yplus :  0.46747E-03 0.52889E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
---------------------------------------------Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.794816899E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19176E+03 0.31343E+02
   Friction velocity        uet   :  0.45277E-01 0.10731E+02
   Friction velocity        uk    :  0.72899E-01 0.75847E+01
   Dimensionless distance   yplus :  0.46401E-03 0.43236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18661
   Nb of faces within the viscous sub-layer     :       7441
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15115E+02     127   0.18790E+00   0.23754E+04 0.10845E+04 
c  Velocity[X]                                      0.58652E+03 
c  Velocity[Y]                                      0.81981E+03 
c  Velocity[Z]                                      0.96910E+03 
c  Pressure     0.19966E+00    1112   0.10108E-01   0.30416E+00 0.12709E+05 
c  k            0.20889E+01      91   0.59655E-02   0.14580E+02 0.12443E+04 
c  epsilon      0.39963E+05      58   0.64616E-02   0.14445E+11 0.99542E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020261                             2
a  epsilon         -597.23                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.936           64.33          3.3073         0.37994
v  Velocity[Y]             -49.09          46.479          1.2431         0.86688
v  Velocity[Z]            -130.46          81.009          -1.662        -0.00185
v  ǁVelocityǁ           0.0017451           148.7          9.9187          8.0709
v  Pressure            -1.102e+06      6.3744e+05      3.4679e+05      3.1033e+05
v  k                   1.4658e-05           82.19         0.20574         0.14038
v
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.948247733E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21615E+03 0.58534E+02
   Friction velocity        uet   :  0.34791E-01 0.96888E+01
   Friction velocity        uk    :  0.68478E-01 0.76270E+01
   Dimensionless distance   yplus :  0.46747E-03 0.52889E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15208E+02     123   0.18866E+00   0.23240E+04 0.10304E+04 
c  Velocity[X]                                      0.58617E+03 
c  Velocity[Y]                                      0.66922E+03 
c  Velocity[Z]                                      0.10686E+04 
c  Pressure     0.21768E+00     790   0.92663E-02   0.32945E+00 0.36576E+04 
c  k            0.22709E+01      84   0.57248E-02   0.21577E+02 0.15502E+04 
c  epsilon      0.43374E+05      55   0.59042E-02   0.60113E+10 0.24717E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippin===============================================================


 INSTANT    0.707000000E+03   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        -0.146420761E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14475E+03 0.50957E+02
   Friction velocity        uet   :  0.39270E-01 0.69817E+01
   Friction velocity        uk    :  0.72030E-01 0.76376E+01
   Dimensionless distance   yplus :  0.47418E-03 0.49407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-------------------------------------------------------------
   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.948247733E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21615E+03 0.58534E+02
   Friction velocity        uet   :  0.34791E-01 0.96888E+01
   Friction velocity        uk    :  0.68478E-01 0.76270E+01
   Dimensionless distance   yplus :  0.46747E-03 0.52889E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15208E+02     123   0.18866E+00   0.23240E+04 0.10304E+04 
c  Velocity[X]                                      0.58617E+03 
c  Velocity[Y]                                      0.66922E+03 
c  Velocity[Z]                                      0.10686E+04 
c  Pressure     0.21768E+00     790   0.92663E-02   0.32945E+00 0.36576E+04 
c  k            0.22709E+01      84   0.57248E-02   0.21577E+02 0.15502E+04 
c  epsilon      0.43374E+05      55   0.59042E-02   0.60113E+10 0.24717E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022777                             2
a  epsilon         -656.62                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.316            56.3           3.325         0.37878
v  Velocity[Y]            -49.762          45.363          1.2148           0.867
v  Velocity[Z]            -95.961          123.54         -1.6756      -0.0020693
v  ǁVelocityǁ           0.0017782          132.52  ===============================================================


 INSTANT    0.707000000E+03   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        -0.146420761E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14475E+03 0.50957E+02
   Friction velocity        uet   :  0.39270E-01 0.69817E+01
   Friction velocity        uk    :  0.72030E-01 0.76376E+01
   Dimensionless distance   yplus :  0.47418E-03 0.49407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15292E+02     121   0.18982E+00   0.19467E+04 0.10199E+04 
c  Velocity[X]                                      0.55148E+03 
c  Velocity[Y]                                      0.58242E+03 
c  Velocity[Z]                                      0.81276E+03 
c  Pressure     0.21726E+00     746   0.67524E-02   0.33178E+00 0.11477E+04 
c  k            0.22806E+01      80   0.81525E-02   0.32771E+02 0.17730E+04 
c  epsilon      0.43256E+05 v  total_pressure     -6.4567e+05      1.1473e+06      8.4619e+05      8.1118e+05


 TIME FOR THE TIME STEP              708:        0.74711E+02

===============================================================


 INSTANT    0.709000000E+03   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.626472545E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28052E+03 0.37391E+02
   Friction velocity        uet   :  0.38463E-01 0.86150E+01
   Friction velocity        uk    :  0.68220E-01 0.76610E+01
   Dimensionless distance   yplus :  0.47784E-03 0.43432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18781
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      4===============================================================


 INSTANT    0.707000000E+03   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        -0.146420761E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14475E+03 0.50957E+02
   Friction velocity        uet   :  0.39270E-01 0.69817E+01
   Friction velocity        uk    :  0.72030E-01 0.76376E+01
   Dimensionless distance   yplus :  0.47418E-03 0.49407E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7501
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15292E+02     121   0.18982E+00   0.19467E+04 0.10199E+04 
c  Velocity[X]                                      0.55148E+03 
c  Velocity[Y]                                      0.58242E+03 
c  Velocity[Z]                                      0.81276E+03 
c  Pressure     0.21726E+00     746   0.67524E-02   0.33178E+00 0.11477E+04 
c  k            0.22806E+01      80   0.81525E-02   0.32771E+02 0.17730E+04 
c  epsilon      0.43256E+05      55   0.83973E-02   0.91853E+10 0.14153E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021302                             2
a  epsilon         -680.38                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.511          54.839          3.3493         0.37825
v  Velocity[Y]            -44.687          65.971          1.1964      v  total_pressure     -6.4567e+05      1.1473e+06      8.4619e+05      8.1118e+05


 TIME FOR THE TIME STEP              708:        0.67268E+02

===============================================================


 INSTANT    0.709000000E+03   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.626472545E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28052E+03 0.37391E+02
   Friction velocity        uet   :  0.38463E-01 0.86150E+01
   Friction velocity        uk    :  0.68220E-01 0.76610E+01
   Dimensionless distance   yplus :  0.47784E-03 0.43432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18781
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15332E+02     120   0.18868E+00   0.21845E+04 0.10458E+04 
c  Velocity[X]                                      0.60211E+03 
c  Velocity[Y]                                      0.62236E+03 
c  Velocity[Z]                                      0.96007E+03 
c  Pressure     0.v  epsilon               0.027426      1.2223e+07           17819          175.38
v  TurbVisc            5.4696e-11         0.85544       0.0065763        0.052863
v  total_pressure     -6.5763e+05      1.1499e+06       8.449e+05      8.1028e+05


 TIME FOR THE TIME STEP              710:        0.64927E+02

===============================================================


 INSTANT    0.711000000E+03   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.163408725E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20736E+03 0.30199E+02
   Friction velocity        uet   :  0.38333E-01 0.95662E+01
   Friction velocity        uk    :  0.55343E-01 0.76915E+01
   Dimensionless distance   yplus :  0.49003E-03 0.43954E+02
   ------------------------------------------------------
   Nb of reversal of the velocitv  total_pressure     -6.4567e+05      1.1473e+06      8.4619e+05      8.1118e+05


 TIME FOR THE TIME STEP              708:        0.83358E+02

===============================================================


 INSTANT    0.709000000E+03   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.626472545E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28052E+03 0.37391E+02
   Friction velocity        uet   :  0.38463E-01 0.86150E+01
   Friction velocity        uk    :  0.68220E-01 0.76610E+01
   Dimensionless distance   yplus :  0.47784E-03 0.43432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18781
   Nb of faces within the viscous sub-layer     :       7508
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15332E+02     120   0.18868E+00   0.21845E+04 0.10458E+04 
c  Velocity[X]                                      0.60211E+03 
c  Velocity[Y]                                      0.62236E+03 
c  Velocity[Z]                                      0.96007E+03 
c  Pressure     0.21562E+00     691   0.67206E-02   0.32753E+00 0.53623E+03 
c  k            0.24586E+01      80   0.98268E-02   0.61649E+02 0.25158E+04 
c  epsilon      0.43755E+05      59   0.10949E-01   0.59687E+11 0.34716E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021766                             2
a  epsilon         -673.83                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  ----v  epsilon               0.027426      1.2223e+07           17819          175.38
v  TurbVisc            5.4696e-11         0.85544       0.0065763        0.052863
v  total_pressure     -6.5763e+05      1.1499e+06       8.449e+05      8.1028e+05


 TIME FOR THE TIME STEP              710:        0.76360E+02

===============================================================


 INSTANT    0.711000000E+03   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.163408725E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20736E+03 0.30199E+02
   Friction velocity        uet   :  0.38333E-01 0.95662E+01
   Friction velocity        uk    :  0.55343E-01 0.76915E+01
   Dimensionless distance   yplus :  0.49003E-03 0.43954E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18800
   Nb of faces within the viscous sub-layer     :       7534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15382E+02     118   0.19093E+00   0.20022E+04 0.10100E+04 
c  Velocity[X]                                   v  Pressure           -1.1676e+06      6.5194e+05      3.4431e+05      3.0999e+05
v  k                   1.2817e-05           58.25          0.2177         0.14921
v  epsilon               0.026745      1.2323e+07           18033          173.17
v  TurbVisc              5.56e-11         0.58839       0.0067739        0.053155
v  total_pressure     -6.6759e+05      1.1519e+06      8.4431e+05      8.0999e+05


 TIME FOR THE TIME STEP              712:        0.64987E+02

===============================================================


 INSTANT    0.713000000E+03   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        -0.177415313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16520E+03 0.44910E+02
   Friction velocity        uet   :  0.38314E-01 0.79212E+01
   Friction velocity        uk    :  0.73935E-01v  epsilon               0.027426      1.2223e+07           17819          175.38
v  TurbVisc            5.4696e-11         0.85544       0.0065763        0.052863
v  total_pressure     -6.5763e+05      1.1499e+06       8.449e+05      8.1028e+05


 TIME FOR THE TIME STEP              710:        0.75504E+02

===============================================================


 INSTANT    0.711000000E+03   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.163408725E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20736E+03 0.30199E+02
   Friction velocity        uet   :  0.38333E-01 0.95662E+01
   Friction velocity        uk    :  0.55343E-01 0.76915E+01
   Dimensionless distance   yplus :  0.49003E-03 0.43954E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18800
   Nb of faces within the viscous sub-layer     :       7534
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15382E+02     118   0.19093E+00   0.20022E+04 0.10100E+04 
c  Velocity[X]                                      0.56055E+03 
c  Velocity[Y]                                      0.60562E+03 
c  Velocity[Z]                                      0.83604E+03 
c  Pressure     0.22260E+00     801   0.76277E-02   0.33727E+00 0.54329E+03 
c  k            0.23930E+01      80   0.13698E-01   0.13778E+03 0.39906E+04 
c  epsilon      0.44754E+05      59   0.11724E-01   0.38769E+11 0.19466E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024274                             2
a  epsilon         -734.53                             1


  ** Computed fields on cells
     ---------------v  Pressure           -1.1676e+06      6.5194e+05      3.4431e+05      3.0999e+05
v  k                   1.2817e-05           58.25          0.2177         0.14921
v  epsilon               0.026745      1.2323e+07           18033          173.17
v  TurbVisc              5.56e-11         0.58839       0.0067739        0.053155
v  total_pressure     -6.6759e+05      1.1519e+06      8.4431e+05      8.0999e+05


 TIME FOR THE TIME STEP              712:        0.65311E+02

===============================================================


 INSTANT    0.713000000E+03   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        -0.177415313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16520E+03 0.44910E+02
   Friction velocity        uet   :  0.38314E-01 0.79212E+01
   Friction velocity        uk    :  0.73935E-01 0.76507E+01
   Dimensionless distance   yplus :  0.49285E-03 0.44649E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18803
   Nb of faces within the viscous sub-layer     :       7506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
--------------------------------------v  Velocity[Z]            -124.55          78.295         -1.7159      -0.0019939
v  ǁVelocityǁ            0.001988          141.26          10.145          8.1188
v  Pressure           -1.1766e+06      6.5248e+05      3.4465e+05      3.1034e+05
v  k                   1.2467e-05          62.128         0.22145         0.14957
v  epsilon               0.026333      1.2468e+07           18316          169.31
v  TurbVisc            5.6895e-11          0.5306        0.006984        0.053381
v  total_pressure     -6.7659e+05      1.1525e+06      8.4465e+05      8.1034e+05


 TIME FOR THE TIME STEP              714:        0.75007E+02

===============================================================


 INSTANT    0.715000000E+03   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.296971472E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Relv  Pressure           -1.1676e+06      6.5194e+05      3.4431e+05      3.0999e+05
v  k                   1.2817e-05           58.25          0.2177         0.14921
v  epsilon               0.026745      1.2323e+07           18033          173.17
v  TurbVisc              5.56e-11         0.58839       0.0067739        0.053155
v  total_pressure     -6.6759e+05      1.1519e+06      8.4431e+05      8.0999e+05


 TIME FOR THE TIME STEP              712:        0.68940E+02

===============================================================


 INSTANT    0.713000000E+03   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        -0.177415313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16520E+03 0.44910E+02
   Friction velocity        uet   :  0.38314E-01 0.79212E+01
   Friction velocity        uk    :  0.73935E-01 0.76507E+01
   Dimensionless distance   yplus :  0.49285E-03 0.44649E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18803
   Nb of faces within the viscous sub-layer     :       7506
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15395E+02     118   0.18959E+00   0.18877E+04 0.99266E+03 
c  Velocity[X]                                      0.54196E+03 
c  Velocity[Y]                                      0.56746E+03 
c  Velocity[Z]                                      0.77824E+03 
c  Pressure     0.22633E+00     729   0.60188E-02   0.34324E+00 0.10961E+04 
c  k            0.19344E+01      82   0.15734E-01   0.86414E+02 0.36068E+04 
c  epsilon      0.41356E+05      59   0.13875E-01   0.29255E+11 0.15563E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
v  Velocity[Z]            -124.55          78.295         -1.7159      -0.0019939
v  ǁVelocityǁ            0.001988          141.26          10.145          8.1188
v  Pressure           -1.1766e+06      6.5248e+05      3.4465e+05      3.1034e+05
v  k                   1.2467e-05          62.128         0.22145         0.14957
v  epsilon               0.026333      1.2468e+07           18316          169.31
v  TurbVisc            5.6895e-11          0.5306        0.006984        0.053381
v  total_pressure     -6.7659e+05      1.1525e+06      8.4465e+05      8.1034e+05


 TIME FOR THE TIME STEP              714:        0.74742E+02

===============================================================


 INSTANT    0.715000000E+03   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.296971472E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11561E+03 0.28932E+02
   Friction velocity        uet   :  0.38289E-01 0.10196E+02
   Friction velocity        uk    :  0.71301E-01 0.76830E+01
   Dimensionless distance   yplus :  0.49656E-03 0.46204E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18800
   Nb of faces within the viscous sub-layer     :       7495
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------------------------v  Velocity[X]            -27.139          62.248          3.4226         0.37788
v  Velocity[Y]            -71.461          46.725          1.2134         0.86698
v  Velocity[Z]            -96.554          100.84         -1.7193      -0.0014681
v  ǁVelocityǁ           0.0019537          123.65          10.176          8.1278
v  Pressure           -1.1841e+06      6.5289e+05      3.4518e+05      3.1084e+05
v  k                   5.5752e-06          64.182         0.22421         0.14973
v  epsilon               0.026177      1.2441e+07           18475          167.68
v  TurbVisc            5.5948e-11         0.51511        0.007151        0.053545
v  total_pressure     -6.8408e+05      1.1529e+06      8.4518e+05      8.1084e+05


 TIME FOR THE TIME STEP              716:        0.66844E+02

===============================================================


 INSTANT    0.717000000E+03   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         0.479811743E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160648E+01
Free inlet               13           0         0.000000000E+00
Convective 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  Velocity[Z]            -124.55          78.295         -1.7159      -0.0019939
v  ǁVelocityǁ            0.001988          141.26          10.145          8.1188
v  Pressure           -1.1766e+06      6.5248e+05      3.4465e+05      3.1034e+05
v  k                   1.2467e-05          62.128         0.22145         0.14957
v  epsilon               0.026333      1.2468e+07           18316          169.31
v  TurbVisc            5.6895e-11          0.5306        0.006984        0.053381
v  total_pressure     -6.7659e+05      1.1525e+06      8.4465e+05      8.1034e+05


 TIME FOR THE TIME STEP              714:        0.73319E+02

===============================================================


 INSTANT    0.715000000E+03   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.296971472E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11561E+03 0.28932E+02
   Friction velocity        uet   :  0.38289E-01 0.10196E+02
   Friction velocity        uk    :  0.71301E-01 0.76830E+01
   Dimensionless distance   yplus :  0.49656E-03 0.46204E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18800
   Nb of faces within the viscous sub-layer     :       7495
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15421E+02     119   0.19223E+00   0.16459E+04 0.95590E+03 
c  Velocity[X]                                      0.49760E+03 
c  Velocity[Y]                                      0.53803E+03 
c  Velocity[Z]                                      0.61025E+03 
c  Pressure     0.22398E+00     681   0.68346E-02   0.34078E+00 0.11170E+04 
c  k            0.17400E+01      83   0.88452E-02   0.30135E+02 0.23586E+04 
c  epsilon      0.39947E+05      60   0.73003E-02   0.12752E+11 0.15445E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026606                             2
a  epsilon         -586.83                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.473          58.182          3.4166          0.3784
v  Velocity[Y]            -45.233          46.451          1.2057         0.86629
v  Velocity[Z]            -113.96          71.627         -1.7172      -0.0022613
v  ǁVelocityǁ           0.0019674          131.13           10.16          8.1234
v  Pressure           -1.1787e+06      6.5091e+05      3.4418e+05      3.1002e+05
v  k                   1.2293e-05          63.637         0.22282         0.14961
v  epsilon                0.02619      1.2476e+07           18382          167.87
v  TurbVisc            5.6232e-11         0.56033       0.0070779        0.053473
v  total_pressure     -6.7874e+05      1.1509e+06      8.4418e+05      8.1002e+05


 TIME FOR THE TIME STEP              715:        0.67106E+02

===============================================================


 INSTANT    0.716000000E+03   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.102215366E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160651E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.858          58.354           3.436         0.37855
v  Velocity[Y]            -49.481          50.619          1.2232         0.86764
v  Velocity[Z]            -82.408          78.035         -1.7217      -0.0016891
v  ǁVelocityǁ           0.0019473          99.876          10.204          8.1356
v  Pressure           -1.1893e+06        6.52e+05      3.4453e+05      3.1056e+05
v  k                   1.1859e-05          63.556         0.22582         0.14986
v  epsilon               0.026394      1.2529e+07           18611           167.4
v  TurbVisc            7.7615e-12         0.51511       0.0072461        0.053653
v  total_pressure     -6.8933e+05       1.152e+06      8.4453e+05      8.1056e+05


 TIME FOR THE TIME STEP              718:        0.71640E+02

===============================================================


 INSTANT    0.719000000E+03   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         0.108505007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           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]            -27.139          62.248          3.4226         0.37788
v  Velocity[Y]            -71.461          46.725          1.2134         0.86698
v  Velocity[Z]            -96.554          100.84         -1.7193      -0.0014681
v  ǁVelocityǁ           0.0019537          123.65          10.176          8.1278
v  Pressure           -1.1841e+06      6.5289e+05      3.4518e+05      3.1084e+05
v  k                   5.5752e-06          64.182         0.22421         0.14973
v  epsilon               0.026177      1.2441e+07           18475          167.68
v  TurbVisc            5.5948e-11         0.51511        0.007151        0.053545
v  total_pressure     -6.8408e+05      1.1529e+06      8.4518e+05      8.1084e+05


 TIME FOR THE TIME STEP              716:        0.73733E+02

===============================================================


 INSTANT    0.717000000E+03   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         0.479811743E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160648E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32620E+03 0.42654E+02
   Friction velocity        uet   :  0.15971E-01 0.97373E+01
   Friction velocity        uk    :  0.63185E-01 0.77122E+01
   Dimensionless distance   yplus :  0.49262E-03 0.46963E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18834
   Nb of faces within the viscous sub-layer     :       7463
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15447E+02     118   0.19432E+00   0.20032E+04 0.10092E+04 
c  Velocity[X]                                      0.53172E+03 
c  Velocity[Y]                                      0.62238E+03 
c  Velocity[Z]                                      0.84906E+03 
c  Pressure     0.21832E+00     511   0.59142E-02   0.32887E+00 0.69281E+03 
c  k            0.18159E+01      82   0.95479E-02   0.26126E+02 0.21370E+04 
c  epsilon      0.42034E+05      58   0.80344E
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.858          58.354           3.436         0.37855
v  Velocity[Y]            -49.481          50.619          1.2232         0.86764
v  Velocity[Z]            -82.408          78.035         -1.7217      -0.0016891
v  ǁVelocityǁ           0.0019473          99.876          10.204          8.1356
v  Pressure           -1.1893e+06        6.52e+05      3.4453e+05      3.1056e+05
v  k                   1.1859e-05          63.556         0.22582         0.14986
v  epsilon               0.026394      1.2529e+07           18611           167.4
v  TurbVisc            7.7615e-12         0.51511       0.0072461        0.053653
v  total_pressure     -6.8933e+05       1.152e+06      8.4453e+05      8.1056e+05


 TIME FOR THE TIME STEP              718:        0.68774E+02

===============================================================


 INSTANT    0.719000000E+03   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         0.108505007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11081E+03 0.39729E+02
   Friction velocity        uet   :  0.17566E-01 0.70042E+01
   Friction velocity        uk    :  0.31273E-01 0.76848E+01
   Dimensionless distance   yplus :  0.49129E-03 0.46733E+02
   ------------------------------------------------------
  a  k            -0.0025196                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.04          58.371          3.4472         0.37894
v  Velocity[Y]            -55.682          53.843          1.2277         0.86636
v  Velocity[Z]            -91.057          77.148         -1.7219       -0.002032
v  ǁVelocityǁ           0.0019319          105.37          10.229          8.1419
v  Pressure           -1.1941e+06      6.5294e+05      3.4573e+05      3.1156e+05
v  k                   1.1691e-05          56.376         0.22628         0.15019
v  epsilon               0.026799      1.2651e+07           18748          167.13
v  TurbVisc             9.981e-13         0.51511       0.0072653        0.053741
v  total_pressure      -6.941e+05      1.1529e+06      8.4573e+05      8.1156e+05


 TIME FOR THE TIME STEP              720:        0.76833E+02

===============================================================


 INSTANT    0.721000000E+03   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.689964241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface        
   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.858          58.354           3.436         0.37855
v  Velocity[Y]            -49.481          50.619          1.2232         0.86764
v  Velocity[Z]            -82.408          78.035         -1.7217      -0.0016891
v  ǁVelocityǁ           0.0019473          99.876          10.204          8.1356
v  Pressure           -1.1893e+06        6.52e+05      3.4453e+05      3.1056e+05
v  k                   1.1859e-05          63.556         0.22582         0.14986
v  epsilon               0.026394      1.2529e+07           18611           167.4
v  TurbVisc            7.7615e-12         0.51511       0.0072461        0.053653
v  total_pressure     -6.8933e+05       1.152e+06      8.4453e+05      8.1056e+05


 TIME FOR THE TIME STEP              718:        0.72172E+02

===============================================================


 INSTANT    0.719000000E+03   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         0.108505007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11081E+03 0.39729E+02
   Friction velocity        uet   :  0.17566E-01 0.70042E+01
   Friction velocity        uk    :  0.31273E-01 0.76848E+01
   Dimensionless distance   yplus :  0.49129E-03 0.46733E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18852
   Nb of faces within the viscous sub-layer     :       7417
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15461E+02     116   0.18797E+00   0.17174E+04 0.96345E+03 
c  Velocity[X]                                      0.52235E+03 
c  Velocity[Y]                                      0.51589E+03 
c  Velocity[Z]                                      0.67911E+03 
c  Pressure     0.20342Ea  k            -0.0025196                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.04          58.371          3.4472         0.37894
v  Velocity[Y]            -55.682          53.843          1.2277         0.86636
v  Velocity[Z]            -91.057          77.148         -1.7219       -0.002032
v  ǁVelocityǁ           0.0019319          105.37          10.229          8.1419
v  Pressure           -1.1941e+06      6.5294e+05      3.4573e+05      3.1156e+05
v  k                   1.1691e-05          56.376         0.22628         0.15019
v  epsilon               0.026799      1.2651e+07           18748          167.13
v  TurbVisc             9.981e-13         0.51511       0.0072653        0.053741
v  total_pressure      -6.941e+05      1.1529e+06      8.4573e+05      8.1156e+05


 TIME FOR THE TIME STEP              720:        0.73865E+02

===============================================================


 INSTANT    0.721000000E+03   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.689964241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14660E+03 0.43548E+02
   Friction velocity        uet   :  0.34807E-01 0.76441E+01
   Friction velocity        uk    :  0.
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025731                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.456          61.305          3.4505         0.37915
v  Velocity[Y]            -50.187          43.169          1.2315          0.8661
v  Velocity[Z]            -90.919          79.848         -1.7182      -0.0016121
v  ǁVelocityǁ            0.001945          104.37          10.243          8.1463
v  Pressure           -1.1968e+06      6.5495e+05      3.4669e+05      3.1229e+05
v  k                   1.1616e-05          57.989         0.22616         0.15071
v  epsilon               0.027221      1.2642e+07           18820          166.28
v  TurbVisc            2.5055e-12         0.51511       0.0072608         0.05386
v  total_pressure     -6.9682e+05       1.155e+06      8.4669e+05      8.1229e+05


 TIME FOR THE TIME STEP              722:        0.76291E+02

===============================================================


 INSTANT    0.723000000E+03   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        -0.461983064E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet        a  k            -0.0025196                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -24.04          58.371          3.4472         0.37894
v  Velocity[Y]            -55.682          53.843          1.2277         0.86636
v  Velocity[Z]            -91.057          77.148         -1.7219       -0.002032
v  ǁVelocityǁ           0.0019319          105.37          10.229          8.1419
v  Pressure           -1.1941e+06      6.5294e+05      3.4573e+05      3.1156e+05
v  k                   1.1691e-05          56.376         0.22628         0.15019
v  epsilon               0.026799      1.2651e+07           18748          167.13
v  TurbVisc             9.981e-13         0.51511       0.0072653        0.053741
v  total_pressure      -6.941e+05      1.1529e+06      8.4573e+05      8.1156e+05


 TIME FOR THE TIME STEP              720:        0.68875E+02

===============================================================


 INSTANT    0.721000000E+03   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.689964241E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160656E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14660E+03 0.43548E+02
   Friction velocity        uet   :  0.34807E-01 0.76441E+01
   Friction velocity        uk    :  0.60263E-01 0.77088E+01
   Dimensionless distance   yplus :  0.48965E-03 0.44011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18899
   Nb of faces within the viscous sub-layer     :       7386
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15500E+02     118   0.19702E+00   0.16950E+04 0.95857E+03 
c  Velocity[X]                                      0.51399E+03 
c  Velocity
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025731                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.456          61.305          3.4505         0.37915
v  Velocity[Y]            -50.187          43.169          1.2315          0.8661
v  Velocity[Z]            -90.919          79.848         -1.7182      -0.0016121
v  ǁVelocityǁ            0.001945          104.37          10.243          8.1463
v  Pressure           -1.1968e+06      6.5495e+05      3.4669e+05      3.1229e+05
v  k                   1.1616e-05          57.989         0.22616         0.15071
v  epsilon               0.027221      1.2642e+07           18820          166.28
v  TurbVisc            2.5055e-12         0.51511       0.0072608         0.05386
v  total_pressure     -6.9682e+05       1.155e+06      8.4669e+05      8.1229e+05


 TIME FOR THE TIME STEP              722:        0.70242E+02

===============================================================


 INSTANT    0.723000000E+03   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        -0.461983064E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025503                             2
a  epsilon         -141.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.045          60.938          3.4461         0.37851
v  Velocity[Y]              -46.7           57.04          1.2365         0.86725
v  Velocity[Z]            -86.985           80.92         -1.7154      -0.0015166
v  ǁVelocityǁ           0.0019777          103.94          10.256          8.1513
v  Pressure           -1.2035e+06      6.5832e+05      3.4798e+05      3.1318e+05
v  k                   1.1601e-05          53.829         0.22598          0.1513
v  epsilon               0.027697      1.2731e+07           18868          165.33
v  TurbVisc            5.5068e-11         0.51511       0.0072428           0.054
v  total_pressure     -7.0347e+05      1.1583e+06      8.4798e+05      8.1318e+05


 TIME FOR THE TIME STEP              724:        0.71601E+02

===============================================================


 INSTANT    0.725000000E+03   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.894329615E-17
Rough wall           
   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025731                             1
a  epsilon


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.456          61.305          3.4505         0.37915
v  Velocity[Y]            -50.187          43.169          1.2315          0.8661
v  Velocity[Z]            -90.919          79.848         -1.7182      -0.0016121
v  ǁVelocityǁ            0.001945          104.37          10.243          8.1463
v  Pressure           -1.1968e+06      6.5495e+05      3.4669e+05      3.1229e+05
v  k                   1.1616e-05          57.989         0.22616         0.15071
v  epsilon               0.027221      1.2642e+07           18820          166.28
v  TurbVisc            2.5055e-12         0.51511       0.0072608         0.05386
v  total_pressure     -6.9682e+05       1.155e+06      8.4669e+05      8.1229e+05


 TIME FOR THE TIME STEP              722:        0.73535E+02

===============================================================


 INSTANT    0.723000000E+03   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        -0.461983064E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14623E+03 0.41935E+02
   Friction velocity        uet   :  0.35433E-01 0.76138E+01
   Friction velocity        uk    :  0.55543E-01 0.77214E+01
   Dimensionless distance   yplus :  0.49098E-03 0.44637E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18893
   Nb of faces within the viscous sub-layer     :       7364
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
---------------------------------------------------------------------------------------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025503                             2
a  epsilon         -141.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.045          60.938          3.4461         0.37851
v  Velocity[Y]              -46.7           57.04          1.2365         0.86725
v  Velocity[Z]            -86.985           80.92         -1.7154      -0.0015166
v  ǁVelocityǁ           0.0019777          103.94          10.256          8.1513
v  Pressure           -1.2035e+06      6.5832e+05      3.4798e+05      3.1318e+05
v  k                   1.1601e-05          53.829         0.22598          0.1513
v  epsilon               0.027697      1.2731e+07           18868          165.33
v  TurbVisc            5.5068e-11         0.51511       0.0072428           0.054
v  total_pressure     -7.0347e+05      1.1583e+06      8.4798e+05      8.1318e+05


 TIME FOR THE TIME STEP              724:        0.72799E+02

===============================================================


 INSTANT    0.725000000E+03   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.894329615E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160657E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------c  k            0.18114E+01      79   0.11362E-01   0.47315E+02 0.24575E+04 
c  epsilon      0.40966E+05      54   0.73356E-02   0.46826E+10 0.99913E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024997                             2
a  epsilon         -408.33                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.582          66.543          3.4328         0.37743
v  Velocity[Y]            -48.389          54.775          1.2414         0.86706
v  Velocity[Z]            -107.06           91.88         -1.7155       -0.001255
v  ǁVelocityǁ            0.001957           123.7          10.266          8.1538
v  Pressure           -1.2013e+06      6.6153e+05      3.4957e+05      3.1419e+05
v  k                   1.1625e-05           72.05         0.22646         0.15239
v  epsilon               0.028235       1.277e+07           18869          167.86
v  TurbVisc            5.4854e-11         0.55867       0.0072321        0.054141
v  total_pressure     -7.0127e+05      1.1615e+06      8.4957e+05      8.1419e+05


 TIME FOR THE TIME STEP              726:        0.71313E+02

===============================================================


 INSTANT    0.727000000E+03   TIME STEP NUMBER             727
 ============================================================= 




   ** 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            -0.0025503                             2
a  epsilon         -141.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.045          60.938          3.4461         0.37851
v  Velocity[Y]              -46.7           57.04          1.2365         0.86725
v  Velocity[Z]            -86.985           80.92         -1.7154      -0.0015166
v  ǁVelocityǁ           0.0019777          103.94          10.256          8.1513
v  Pressure           -1.2035e+06      6.5832e+05      3.4798e+05      3.1318e+05
v  k                   1.1601e-05          53.829         0.22598          0.1513
v  epsilon               0.027697      1.2731e+07           18868          165.33
v  TurbVisc            5.5068e-11         0.51511       0.0072428           0.054
v  total_pressure     -7.0347e+05      1.1583e+06      8.4798e+05      8.1318e+05


 TIME FOR THE TIME STEP              724:        0.76800E+02

===============================================================


 INSTANT    0.725000000E+03   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.894329615E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160657E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19350E+03 0.35249E+02
   Friction velocity        uet   :  0.34407E-01 0.73740E+01
   Friction velocity        uk    :  0.54775E-01 0.77149E+01
   Dimensionless distance   yplus :  0.49559E-03 0.43003E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18922
   Nb of faces within the viscous sub-layer     :       7312
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15547E+02     116   0.19086E+00   0.18110E+04 0.97206E+03 
c  Velocity[X]                                      0.55757E+03 
c  Velocity[Y]                                      0.58402E+03 
c  Velocity[Z]                                      0.66939E+03 
c  Pressure     0.22213E+00     712   0.60971E-02   0.33750E+00 0.10456E+04 
c  k            0.16651E+01      80   0.10123E-01   0.32171E+02 0.21022E+04 
c  epsilon      0.40285E+05      53   0.65885E-02   0.46002E+10 0.23621E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023725                             2
a  epsilon         -775.58                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.479          53.502          3.4402         0.37774
v  Velocity[Y]            -48.815          62.455          1.2377         0.86602
v  Velocity[Z]            -96.262          94.124         -1.7145      -0.0011845
v  ǁVelocityǁ           0.0019605          110.75          10.261          8.1529
v  Pressure           -1.2048e+06      6.5829e+05      3.4868e+05      3.1363e+05
v  k                   1.1608e-05          67.292          0.2262         0.15177
v  epsilon                0.02791      1.2819e+07           18888          166.21
v  TurbVisc            5.5089e-11         0.51511       0.0072357        0.054071
v  total_pressure     -7.0475e+05      1.1583e+06      8.4868e+05      8.1363e+05


 TIME FOR THE TIME STEP              725:        0.76350E+02

===============================================================


 INSTANT    0.726000000E+03   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.56c  Velocity[Z]                                      0.76138E+03 
c  Pressure     0.22451E+00     714   0.74892E-02   0.34377E+00 0.18535E+04 
c  k            0.24037E+01      77   0.13071E-01   0.73720E+02 0.25213E+04 
c  epsilon      0.46121E+05      56   0.12987E-01   0.14393E+11 0.64549E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025537                             2
a  epsilon         -514.28                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.635          54.755          3.4159         0.37674
v  Velocity[Y]             -47.65          56.665           1.244         0.86716
v  Velocity[Z]            -94.403          75.857         -1.7205     -0.00083762
v  ǁVelocityǁ           0.0019683          109.68          10.275          8.1557
v  Pressure           -1.2053e+06      6.6258e+05      3.5059e+05      3.1491e+05
v  k                   1.1706e-05           98.07         0.22823         0.15431
v  epsilon               0.028673      1.2844e+07           18945          176.39
v  TurbVisc            5.5027e-11         0.83275       0.0072481        0.054286
v  total_pressure     -7.0531e+05      1.1626e+06      8.5059e+05      8.1491e+05


 TIME FOR THE TIME STEP              728:        0.71502E+02

===============================================================


 INSTANT    0.729000000E+03   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      --------------c  k            0.18114E+01      79   0.11362E-01   0.47315E+02 0.24575E+04 
c  epsilon      0.40966E+05      54   0.73356E-02   0.46826E+10 0.99913E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024997                             2
a  epsilon         -408.33                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.582          66.543          3.4328         0.37743
v  Velocity[Y]            -48.389          54.775          1.2414         0.86706
v  Velocity[Z]            -107.06           91.88         -1.7155       -0.001255
v  ǁVelocityǁ            0.001957           123.7          10.266          8.1538
v  Pressure           -1.2013e+06      6.6153e+05      3.4957e+05      3.1419e+05
v  k                   1.1625e-05           72.05         0.22646         0.15239
v  epsilon               0.028235       1.277e+07           18869          167.86
v  TurbVisc            5.4854e-11         0.55867       0.0072321        0.054141
v  total_pressure     -7.0127e+05      1.1615e+06      8.4957e+05      8.1419e+05


 TIME FOR THE TIME STEP              726:        0.74623E+02

===============================================================


 INSTANT    0.727000000E+03   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        -0.694776192E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17127E+03 0.44316E+02
   Friction velocity        uet   :  0.22447E-01 0.90120E+01
   Friction velocity        uk    :  0.28977E-01 0.77102E+01
   Dimensionless distance   yplus :  0.49236E-03 0.46275E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18903
   Nb of faces within the viscous sub-layer     :       7271
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15562E+02     116   0.19619E+00   0.17988E+04 0.98038E+03 
c  Velocity[X]                                      0.55189E+03 
c  Velocity[Y]                                      0.58827E+03 
c  Velocity[Z]                                      0.65865E+03 
c  Pressure     0.21942E+00     772   0.62916E-02   0.33406E+00 0.67735E+03 
c  k            0.21149E+01      77   0.13510E-01   0.63230E+02 0.24176E+04 
c  epsilon      0.43785E+05      54   0.10938E-01   0.25202E+11 0.11240E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026149                             2
a  epsilon         -629.53                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.494          59.401          3.4254         0.37687
v  Velocity[Y]            -51.499          52.785          1.2422         0.86657
v  Velocity[Z]            -96.839          84.742         -1.7164      -0.0012388
v  ǁVelocityǁ           0.0019778          108.88          10.271          8.1551
v  Pressure           -1.2011e+06      6.6125e+05      3.4973e+05      3.1434e+05
v  k                   1.1656e-05          85.691          0.2273         0.15328
v  epsilon                0.02844      1.2814e+07           18922          171.68
v  TurbVisc            5.5065e-11         0.70894       0.0072345        0.054213
v  total_pressure     -7.0114e+05      1.1613e+06      8.4973e+05      8.1434e+05


 TIME FOR THE TIME STEP              727:        0.75502E+02

===============================================================


 INSTANT    0.728000000E+03   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nbc  Velocity     0.15538E+02     117   0.18955E+00   0.19417E+04 0.10028E+04 
c  Velocity[X]                                      0.58353E+03 
c  Velocity[Y]                                      0.60315E+03 
c  Velocity[Z]                                      0.75498E+03 
c  Pressure     0.21907E+00     768   0.62435E-02   0.33665E+00 0.63230E+03 
c  k            0.28501E+01      77   0.89245E-02   0.75846E+02 0.23329E+04 
c  epsilon      0.52574E+05      56   0.99479E-02   0.11929E+11 0.84553E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024977                             2
a  epsilon         -672.84                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.908          62.195          3.3979         0.37658
v  Velocity[Y]            -45.276          48.914          1.2485         0.86746
v  Velocity[Z]            -93.108          75.281          -1.732      -0.0013407
v  ǁVelocityǁ           0.0019687          108.86          10.283           8.155
v  Pressure           -1.2055e+06       6.628e+05      3.5102e+05      3.1532e+05
v  k                   1.1859e-05          85.736          0.2302         0.15636
v  epsilon               0.029151      1.2776e+07           18942          185.72
v  TurbVisc            5.5392e-11         0.90244       0.0073139        0.054437
v  total_pressure     -7.0548e+05      1.1628e+06      8.5102e+05      8.1532e+05


 TIME FOR THE TIME STEP              730:        0.74993E+02

===============================================================


 INSTANT    0.731000000E+03   TIME STEP NUMBERc  Velocity[Z]                                      0.76138E+03 
c  Pressure     0.22451E+00     714   0.74892E-02   0.34377E+00 0.18535E+04 
c  k            0.24037E+01      77   0.13071E-01   0.73720E+02 0.25213E+04 
c  epsilon      0.46121E+05      56   0.12987E-01   0.14393E+11 0.64549E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025537                             2
a  epsilon         -514.28                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.635          54.755          3.4159         0.37674
v  Velocity[Y]             -47.65          56.665           1.244         0.86716
v  Velocity[Z]            -94.403          75.857         -1.7205     -0.00083762
v  ǁVelocityǁ           0.0019683          109.68          10.275          8.1557
v  Pressure           -1.2053e+06      6.6258e+05      3.5059e+05      3.1491e+05
v  k                   1.1706e-05           98.07         0.22823         0.15431
v  epsilon               0.028673      1.2844e+07           18945          176.39
v  TurbVisc            5.5027e-11         0.83275       0.0072481        0.054286
v  total_pressure     -7.0531e+05      1.1626e+06      8.5059e+05      8.1491e+05


 TIME FOR THE TIME STEP              728:        0.69548E+02

===============================================================


 INSTANT    0.729000000E+03   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        -0.138787719E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11681E+03 0.41150E+02
   Friction velocity        uet   :  0.37970E-01 0.81223E+01
   Friction velocity        uk    :  0.41688E-01 0.77182E+01
   Dimensionless distance   yplus :  0.49392E-03 0.48005E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wc  Velocity     0.15538E+02     117   0.18955E+00   0.19417E+04 0.10028E+04 
c  Velocity[X]                                      0.58353E+03 
c  Velocity[Y]                                      0.60315E+03 
c  Velocity[Z]                                      0.75498E+03 
c  Pressure     0.21907E+00     768   0.62435E-02   0.33665E+00 0.63230E+03 
c  k            0.28501E+01      77   0.89245E-02   0.75846E+02 0.23329E+04 
c  epsilon      0.52574E+05      56   0.99479E-02   0.11929E+11 0.84553E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024977                             2
a  epsilon         -672.84                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.908          62.195          3.3979         0.37658
v  Velocity[Y]            -45.276          48.914          1.2485         0.86746
v  Velocity[Z]            -93.108          75.281          -1.732      -0.0013407
v  ǁVelocityǁ           0.0019687          108.86          10.283           8.155
v  Pressure           -1.2055e+06       6.628e+05      3.5102e+05      3.1532e+05
v  k                   1.1859e-05          85.736          0.2302         0.15636
v  epsilon               0.029151      1.2776e+07           18942          185.72
v  TurbVisc            5.5392e-11         0.90244       0.0073139        0.054437
v  total_pressure     -7.0548e+05      1.1628e+06      8.5102e+05      8.1532e+05


 TIME FOR THE TIME STEP              730:        0.68120E+02

===============================================================


 INSTANT    0.731000000E+03   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.117557124E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Fr   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15547E+02     117   0.19541E+00   0.18772E+04 0.99291E+03 
c  Velocity[X]                                      0.56791E+03 
c  Velocity[Y]                                      0.54535E+03 
c  Velocity[Z]                                      0.76399E+03 
c  Pressure     0.22289E+00     585   0.72141E-02   0.34001E+00 0.58416E+03 
c  k            0.27851E+01      78   0.10043E-01   0.57796E+02 0.20864E+04 
c  epsilon      0.52673E+05      56   0.97717E-02   0.99003E+10 0.14910E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026053                             2
a  epsilon         -767.63                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.839          57.394           3.383         0.37649
v  Velocity[Y]            -50.039          49.467          1.2531         0.86758
v  Velocity[Z]            -88.196          97.303         -1.7443     -0.00092731
v  ǁVelocityǁ           0.0020092           104.4          10.293          8.1552
v  Pressure           -1.2041e+06      6.6299e+05      3.5117e+05      3.1555e+05
v  k                   1.2048e-05           88.04         0.23159         0.15767
v  epsilon               0.029317      1.2831e+07           18930           187.5
v  TurbVisc            5.6445e-11         0.90573       0.0074063        0.054585
v  total_pressure      -7.041e+05       1.163e+06  c  Velocity     0.15538E+02     117   0.18955E+00   0.19417E+04 0.10028E+04 
c  Velocity[X]                                      0.58353E+03 
c  Velocity[Y]                                      0.60315E+03 
c  Velocity[Z]                                      0.75498E+03 
c  Pressure     0.21907E+00     768   0.62435E-02   0.33665E+00 0.63230E+03 
c  k            0.28501E+01      77   0.89245E-02   0.75846E+02 0.23329E+04 
c  epsilon      0.52574E+05      56   0.99479E-02   0.11929E+11 0.84553E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024977                             2
a  epsilon         -672.84                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.908          62.195          3.3979         0.37658
v  Velocity[Y]            -45.276          48.914          1.2485         0.86746
v  Velocity[Z]            -93.108          75.281          -1.732      -0.0013407
v  ǁVelocityǁ           0.0019687          108.86          10.283           8.155
v  Pressure           -1.2055e+06       6.628e+05      3.5102e+05      3.1532e+05
v  k                   1.1859e-05          85.736          0.2302         0.15636
v  epsilon               0.029151      1.2776e+07           18942          185.72
v  TurbVisc            5.5392e-11         0.90244       0.0073139        0.054437
v  total_pressure     -7.0548e+05      1.1628e+06      8.5102e+05      8.1532e+05


 TIME FOR THE TIME STEP              730:        0.69191E+02

===============================================================


 INSTANT    0.731000000E+03   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.117557124E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13402E+03 0.38535E+02
   Friction velocity        uet   :  0.39338E-01 0.80196E+01
   Friction velocity        uk    :  0.64683E-01 0.77269E+01
   Di   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15547E+02     117   0.19541E+00   0.18772E+04 0.99291E+03 
c  Velocity[X]                                      0.56791E+03 
c  Velocity[Y]                                      0.54535E+03 
c  Velocity[Z]                                      0.76399E+03 
c  Pressure     0.22289E+00     585   0.72141E-02   0.34001E+00 0.58416E+03 
c  k            0.27851E+01      78   0.10043E-01   0.57796E+02 0.20864E+04 
c  epsilon      0.52673E+05      56   0.97717E-02   0.99003E+10 0.14910E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026053                             2
a  epsilon         -767.63                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.839          57.394           3.383         0.37649
v  Velocity[Y]            -50.039          49.467          1.2531         0.86758
v  Velocity[Z]            -88.196          97.303         -1.7443     -0.00092731
v  ǁVelocityǁ           0.0020092           104.4          10.293          8.1552
v  Pressure           -1.2041e+06      6.6299e+05      3.5117e+05      3.1555e+05
v  k                   1.2048e-05           88.04         0.23159         0.15767
v  epsilon               0.029317      1.2831e+07           18930           187.5
v  TurbVisc            5.6445e-11         0.90573       0.0074063        0.054585
v  total_pressure      -7.041e+05       1.163e+06      8.5117e+05      8.1555e+05


 TIME FOR THE TIME STEP              732:        0.69803E+02

===============================================================


 INSTANT    0.733000000E+03   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15526E+02     117   0.19518E+00   0.19876E+04 0.10041E+04 
c  Velocity[X]                                      0.58272E+03 
c  Velocity[Y]                                      0.60162E+03 
c  Velocity[Z]                                      0.80322E+03 
c  Pressure     0.23555E+00     712   0.63742E-02   0.35249E+00 0.53903E+03 
c  k            0.25935E+01      80   0.99156E-02   0.37421E+02 0.17563E+04 
c  epsilon      0.49228E+05      57   0.10410E-01   0.77006E+10 0.85699E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002201                             2
a  epsilon         -784.35                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.818          58.834          3.3754         0.37549
v  Velocity[Y]            -47.522          46.088          1.2593         0.86802
v  Velocity[Z]            -89.243          112.49         -1.7555     -0.00081004
v  ǁVelocityǁ           0.0020749          115.25          10.305          8.1529
v  Pressure           -1.2077e+06      6.6172e+05      3.5006e+05      3.1496e+05
v  k                   1.2203e-05          86.737         0.23381         0.15899
v  epsilon               0.029188      1.2858e+07             Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15547E+02     117   0.19541E+00   0.18772E+04 0.99291E+03 
c  Velocity[X]                                      0.56791E+03 
c  Velocity[Y]                                      0.54535E+03 
c  Velocity[Z]                                      0.76399E+03 
c  Pressure     0.22289E+00     585   0.72141E-02   0.34001E+00 0.58416E+03 
c  k            0.27851E+01      78   0.10043E-01   0.57796E+02 0.20864E+04 
c  epsilon      0.52673E+05      56   0.97717E-02   0.99003E+10 0.14910E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026053                             2
a  epsilon         -767.63                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -25.839          57.394           3.383         0.37649
v  Velocity[Y]            -50.039          49.467          1.2531         0.86758
v  Velocity[Z]            -88.196          97.303         -1.7443     -0.00092731
v  ǁVelocityǁ           0.0020092           104.4          10.293          8.1552
v  Pressure           -1.2041e+06      6.6299e+05      3.5117e+05      3.1555e+05
v  k                   1.2048e-05           88.04         0.23159         0.15767
v  epsilon               0.029317      1.2831e+07           18930           187.5
v  TurbVisc            5.6445e-11         0.90573       0.0074063        0.054585
v  total_pressure      -7.041e+05       1.163e+06      8.5117e+05      8.1555e+05


 TIME FOR THE TIME STEP              732:        0.70577E+02

===============================================================


 INSTANT    0.733000000E+03   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.103060889E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160649E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15732E+03 0.38073E+02
   Friction velocity        uet   :  0.40414E-01 0.78009E+01
   Friction velocity        uk    :  0.61323E-01 0.77355E+01
   Dimensionless distance   yplus :  0.49905E-03 0.45346E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18880
   Nb of faces within the viscous sub-layer     :       7262
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15539E+02     117   0.19450E+00   0.18404E+04 0.98106E+03 
c  Velocity[X]                                      0.56011E+03 
c  Velocity[Y]                                      0.57150E+03 
c  Velocity[Z]                                      0.70882E+03 
c  Pressure     0.22469E+00     572   0.62673E-02   0.34026E+00 0.16670E+04 
c  k            0.27032E+01      79   0.84078E-02   0.38613E+02 0.18097E+04 
c  epsilon      0.51116E+05      57   0.91153E-02   0.79670E+10 0.16382E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010919                             1
a  epsilon         -811.68                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.141           55.81          3.3791         0.37673
v  Velocity[Y]            -57.001          80.295          1.2558         0.86728
v  Velocity[Z]            -84.413          91.539         -1.7497      -0.0008969
v  ǁVelocityǁ           0.0020195          103.99            10.3          8.1544
v  Pressure           -1.2062e+06      6.6122e+05      3.5027e+05      3.1508e+05
v  k                   1.2134e-05          85.968         0.23255         0.15836
v  epsilon               0.029278      1.2836e+07           18936          187.77
v  TurbVisc            5.6774e-11         0.93894       0.0074624        0.054661
v  total_pressure     -7.0622   Nb of faces within the viscous sub-layer     :       7239
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15512E+02     115   0.19434E+00   0.23818E+04 0.10381E+04 
c  Velocity[X]                                      0.57317E+03 
c  Velocity[Y]                                      0.60814E+03 
c  Velocity[Z]                                      0.12005E+04 
c  Pressure     0.23548E+00     753   0.67536E-02   0.35270E+00 0.23009E+03 
c  k            0.23208E+01      80   0.85494E-02   0.28182E+02 0.17422E+04 
c  epsilon      0.46309E+05      56   0.80346E-02   0.63556E+10 0.12266E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018772                             2
a  epsilon         -791.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.555          68.205           3.377         0.37554
v  Velocity[Y]            -55.243           45.61          1.2637         0.86737
v  Velocity[Z]            -111.92          75.365         -1.7616      -0.0012178
v  ǁVelocityǁ           0.0021175          129.41          10.316          8.1514
v  Pressure           -1.2035e+06       6.618e+05      3.5001e+05      3.1515e+   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15526E+02     117   0.19518E+00   0.19876E+04 0.10041E+04 
c  Velocity[X]                                      0.58272E+03 
c  Velocity[Y]                                      0.60162E+03 
c  Velocity[Z]                                      0.80322E+03 
c  Pressure     0.23555E+00     712   0.63742E-02   0.35249E+00 0.53903E+03 
c  k            0.25935E+01      80   0.99156E-02   0.37421E+02 0.17563E+04 
c  epsilon      0.49228E+05      57   0.10410E-01   0.77006E+10 0.85699E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002201                             2
a  epsilon         -784.35                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.818          58.834          3.3754         0.37549
v  Velocity[Y]            -47.522          46.088          1.2593         0.86802
v  Velocity[Z]            -89.243          112.49         -1.7555     -0.00081004
v  ǁVelocityǁ           0.0020749          115.25          10.305          8.1529
v  Pressure           -1.2077e+06      6.6172e+05      3.5006e+05      3.1496e+05
v  k                   1.2203e-05          86.737         0.23381         0.15899
v  epsilon               0.029188      1.2858e+07           18953          187.66
v  TurbVisc            5.7292e-11         0.94195        0.007537        0.054745
v  total_pressure     -7.0765e+05      1.1617e+06      8.5006e+05      8.1496e+05


 TIME FOR THE TIME STEP              734:        0.69546E+02

===============================================================


 INSTANT    0.735000000E+03   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.170173558E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
-----------------------------------------   Nb of faces within the viscous sub-layer     :       7239
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15512E+02     115   0.19434E+00   0.23818E+04 0.10381E+04 
c  Velocity[X]                                      0.57317E+03 
c  Velocity[Y]                                      0.60814E+03 
c  Velocity[Z]                                      0.12005E+04 
c  Pressure     0.23548E+00     753   0.67536E-02   0.35270E+00 0.23009E+03 
c  k            0.23208E+01      80   0.85494E-02   0.28182E+02 0.17422E+04 
c  epsilon      0.46309E+05      56   0.80346E-02   0.63556E+10 0.12266E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018772                             2
a  epsilon         -791.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.555          68.205           3.377         0.37554
v  Velocity[Y]            -55.243           45.61          1.2637         0.86737
v  Velocity[Z]            -111.92          75.365         -1.7616      -0.0012178
v  ǁVelocityǁ           0.0021175          129.41          10.316          8.1514
v  Pressure           -1.2035e+06       6.618e+05      3.5001e+05      3.1515e+05
v  k                   1.2273e-05          77.879         0.23696         0.16008
v  epsilon                0.02904      1.2842e+07           19010          185.45
v  TurbVisc            6.0261e-11         0.85582       0.0077405        0.054915
v  total_pressure     -7.0355e+05      1.1618e+06      8.5001e+05      8.1515e+05


 TIME FOR THE TIME STEP              736:        0.78380E+02

===============================================================


 INSTANT    0.737000000E+03   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUND   Dimensionless distance   yplus :  0.51274E-03 0.51201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18877
   Nb of faces within the viscous sub-layer     :       7230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15501E+02     114   0.19397E+00   0.21290E+04 0.10441E+04 
c  Velocity[X]                                      0.56497E+03 
c  Velocity[Y]                                      0.65192E+03 
c  Velocity[Z]                                      0.91215E+03 
c  Pressure     0.22828E+00     664   0.58708E-02   0.34139E+00 0.25175E+04 
c  k            0.22572E+01      80   0.76867E-02   0.25109E+02 0.15469E+04 
c  epsilon      0.46238E+05      55   0.74173E-02   0.90803E+10 0.81396E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022376                             2
a  epsilon         -1001.5                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.404          53.568          3.3847         0.37502
v  Velocity[Y]            -47.533          43.226          1.2683         0.86753
v  Velocity[Z]            -87.292          76.076         -   Nb of faces within the viscous sub-layer     :       7239
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15512E+02     115   0.19434E+00   0.23818E+04 0.10381E+04 
c  Velocity[X]                                      0.57317E+03 
c  Velocity[Y]                                      0.60814E+03 
c  Velocity[Z]                                      0.12005E+04 
c  Pressure     0.23548E+00     753   0.67536E-02   0.35270E+00 0.23009E+03 
c  k            0.23208E+01      80   0.85494E-02   0.28182E+02 0.17422E+04 
c  epsilon      0.46309E+05      56   0.80346E-02   0.63556E+10 0.12266E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018772                             2
a  epsilon         -791.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.555          68.205           3.377         0.37554
v  Velocity[Y]            -55.243           45.61          1.2637         0.86737
v  Velocity[Z]            -111.92          75.365         -1.7616      -0.0012178
v  ǁVelocityǁ           0.0021175          129.41          10.316          8.1514
v  Pressure           -1.2035e+06       6.618e+05      3.5001e+05      3.1515e+05
v  k                   1.2273e-05          77.879         0.23696         0.16008
v  epsilon                0.02904      1.2842e+07           19010          185.45
v  TurbVisc            6.0261e-11         0.85582       0.0077405        0.054915
v  total_pressure     -7.0355e+05      1.1618e+06      8.5001e+05      8.1515e+05


 TIME FOR THE TIME STEP              736:        0.68887E+02

===============================================================


 INSTANT    0.737000000E+03   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.688097231E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
-------------   Dimensionless distance   yplus :  0.51274E-03 0.51201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18877
   Nb of faces within the viscous sub-layer     :       7230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15501E+02     114   0.19397E+00   0.21290E+04 0.10441E+04 
c  Velocity[X]                                      0.56497E+03 
c  Velocity[Y]                                      0.65192E+03 
c  Velocity[Z]                                      0.91215E+03 
c  Pressure     0.22828E+00     664   0.58708E-02   0.34139E+00 0.25175E+04 
c  k            0.22572E+01      80   0.76867E-02   0.25109E+02 0.15469E+04 
c  epsilon      0.46238E+05      55   0.74173E-02   0.90803E+10 0.81396E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022376                             2
a  epsilon         -1001.5                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.404          53.568          3.3847         0.37502
v  Velocity[Y]            -47.533          43.226          1.2683         0.86753
v  Velocity[Z]            -87.292          76.076         -1.7658      -0.0013759
v  ǁVelocityǁ           0.0021656          101.46          10.328          8.1492
v  Pressure           -1.1994e+06      6.6153e+05      3.4963e+05       3.149e+05
v  k                   1.2228e-05           77.25         0.24147         0.16158
v  epsilon               0.029035      1.2848e+07           19102          185.71
v  TurbVisc            6.7959e-11         0.71019        0.008024        0.055106
v  total_pressure     -6.9938e+05      1.1615e+06      8.4963e+05       8.149e+05


 TIME FOR THE TIME STEP              738:        0.62120E+02

=========================   Rel velocity at the wall uiptn : -0.28263E+03 0.37531E+02
   Friction velocity        uet   :  0.28990E-01 0.86619E+01
   Friction velocity        uk    :  0.64265E-01 0.77390E+01
   Dimensionless distance   yplus :  0.52285E-03 0.53635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18858
   Nb of faces within the viscous sub-layer     :       7198
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15492E+02     114   0.19441E+00   0.18816E+04 0.98241E+03 
c  Velocity[X]                                      0.54518E+03 
c  Velocity[Y]                                      0.58435E+03 
c  Velocity[Z]                                      0.75211E+03 
c  Pressure     0.23558E+00     698   0.68465E-02   0.35314E+00 0.25967E+04 
c  k            0.21343E+01      80   0.87711E-02   0.23293E+02 0.14586E+04 
c  epsilon      0.44869E+05      55   0.73300E-02   0.47966E+10 0.21207E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028373                             3
a  epsilon         -992.67                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -27.651             Dimensionless distance   yplus :  0.51274E-03 0.51201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18877
   Nb of faces within the viscous sub-layer     :       7230
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15501E+02     114   0.19397E+00   0.21290E+04 0.10441E+04 
c  Velocity[X]                                      0.56497E+03 
c  Velocity[Y]                                      0.65192E+03 
c  Velocity[Z]                                      0.91215E+03 
c  Pressure     0.22828E+00     664   0.58708E-02   0.34139E+00 0.25175E+04 
c  k            0.22572E+01      80   0.76867E-02   0.25109E+02 0.15469E+04 
c  epsilon      0.46238E+05      55   0.74173E-02   0.90803E+10 0.81396E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022376                             2
a  epsilon         -1001.5                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -26.404          53.568          3.3847         0.37502
v  Velocity[Y]            -47.533          43.226          1.2683         0.86753
v  Velocity[Z]            -87.292          76.076         -1.7658      -0.0013759
v  ǁVelocityǁ           0.0021656          101.46          10.328          8.1492
v  Pressure           -1.1994e+06      6.6153e+05      3.4963e+05       3.149e+05
v  k                   1.2228e-05           77.25         0.24147         0.16158
v  epsilon               0.029035      1.2848e+07           19102          185.71
v  TurbVisc            6.7959e-11         0.71019        0.008024        0.055106
v  total_pressure     -6.9938e+05      1.1615e+06      8.4963e+05       8.149e+05


 TIME FOR THE TIME STEP              738:        0.71961E+02

===============================================================


 INSTANT    0.739000000E+03   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        -0.991977564E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         Rel velocity at the wall uiptn : -0.28263E+03 0.37531E+02
   Friction velocity        uet   :  0.28990E-01 0.86619E+01
   Friction velocity        uk    :  0.64265E-01 0.77390E+01
   Dimensionless distance   yplus :  0.52285E-03 0.53635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18858
   Nb of faces within the viscous sub-layer     :       7198
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15492E+02     114   0.19441E+00   0.18816E+04 0.98241E+03 
c  Velocity[X]                                      0.54518E+03 
c  Velocity[Y]                                      0.58435E+03 
c  Velocity[Z]                                      0.75211E+03 
c  Pressure     0.23558E+00     698   0.68465E-02   0.35314E+00 0.25967E+04 
c  k            0.21343E+01      80   0.87711E-02   0.23293E+02 0.14586E+04 
c  epsilon      0.44869E+05      55   0.73300E-02   0.47966E+10 0.21207E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028373                             3
a  epsilon         -992.67                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -27.651           60.95          3.4001         0.37563
v  Velocity[Y]             -48.62          50.298          1.2742         0.86667
v  Velocity[Z]            -92.373          83.015         -1.7652     -0.00084203
v  ǁVelocityǁ           0.0021885          107.44           10.34          8.1473
v  Pressure           -1.1971e+06      6.6023e+05      3.4983e+05      3.1509e+05
v  k                   1.2077e-05          74.278         0.24592         0.16301
v  epsilon               0.021984      1.2801e+07           19139          185.83
v  TurbVisc            8.2149e-11         0.66578       0.0083617     ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17064E+03 0.47737E+02
   Friction velocity        uet   :  0.31070E-01 0.72475E+01
   Friction velocity        uk    :  0.61380E-01 0.77505E+01
   Dimensionless distance   yplus :  0.51564E-03 0.46807E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18852
   Nb of faces within the viscous sub-layer     :       7178
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15466E+02     115   0.19349E+00   0.17919E+04 0.98252E+03 
c  Velocity[X]                                      0.53756E+03 
c  Velocity[Y]                                      0.54225E+03 
c  Velocity[Z]                                      0.71210E+03 
c  Pressure     0.24271E+00     765   0.62262E-02   0.36463E+00 0.77299E+03 
c  k            0.21259E+01      80   0.90990E-02   0.32654E+02 0.19379E+04 
c  epsilon      0.44285E+05      54   0.83082E-02   0.51191E+10 0.17655E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025508                             3
a  epsilon         -904.76                             1


  ** Computed fields on cells
     ------------------------

   field                   Rel velocity at the wall uiptn : -0.28263E+03 0.37531E+02
   Friction velocity        uet   :  0.28990E-01 0.86619E+01
   Friction velocity        uk    :  0.64265E-01 0.77390E+01
   Dimensionless distance   yplus :  0.52285E-03 0.53635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18858
   Nb of faces within the viscous sub-layer     :       7198
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15492E+02     114   0.19441E+00   0.18816E+04 0.98241E+03 
c  Velocity[X]                                      0.54518E+03 
c  Velocity[Y]                                      0.58435E+03 
c  Velocity[Z]                                      0.75211E+03 
c  Pressure     0.23558E+00     698   0.68465E-02   0.35314E+00 0.25967E+04 
c  k            0.21343E+01      80   0.87711E-02   0.23293E+02 0.14586E+04 
c  epsilon      0.44869E+05      55   0.73300E-02   0.47966E+10 0.21207E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028373                             3
a  epsilon         -992.67                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -27.651           60.95          3.4001         0.37563
v  Velocity[Y]             -48.62          50.298          1.2742         0.86667
v  Velocity[Z]            -92.373          83.015         -1.7652     -0.00084203
v  ǁVelocityǁ           0.0021885          107.44           10.34          8.1473
v  Pressure           -1.1971e+06      6.6023e+05      3.4983e+05      3.1509e+05
v  k                   1.2077e-05          74.278         0.24592         0.16301
v  epsilon               0.021984      1.2801e+07           19139          185.83
v  TurbVisc            8.2149e-11         0.66578       0.0083617        0.055315
v  total_pressure      -6.971e+05      1.1602e+06      8.4983e+05      8.1509e+05


 TIME FOR THE TIME STEP              740:        0.68066E+02

===============================================================


 INSTANT    0.741000000E+03   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        -0.272628499E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4    ------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17064E+03 0.47737E+02
   Friction velocity        uet   :  0.31070E-01 0.72475E+01
   Friction velocity        uk    :  0.61380E-01 0.77505E+01
   Dimensionless distance   yplus :  0.51564E-03 0.46807E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18852
   Nb of faces within the viscous sub-layer     :       7178
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15466E+02     115   0.19349E+00   0.17919E+04 0.98252E+03 
c  Velocity[X]                                      0.53756E+03 
c  Velocity[Y]                                      0.54225E+03 
c  Velocity[Z]                                      0.71210E+03 
c  Pressure     0.24271E+00     765   0.62262E-02   0.36463E+00 0.77299E+03 
c  k            0.21259E+01      80   0.90990E-02   0.32654E+02 0.19379E+04 
c  epsilon      0.44285E+05      54   0.83082E-02   0.51191E+10 0.17655E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025508                             3
a  epsilon         -904.76                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.036          59.333           3.417         0.37559
v  Velocity[Y]            -51.906          43.881           1.283         0.86673
v  Velocity[Z]             -86.82          78.699         -1.7684     -0.00069674
v  ǁVelocityǁ           0.0022034          101.57          10.357          8.1465
v  Pressure           -1.1935e+06      6.6163e+05      3.5081e+05      3.1587e+05
v  k                   1.1862e-05          74.979          0.2501         0.16447
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43307E+03 0.34027E+02
   Friction velocity        uet   :  0.42313E-01 0.11151E+02
   Friction velocity        uk    :  0.60155E-01 0.77582E+01
   Dimensionless distance   yplus :  0.52076E-03 0.47646E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18826
   Nb of faces within the viscous sub-layer     :       7159
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15475E+02     117   0.19316E+00   0.22480E+04 0.10557E+04 
c  Velocity[X]                                      0.56414E+03 
c  Velocity[Y]                                      0.57422E+03 
c  Velocity[Z]                                      0.11096E+04 
c  Pressure     0.22387E+00     589   0.54245E-02   0.33794E+00 0.11392E+04 
c  k            0.23568E+01      80   0.12182E-01   0.62288E+02 0.24451E+04 
c  epsilon      0.45519E+05      57   0.10388E-01   0.64235E+10 0.67281E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17064E+03 0.47737E+02
   Friction velocity        uet   :  0.31070E-01 0.72475E+01
   Friction velocity        uk    :  0.61380E-01 0.77505E+01
   Dimensionless distance   yplus :  0.51564E-03 0.46807E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18852
   Nb of faces within the viscous sub-layer     :       7178
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15466E+02     115   0.19349E+00   0.17919E+04 0.98252E+03 
c  Velocity[X]                                      0.53756E+03 
c  Velocity[Y]                                      0.54225E+03 
c  Velocity[Z]                                      0.71210E+03 
c  Pressure     0.24271E+00     765   0.62262E-02   0.36463E+00 0.77299E+03 
c  k            0.21259E+01      80   0.90990E-02   0.32654E+02 0.19379E+04 
c  epsilon      0.44285E+05      54   0.83082E-02   0.51191E+10 0.17655E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025508                             3
a  epsilon         -904.76                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.036          59.333           3.417         0.37559
v  Velocity[Y]            -51.906          43.881           1.283         0.86673
v  Velocity[Z]             -86.82          78.699         -1.7684     -0.00069674
v  ǁVelocityǁ           0.0022034          101.57          10.357          8.1465
v  Pressure           -1.1935e+06      6.6163e+05      3.5081e+05      3.1587e+05
v  k                   1.1862e-05          74.979          0.2501         0.16447
v  epsilon               0.029343       1.283e+07           19185          186.54
v  TurbVisc            8.6237e-11         0.67143       0.0087104        0.055529
v  total_pressure     -6.9352e+05      1.1616e+06      8.5081e+05      8.1587e+05


 TIME FOR THE TIME STEP              742:        0.74225E+02

===============================================================


 INSTANT    0.743000000E+03   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth ---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43307E+03 0.34027E+02
   Friction velocity        uet   :  0.42313E-01 0.11151E+02
   Friction velocity        uk    :  0.60155E-01 0.77582E+01
   Dimensionless distance   yplus :  0.52076E-03 0.47646E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18826
   Nb of faces within the viscous sub-layer     :       7159
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15475E+02     117   0.19316E+00   0.22480E+04 0.10557E+04 
c  Velocity[X]                                      0.56414E+03 
c  Velocity[Y]                                      0.57422E+03 
c  Velocity[Z]                                      0.11096E+04 
c  Pressure     0.22387E+00     589   0.54245E-02   0.33794E+00 0.11392E+04 
c  k            0.23568E+01      80   0.12182E-01   0.62288E+02 0.24451E+04 
c  epsilon      0.45519E+05      57   0.10388E-01   0.64235E+10 0.67281E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025912                             3
a  epsilon         -931.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -33.27          63.651          3.4343         0.37676
v  Velocity[Y]            -48.729          43.798          1.2937         0.86568
v  Velocity[Z]             -97.05          77.792         -1.7749     -0.00065358
v  ǁVelocityǁ           0.0021706          112.76     Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12710E+03 0.49661E+02
   Friction velocity        uet   :  0.28435E-01 0.75519E+01
   Friction velocity        uk    :  0.32342E-01 0.77627E+01
   Dimensionless distance   yplus :  0.51885E-03 0.42041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18750
   Nb of faces within the viscous sub-layer     :       7142
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15482E+02     114   0.18811E+00   0.17643E+04 0.97066E+03 
c  Velocity[X]                                      0.53897E+03 
c  Velocity[Y]                                      0.50711E+03 
c  Velocity[Z]                                      0.71818E+03 
c  Pressure     0.21717E+00     770   0.52597E-02   0.32582E+00 0.68215E+03 
c  k            0.21886E+01      81   0.12827E-01   0.91615E+02 0.31481E+04 
c  epsilon      0.45350E+05      56   0.10787E-01   0.10176E+11 0.20603E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43307E+03 0.34027E+02
   Friction velocity        uet   :  0.42313E-01 0.11151E+02
   Friction velocity        uk    :  0.60155E-01 0.77582E+01
   Dimensionless distance   yplus :  0.52076E-03 0.47646E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18826
   Nb of faces within the viscous sub-layer     :       7159
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15475E+02     117   0.19316E+00   0.22480E+04 0.10557E+04 
c  Velocity[X]                                      0.56414E+03 
c  Velocity[Y]                                      0.57422E+03 
c  Velocity[Z]                                      0.11096E+04 
c  Pressure     0.22387E+00     589   0.54245E-02   0.33794E+00 0.11392E+04 
c  k            0.23568E+01      80   0.12182E-01   0.62288E+02 0.24451E+04 
c  epsilon      0.45519E+05      57   0.10388E-01   0.64235E+10 0.67281E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025912                             3
a  epsilon         -931.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -33.27          63.651          3.4343         0.37676
v  Velocity[Y]            -48.729          43.798          1.2937         0.86568
v  Velocity[Z]             -97.05          77.792         -1.7749     -0.00065358
v  ǁVelocityǁ           0.0021706          112.76          10.374          8.1457
v  Pressure           -1.1944e+06      6.6281e+05      3.5161e+05      3.1636e+05
v  k                   1.1634e-05          91.753         0.25368         0.16617
v  epsilon               0.028983       1.282e+07           19220          189.02
v  TurbVisc            8.6436e-11         0.78897       0.0090398        0.055736
v  total_pressure     -6.9442e+05      1.1628e+06      8.5161e+05      8.1636e+05


 TIME FOR THE TIME STEP              744:        0.61845E+02

===============================================================


 INSTANT    0.745000000E+03   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
BouConvective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12710E+03 0.49661E+02
   Friction velocity        uet   :  0.28435E-01 0.75519E+01
   Friction velocity        uk    :  0.32342E-01 0.77627E+01
   Dimensionless distance   yplus :  0.51885E-03 0.42041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18750
   Nb of faces within the viscous sub-layer     :       7142
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15482E+02     114   0.18811E+00   0.17643E+04 0.97066E+03 
c  Velocity[X]                                      0.53897E+03 
c  Velocity[Y]                                      0.50711E+03 
c  Velocity[Z]                                      0.71818E+03 
c  Pressure     0.21717E+00     770   0.52597E-02   0.32582E+00 0.68215E+03 
c  k            0.21886E+01      81   0.12827E-01   0.91615E+02 0.31481E+04 
c  epsilon      0.45350E+05      56   0.10787E-01   0.10176E+11 0.20603E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024373                             3
a  epsilon         -934.31                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -21.26          57.965          3.4472         0.37576
v  Velocity[Y]            -5Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160651E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14969E+03 0.29731E+02
   Friction velocity        uet   :  0.29962E-01 0.82781E+01
   Friction velocity        uk    :  0.29921E-01 0.77539E+01
   Dimensionless distance   yplus :  0.50985E-03 0.49068E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18739
   Nb of faces within the viscous sub-layer     :       7127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15505E+02     114   0.19206E+00   0.15691E+04 0.93582E+03 
c  Velocity[X]                                      0.51002E+03 
c  Velocity[Y]                                      0.49951E+03 
c  Velocity[Z]                                      0.55955E+03 
c  Pressure     0.22852E+00     877   0.58392E-02   0.34231E+00 0.42429E+03 
c  k            0.18630E+01      84   0.11684E-01   0.48394E+02 0.25158E+04 
c  epsilon      0.42466E+05      60   0.99676E-02   0.74496E+10 0.97880E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027811                             3
a  epsilon         -721.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.983          64.108          3.4566         0.37562
v  Velocity[Y]            -51.244          47.797          1.3139         0.86488
v  Velocity[Z]            -101.29          133.39         -1.7879      -0.0010583
v  ǁVelocityǁ           0.0020838          140.46          10.408          8.1496
v  Pressure           -1.2031e+06      6.6556e+05      3.5229e+05      3.1713e+05
v  k                    5.227e-06          60.468          0.2585         0.16866
v  epsilon               0.027881      1.2791e+07           19240           186.1
v  TurbVisc            8.5214e-11         0.51531       0.0095673        0.056146
v  total_pressure     -7.0308e+05      1.1656e+06      8.5229e+05      8.1713e+05


 TIME FOR THE TIME STEP              748:        0.79640E+02

===============================================================


 INSTANT    0.749000000E+03   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         0.533558103E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29745E+03 0.48229E+02
   Friction velocity        uet   :  0.38865E-01 0.90966E+01
   Friction velocity        uk    :  0.74808E-01 0.77502E+01
   Dimensionless distance   yplus :  0.50730E-03 0.45425E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18720
   Nb of faces within the viscous sub-layer     :       7110
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
------------Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160651E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14969E+03 0.29731E+02
   Friction velocity        uet   :  0.29962E-01 0.82781E+01
   Friction velocity        uk    :  0.29921E-01 0.77539E+01
   Dimensionless distance   yplus :  0.50985E-03 0.49068E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18739
   Nb of faces within the viscous sub-layer     :       7127
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15505E+02     114   0.19206E+00   0.15691E+04 0.93582E+03 
c  Velocity[X]                                      0.51002E+03 
c  Velocity[Y]                                      0.49951E+03 
c  Velocity[Z]                                      0.55955E+03 
c  Pressure     0.22852E+00     877   0.58392E-02   0.34231E+00 0.42429E+03 
c  k            0.18630E+01      84   0.11684E-01   0.48394E+02 0.25158E+04 
c  epsilon      0.42466E+05      60   0.99676E-02   0.74496E+10 0.97880E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027811                             3
a  epsilon         -721.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.137741228E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160662E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14522E+03 0.34454E+02
   Friction velocity        uet   :  0.38480E-01 0.74383E+01
   Friction velocity        uk    :  0.59734E-01 0.77653E+01
   Dimensionless distance   yplus :  0.50638E-03 0.44141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     115   0.19318E+00   0.17444E+04 0.94788E+03 
c  Velocity[X]                                      0.54376E+03 
c  Velocity[Y]                                      0.52012E+03 
c  Velocity[Z]                                      0.68049E+03 
c  Pressure     0.21988E+00     695   0.54609E-02   0.33217E+00 0.21120E+04 
c  k            0.18694E+01      86   0.62455E-02   0.20235E+02 0.18198E+04 
c  epsilon      0.42240E+05      59   0.53241E-02   0.35762E+10 0.16880E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002456                             3
a  epsilon         -510.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.093          55.144          3.4642         0.37542
v  Velocity[Y]            -50.199          52.495          1.3165           0.865
v  Velocity[Z]            -82.887          119.27         -1.7892     -0.00069405
v  ǁVelocityǁ           0.0020764          130.55          10.419          8.1511
v  Pressure           -1.2148e+06      6.6435e+05      3.5099e+05       3.164e+05
v  k                    1.049e-05          64.601         0.26066         0.17013
v  epsilon               0.027068      1.2815e+07           19265          186.61
v  TurbVisc            8.4512e-11         0.57949       0.0097713        0.056348
v  total_pressure     -7.1476e+05      1.1644e+06      8.5099e+05       8.164e+05


 TIME FOR THE TIME STEP              750:        0.70339E+02

===============================================================


 INSTANT    0.751000000E+03   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        -0.134275356E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31711E+03 0.35068E+02
   Friction velocity        uet   :  0.30511E-01 0.94650E+01
   Friction velocity        uk    :  0.62432E-01 0.77360E+01
   Dimensionless distance   yplus :  0.50595E-03 0.43486E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18723
   Nb of faces within the viscous sub-layer     :       7123
   Total nuInlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.137741228E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160662E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14522E+03 0.34454E+02
   Friction velocity        uet   :  0.38480E-01 0.74383E+01
   Friction velocity        uk    :  0.59734E-01 0.77653E+01
   Dimensionless distance   yplus :  0.50638E-03 0.44141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     115   0.19318E+00   0.17444E+04 0.94788E+03 
c  Velocity[X]                                      0.54376E+03 
c  Velocity[Y]                                      0.52012E+03 
c  Velocity[Z]                                      0.68049E+03 
c  Pressure     0.21988E+00     695   0.54609E-02   0.33217E+00 0.21120E+04 
c  k            0.18694E+01      86   0.62455E-02   0.20235E+02 0.18198E+04 
c  epsilon      0.42240E+05      59   0.53241E-02   0.35762E+10 0.16880E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002456                             3
a  epsilon    ---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.461268409E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11074E+03 0.31647E+02
   Friction velocity        uet   :  0.14655E-01 0.75550E+01
   Friction velocity        uk    :  0.54116E-01 0.77961E+01
   Dimensionless distance   yplus :  0.50868E-03 0.40665E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18739
   Nb of faces within the viscous sub-layer     :       7121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15548E+02     115   0.18739E+00   0.16479E+04 0.96055E+03 
c  Velocity[X]Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.137741228E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160662E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14522E+03 0.34454E+02
   Friction velocity        uet   :  0.38480E-01 0.74383E+01
   Friction velocity        uk    :  0.59734E-01 0.77653E+01
   Dimensionless distance   yplus :  0.50638E-03 0.44141E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18721
   Nb of faces within the viscous sub-layer     :       7118
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     115   0.19318E+00   0.17444E+04 0.94788E+03 
c  Velocity[X]                                      0.54376E+03 
c  Velocity[Y]                                      0.52012E+03 
c  Velocity[Z]                                      0.68049E+03 
c  Pressure     0.21988E+00     695   0.54609E-02   0.33217E+00 0.21120E+04 
c  k            0.18694E+01      86   0.62455E-02   0.20235E+02 0.18198E+04 
c  epsilon      0.42240E+05      59   0.53241E-02   0.35762E+10 0.16880E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002456                             3
a  epsilon         -510.66                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.093          55.144          3.4642         0.37542
v  Velocity[Y]            -50.199          52.495          1.3165           0.865
v  Velocity[Z]            -82.887          119.27         -1.7892     -0.00069405
v  ǁVelocityǁ           0.0020764          130.55          10.419          8.1511
v  Pressure           -1.2148e+06      6.6435e+05      3.5099e+05       3.164e+05
v  k                    1.049e-05          64.601         0.26066         0.17013
v  epsilon               0.027068      1.2815e+07           19265          18---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.461268409E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11074E+03 0.31647E+02
   Friction velocity        uet   :  0.14655E-01 0.75550E+01
   Friction velocity        uk    :  0.54116E-01 0.77961E+01
   Dimensionless distance   yplus :  0.50868E-03 0.40665E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18739
   Nb of faces within the viscous sub-layer     :       7121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15548E+02     115   0.18739E+00   0.16479E+04 0.96055E+03 
c  Velocity[X]                                      0.53229E+03 
c  Velocity[Y]                                      0.50228E+03 
c  Velocity[Z]                                      0.61329E+03 
c  Pressure     0.19642E+00     716   0.53225E-02   0.29473E+00 0.17944E+04 
c  k            0.19680E+01      85   0.58028E-02   0.12786E+02 0.15193E+04 
c  epsilon      0.43026E+05      58   0.48577E-02   0.30424E+11 0.80277E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.294760376E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11626E+03 0.33693E+02
   Friction velocity        uet   :  0.40212E-01 0.75270E+01
   Friction velocity        uk    :  0.47440E-01 0.77769E+01
   Dimensionless distance   yplus :  0.50465E-03 0.41764E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18757
   Nb of faces within the viscous sub-layer     :       7129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      de---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.461268409E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11074E+03 0.31647E+02
   Friction velocity        uet   :  0.14655E-01 0.75550E+01
   Friction velocity        uk    :  0.54116E-01 0.77961E+01
   Dimensionless distance   yplus :  0.50868E-03 0.40665E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18739
   Nb of faces within the viscous sub-layer     :       7121
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15548E+02     115   0.18739E+00   0.16479E+04 0.96055E+03 
c  Velocity[X]                                      0.53229E+03 
c  Velocity[Y]                                      0.50228E+03 
c  Velocity[Z]                                      0.61329E+03 
c  Pressure     0.19642E+00     716   0.53225E-02   0.29473E+00 0.17944E+04 
c  k            0.19680E+01      85   0.58028E-02   0.12786E+02 0.15193E+04 
c  epsilon      0.43026E+05      58   0.48577E-02   0.30424E+11 0.80277E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025157                             3
a  epsilon         -467.33                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.464           59.83          3.4692          0.3747
v  Velocity[Y]            -49.075          45.283          1.3128         0.86465
v  Velocity[Z]            -102.88          76.261         -1.7872      -0.0015676
v  ǁVelocityǁ           0.0021003          117.26          10.418          8.1532
v  Pressure           -1.2239e+06       6.633e+05      3.4897e+05      3.1504e+05
v  k             ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.294760376E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11626E+03 0.33693E+02
   Friction velocity        uet   :  0.40212E-01 0.75270E+01
   Friction velocity        uk    :  0.47440E-01 0.77769E+01
   Dimensionless distance   yplus :  0.50465E-03 0.41764E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18757
   Nb of faces within the viscous sub-layer     :       7129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15540E+02     115   0.18962E+00   0.19237E+04 0.99039E+03 
c  Velocity[X]                                      0.59192E+03 
c  Velocity[Y]                                      0.56861E+03 
c  Velocity[Z]                                      0.76319E+03 
c  Pressure     0.20610E+00     638   0.52986E-02   0.31012E+00 0.17243E+04 
c  k            0.18972E+01      85   0.76039E-02   0.19002E+02 0.16059E+04 
c  epsilon      0.42750E+05      58   0.61242E-02   0.34480E+10 0.19688E+06 
----------------------------------- TIME FOR THE TIME STEP              755:        0.70293E+02

===============================================================


 INSTANT    0.756000000E+03   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        -0.150466478E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10182E+03 0.37118E+02
   Friction velocity        uet   :  0.37098E-01 0.76047E+01
   Friction velocity        uk    :  0.68725E-01 0.77718E+01
   Dimensionless distance   yplus :  0.50686E-03 0.40281E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18689
   Nb of faces within the viscous sub-layer     :       7137
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------- ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.294760376E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.11626E+03 0.33693E+02
   Friction velocity        uet   :  0.40212E-01 0.75270E+01
   Friction velocity        uk    :  0.47440E-01 0.77769E+01
   Dimensionless distance   yplus :  0.50465E-03 0.41764E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18757
   Nb of faces within the viscous sub-layer     :       7129
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15540E+02     115   0.18962E+00   0.19237E+04 0.99039E+03 
c  Velocity[X]                                      0.59192E+03 
c  Velocity[Y]                                      0.56861E+03 
c  Velocity[Z]                                      0.76319E+03 
c  Pressure     0.20610E+00     638   0.52986E-02   0.31012E+00 0.17243E+04 
c  k            0.18972E+01      85   0.76039E-02   0.19002E+02 0.16059E+04 
c  epsilon      0.42750E+05      58   0.61242E-02   0.34480E+10 0.19688E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026721                             3
a  epsilon         -584.12                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.725          55.358          3.4713         0.37556
v  Velocity[Y]            -46.365           53.56          1.3038         0.86567
v  Velocity[Z]             -80.35          111.39          -1.777      -0 TIME FOR THE TIME STEP              755:        0.70080E+02

===============================================================


 INSTANT    0.756000000E+03   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        -0.150466478E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10182E+03 0.37118E+02
   Friction velocity        uet   :  0.37098E-01 0.76047E+01
   Friction velocity        uk    :  0.68725E-01 0.77718E+01
   Dimensionless distance   yplus :  0.50686E-03 0.40281E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18689
   Nb of faces within the viscous sub-layer     :       7137
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15574E+02     117   0.19400E+00   0.18752E+04 0.98260E+03 
c  Velocity[X]                                      0.54974E+03 
c  Velocity[Y]                                      0.57969E+03 
c  Velocity[Z]                                      0.74582E+03 
c  Pressure     0.25619E+00     652   0.55996E-02   0.38555E+00 0.19244E+04 
c  k            0.18058v  TurbVisc            8.3793e-11         0.52199        0.010166        0.057198
v  total_pressure     -7.3405e+05       1.162e+06      8.4606e+05      8.1276e+05


 TIME FOR THE TIME STEP              757:        0.68100E+02

===============================================================


 INSTANT    0.758000000E+03   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.135127605E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160660E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14417E+03 0.31796E+02
   Friction velocity        uet   :  0.25283E-01 0.74341E+01
   Friction velocity        uk    :  0.71484E-01 0.77630E+01
   Dimensionless distance   yplus :  0.51245E-03 0.44373E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       TIME FOR THE TIME STEP              755:        0.79293E+02

===============================================================


 INSTANT    0.756000000E+03   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        -0.150466478E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160653E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.10182E+03 0.37118E+02
   Friction velocity        uet   :  0.37098E-01 0.76047E+01
   Friction velocity        uk    :  0.68725E-01 0.77718E+01
   Dimensionless distance   yplus :  0.50686E-03 0.40281E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18689
   Nb of faces within the viscous sub-layer     :       7137
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15574E+02     117   0.19400E+00   0.18752E+04 0.98260E+03 
c  Velocity[X]                                      0.54974E+03 
c  Velocity[Y]                                      0.57969E+03 
c  Velocity[Z]                                      0.74582E+03 
c  Pressure     0.25619E+00     652   0.55996E-02   0.38555E+00 0.19244E+04 
c  k            0.18058E+01      85   0.73127E-02   0.19785E+02 0.15798E+04 
c  epsilon      0.41402E+05      58   0.54344E-02   0.30740E+11 0.74592E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024426                             3
a  epsilon          -614.3                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -24.112          56.451          3.4694         0.37542
v  Velocity[Y]            -60.377          43.462          1.2878         0.86596
v  Velocity[Z]            -113.39          82.222         -1.7638      -0.0014206
v  ǁVelocityǁ           0.0021024          118.77          10.391           8.154
v  Pressure           -1.2292e+06      6.6318e+05      3.4713e+05      3.1367e+05
v  k                   1.0114e-05          56.897         0.26407         0.17475
v  epsilon               0.012213      1.2853e+07           19246          188.44
v  TurbVisc            8.4035e-11         0.52812        0.010129        0.057061
v  total_pressure     -7.2919e+05      1.1632e+06      8.4713e+05      8.1367e+05


 TIME FOR THE TIME STEP              756:        0.73160E+02

===============================================================


 INSTANT    0.757000000E+03   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.306720376E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160621E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33824E+03 0.39704E+02
   Friction velocity        uet   :  0.12925E-01 0.95422E+01
   Friction velocity        uk    :  0.73954E-01 0.77315E+01
   Dimensionless distance   yplus :  0.50927E-03 0.40539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18687
   Nb of faces within the viscous sub-layer     :       7133
   Total number of wall faces                   :      41000
------------------------------------------------------------



   v  k                   1.0337e-05          68.755         0.26606         0.17861
v  epsilon               0.018644      1.2941e+07           19128          195.89
v  TurbVisc            8.3795e-11         0.69224        0.010252        0.057514
v  total_pressure     -7.3369e+05      1.1606e+06      8.4462e+05      8.1164e+05


 TIME FOR THE TIME STEP              759:        0.73601E+02

===============================================================


 INSTANT    0.760000000E+03   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.138978592E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160650E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20745E+03 0.31421E+02
   Friction velocity        uet   :  0.41438E-01 0.85277E+01
   Friction velocity        uk    :  0.63535E-01 0.77781E+01
   Dimensionless distance   yplus :  0.51077E-03 0.47321E+02
   -----v  TurbVisc            8.3793e-11         0.52199        0.010166        0.057198
v  total_pressure     -7.3405e+05       1.162e+06      8.4606e+05      8.1276e+05


 TIME FOR THE TIME STEP              757:        0.78156E+02

===============================================================


 INSTANT    0.758000000E+03   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.135127605E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160660E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14417E+03 0.31796E+02
   Friction velocity        uet   :  0.25283E-01 0.74341E+01
   Friction velocity        uk    :  0.71484E-01 0.77630E+01
   Dimensionless distance   yplus :  0.51245E-03 0.44373E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18685
   Nb of faces within the viscous sub-layer     :       7151
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15562E+02     117   0.18868E+00   0.17534E+04 0.97698E+03 
c  Velocity[X]                                      0.58603E+03 
c  Velocity[Y]                                      0.53650E+03 
c  Velocity[Z]                                      0.63087E+03 
c  Pressure     0.19409E+00     630   0.53436E-02   0.29386E+00 0.10267E+04 
c  k            0.19207E+01      84   0.95136E-02   0.44067E+02 0.18303E+04 
c  epsilon      0.41508E+05      58   0.78543E-02   0.58394E+10 0.15325E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024834                             3
a  epsilon         -566.89                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.875          53.552          3.4625         0.37552
v  Velocity[Y]            -46.334          48.319          1.2663          0.8662
v  Velocity[Z]              -81.2          94.139         -1.7467      -0.0012081
v  ǁVelocityǁ           0.0021106          101.51          10.367          8.1525
v  Pressure           -1.2324e+06      6.6281e+05      3.4608e+05      3.1274e+05
v  k                   1.0276e-05          64.524         0.26535         0.17718
v  epsilon               0.018344      1.2823e+07           19159          192.96
v  TurbVisc            8.3946e-11         0.56961        0.010209        0.057353
v  total_pressure     -7.3237e+05      1.1628e+06      8.4608e+05      8.1274e+05


 TIME FOR THE TIME STEP              758:        0.73363E+02

===============================================================


 INSTANT    0.759000000E+03   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.305812192E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160614E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17809E+03 0.34554E+02
   Friction velocity        uet   :  0.25747E-01 0.70609E+01
   Friction velocity        uk    :  0.25795E-01 0.77452E+01
   Dimensionless distance   yplus :  0.51003E-03 0.47085E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18613
   Nb of faces within tv  ǁVelocityǁ           0.0021039          100.09          10.324          8.1516
v  Pressure           -1.2313e+06      6.5915e+05      3.4416e+05      3.1109e+05
v  k                   1.0363e-05          78.743         0.26761         0.18163
v  epsilon              0.0019117      1.2979e+07           19061          203.82
v  TurbVisc            8.4324e-11         0.85833        0.010349        0.057871
v  total_pressure     -7.3128e+05      1.1592e+06      8.4416e+05      8.1109e+05


 TIME FOR THE TIME STEP              761:        0.65311E+02

===============================================================


 INSTANT    0.762000000E+03   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.171264805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160642E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16444E+03 0.31955E+02
   Friction velocity       v  k                   1.0337e-05          68.755         0.26606         0.17861
v  epsilon               0.018644      1.2941e+07           19128          195.89
v  TurbVisc            8.3795e-11         0.69224        0.010252        0.057514
v  total_pressure     -7.3369e+05      1.1606e+06      8.4462e+05      8.1164e+05


 TIME FOR THE TIME STEP              759:        0.66698E+02

===============================================================


 INSTANT    0.760000000E+03   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.138978592E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160650E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20745E+03 0.31421E+02
   Friction velocity        uet   :  0.41438E-01 0.85277E+01
   Friction velocity        uk    :  0.63535E-01 0.77781E+01
   Dimensionless distance   yplus :  0.51077E-03 0.47321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18560
   Nb of faces within the viscous sub-layer     :       7150
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15566E+02     117   0.19089E+00   0.18119E+04 0.97739E+03 
c  Velocity[X]                                      0.55238E+03 
c  Velocity[Y]                                      0.58225E+03 
c  Velocity[Z]                                      0.67732E+03 
c  Pressure     0.21268E+00     552   0.66133E-02   0.32137E+00 0.11297E+04 
c  k            0.22042E+01      83   0.79857E-02   0.53108E+02 0.17916E+04 
c  epsilon      0.42960E+05      59   0.69396E-02   0.56974E+10 0.64240E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023962                             3
a  epsilon         -620.7v  ǁVelocityǁ           0.0021039          100.09          10.324          8.1516
v  Pressure           -1.2313e+06      6.5915e+05      3.4416e+05      3.1109e+05
v  k                   1.0363e-05          78.743         0.26761         0.18163
v  epsilon              0.0019117      1.2979e+07           19061          203.82
v  TurbVisc            8.4324e-11         0.85833        0.010349        0.057871
v  total_pressure     -7.3128e+05      1.1592e+06      8.4416e+05      8.1109e+05


 TIME FOR THE TIME STEP              761:        0.73207E+02

===============================================================


 INSTANT    0.762000000E+03   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.171264805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160642E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16444E+03 0.31955E+02
   Friction velocity        uet   :  0.37919E-01 0.72138E+01
   Friction velocity        uk    :  0.68668E-01 0.77607E+01
   Dimensionless distance   yplus :  0.50927E-03 0.44957E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18477
   Nb of faces within the viscous sub-layer     :       7180
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_itev  Velocity[Y]            -47.688          44.068          1.1985         0.86704
v  Velocity[Z]            -93.075          73.846         -1.7189      -0.0018532
v  ǁVelocityǁ           0.0021442          109.26          10.302          8.1533
v  Pressure            -1.234e+06      6.5871e+05      3.4395e+05      3.1079e+05
v  k                   1.0292e-05          86.635         0.26867           0.184
v  epsilon               0.026402      1.2911e+07           18978           206.3
v  TurbVisc            8.5089e-11         0.98956        0.010464        0.058239
v  total_pressure       -7.34e+05      1.1587e+06      8.4395e+05      8.1079e+05


 TIME FOR THE TIME STEP              763:        0.67193E+02

===============================================================


 INSTANT    0.764000000E+03   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.162147377E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minv  ǁVelocityǁ           0.0021039          100.09          10.324          8.1516
v  Pressure           -1.2313e+06      6.5915e+05      3.4416e+05      3.1109e+05
v  k                   1.0363e-05          78.743         0.26761         0.18163
v  epsilon              0.0019117      1.2979e+07           19061          203.82
v  TurbVisc            8.4324e-11         0.85833        0.010349        0.057871
v  total_pressure     -7.3128e+05      1.1592e+06      8.4416e+05      8.1109e+05


 TIME FOR THE TIME STEP              761:        0.69510E+02

===============================================================


 INSTANT    0.762000000E+03   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.171264805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160642E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16444E+03 0.31955E+02
   Friction velocity        uet   :  0.37919E-01 0.72138E+01
   Friction velocity        uk    :  0.68668E-01 0.77607E+01
   Dimensionless distance   yplus :  0.50927E-03 0.44957E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18477
   Nb of faces within the viscous sub-layer     :       7180
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15561E+02     116   0.19369E+00   0.18134E+04 0.97763E+03 
c  Velocity[X]                                      0.55467E+03 
c  Velocity[Y]                                      0.54592E+03 
c  Velocity[Z]                                      0.71280E+03 
c  Pressure     0.19877E+00     575   0.59620E-02   0.30158E+00 0.15971E+04 
c  k            0.23789E+01      82   0.61056E-02   0.34657E+02 0.16086E+04 
c  epsilon      0.44229E+05      59   0.63237E-02   0.72427E+10 0.13399E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clv  Velocity[Y]            -47.688          44.068          1.1985         0.86704
v  Velocity[Z]            -93.075          73.846         -1.7189      -0.0018532
v  ǁVelocityǁ           0.0021442          109.26          10.302          8.1533
v  Pressure            -1.234e+06      6.5871e+05      3.4395e+05      3.1079e+05
v  k                   1.0292e-05          86.635         0.26867           0.184
v  epsilon               0.026402      1.2911e+07           18978           206.3
v  TurbVisc            8.5089e-11         0.98956        0.010464        0.058239
v  total_pressure       -7.34e+05      1.1587e+06      8.4395e+05      8.1079e+05


 TIME FOR THE TIME STEP              763:        0.70887E+02

===============================================================


 INSTANT    0.764000000E+03   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.162147377E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13531E+03 0.32705E+02
   Friction velocity        uet   :  0.40469E-01 0.79040E+01
   Friction velocity        uk    :  0.62873E-01 0.77661E+01
   Dimensionless distance   yplus :  0.51472E-03 0.44730E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18414
   Nb of faces within the viscous sub-layer     :       7196
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMAT-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.129          63.728          3.4312         0.37651
v  Velocity[Y]             -46.08          42.716          1.1749         0.86782
v  Velocity[Z]            -104.27          95.055         -1.7147      -0.0014025
v  ǁVelocityǁ           0.0021228          120.33          10.284          8.1538
v  Pressure           -1.2391e+06        6.58e+05      3.4371e+05      3.1041e+05
v  k                   1.0204e-05          88.457         0.27045          0.1862
v  epsilon               0.018131      1.2939e+07           18946          207.51
v  TurbVisc            8.5106e-11         0.91528        0.010624        0.058608
v  total_pressure     -7.3912e+05       1.158e+06      8.4371e+05      8.1041e+05


 TIME FOR THE TIME STEP              765:        0.60804E+02

===============================================================


 INSTANT    0.766000000E+03   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        -0.321303235E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160640E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS Fv  Velocity[Y]            -47.688          44.068          1.1985         0.86704
v  Velocity[Z]            -93.075          73.846         -1.7189      -0.0018532
v  ǁVelocityǁ           0.0021442          109.26          10.302          8.1533
v  Pressure            -1.234e+06      6.5871e+05      3.4395e+05      3.1079e+05
v  k                   1.0292e-05          86.635         0.26867           0.184
v  epsilon               0.026402      1.2911e+07           18978           206.3
v  TurbVisc            8.5089e-11         0.98956        0.010464        0.058239
v  total_pressure       -7.34e+05      1.1587e+06      8.4395e+05      8.1079e+05


 TIME FOR THE TIME STEP              763:        0.66338E+02

===============================================================


 INSTANT    0.764000000E+03   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.162147377E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160652E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13531E+03 0.32705E+02
   Friction velocity        uet   :  0.40469E-01 0.79040E+01
   Friction velocity        uk    :  0.62873E-01 0.77661E+01
   Dimensionless distance   yplus :  0.51472E-03 0.44730E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18414
   Nb of faces within the viscous sub-layer     :       7196
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15561E+02     115   0.19549E+00   0.19772E+04 0.98918E+03 
c  Velocity[X]                                      0.58561E+03 
c  Velocity[Y]                                      0.55748E+03 
c  Velocity[Z]                                      0.83411E+03 
c  Pressure     0.24229E+00     682   0.77464E-02   0.36857E+00 0.15745E+04 
c  k            0.24567E+01      82   0.70392E-02   0.28509E+02 0.13949E+04 
c  epsilon      0.45256E+05      58   0.71255E-02   0.46750E+10 0.69686E+05 
-----------------------------------------------------  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.129          63.728          3.4312         0.37651
v  Velocity[Y]             -46.08          42.716          1.1749         0.86782
v  Velocity[Z]            -104.27          95.055         -1.7147      -0.0014025
v  ǁVelocityǁ           0.0021228          120.33          10.284          8.1538
v  Pressure           -1.2391e+06        6.58e+05      3.4371e+05      3.1041e+05
v  k                   1.0204e-05          88.457         0.27045          0.1862
v  epsilon               0.018131      1.2939e+07           18946          207.51
v  TurbVisc            8.5106e-11         0.91528        0.010624        0.058608
v  total_pressure     -7.3912e+05       1.158e+06      8.4371e+05      8.1041e+05


 TIME FOR THE TIME STEP              765:        0.60323E+02

===============================================================


 INSTANT    0.766000000E+03   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        -0.321303235E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160640E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16632E+03 0.40955E+02
   Friction velocity        uet   :  0.36874E-01 0.88877E+01
   Friction velocity        uk    :  0.50856E-01 0.77343E+01
   Dimensionless distance   yplus :  0.51117E-03 0.45247E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18358
   Nb of faces within the viscous sub-layer     :       
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.246          54.661          3.4276         0.37534
v  Velocity[Y]            -45.335           42.38           1.162         0.86909
v  Velocity[Z]            -86.838          75.642         -1.7133      -0.0013467
v  ǁVelocityǁ           0.0021496          101.36          10.274           8.152
v  Pressure            -1.234e+06      6.5745e+05      3.4397e+05      3.1044e+05
v  k                    1.013e-05          81.964         0.27278         0.18834
v  epsilon               0.025949      1.2942e+07           18919           209.5
v  TurbVisc            8.5825e-11         0.76398        0.010799        0.058956
v  total_pressure     -7.3398e+05      1.1574e+06      8.4397e+05      8.1044e+05


 TIME FOR THE TIME STEP              767:        0.67518E+02

===============================================================


 INSTANT    0.768000000E+03   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         0.746476894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160611E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.0000000-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.129          63.728          3.4312         0.37651
v  Velocity[Y]             -46.08          42.716          1.1749         0.86782
v  Velocity[Z]            -104.27          95.055         -1.7147      -0.0014025
v  ǁVelocityǁ           0.0021228          120.33          10.284          8.1538
v  Pressure           -1.2391e+06        6.58e+05      3.4371e+05      3.1041e+05
v  k                   1.0204e-05          88.457         0.27045          0.1862
v  epsilon               0.018131      1.2939e+07           18946          207.51
v  TurbVisc            8.5106e-11         0.91528        0.010624        0.058608
v  total_pressure     -7.3912e+05       1.158e+06      8.4371e+05      8.1041e+05


 TIME FOR THE TIME STEP              765:        0.66572E+02

===============================================================


 INSTANT    0.766000000E+03   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        -0.321303235E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160640E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16632E+03 0.40955E+02
   Friction velocity        uet   :  0.36874E-01 0.88877E+01
   Friction velocity        uk    :  0.50856E-01 0.77343E+01
   Dimensionless distance   yplus :  0.51117E-03 0.45247E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18358
   Nb of faces within the viscous sub-layer     :       7188
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15551E+02     115   0.19090E+00   0.20650E+04 0.10239E+04 
c  Velocity[X]                                      0.61215E+03 
c  Velocity[Y]                                      0.59828E+03 
c  Velocity[Z]                                      0.85456E+03 
c  Pressure     0.20919E+00     712   0.58558E-02   0.31822E+00 0.56209E+03 
c  k            0.24896E+01      81   0.10602E-01   0.57076E+0
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.246          54.661          3.4276         0.37534
v  Velocity[Y]            -45.335           42.38           1.162         0.86909
v  Velocity[Z]            -86.838          75.642         -1.7133      -0.0013467
v  ǁVelocityǁ           0.0021496          101.36          10.274           8.152
v  Pressure            -1.234e+06      6.5745e+05      3.4397e+05      3.1044e+05
v  k                    1.013e-05          81.964         0.27278         0.18834
v  epsilon               0.025949      1.2942e+07           18919           209.5
v  TurbVisc            8.5825e-11         0.76398        0.010799        0.058956
v  total_pressure     -7.3398e+05      1.1574e+06      8.4397e+05      8.1044e+05


 TIME FOR THE TIME STEP              767:        0.64365E+02

===============================================================


 INSTANT    0.768000000E+03   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         0.746476894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160611E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13011E+03 0.38954E+02
   Friction velocity        uet   :  0.32510E-01 0.73471E+01
   Friction velocity        uk    :  0.35076E-01 0.77600E+01
   Dimensionless distance   yplus :  0.51533E-03 0-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010837                             1
a  epsilon         -840.02                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.527          63.092           3.432         0.37514
v  Velocity[Y]            -44.765          42.232          1.1633         0.86861
v  Velocity[Z]            -116.32          93.268         -1.7118      -0.0013516
v  ǁVelocityǁ           0.0022099          133.23          10.277          8.1512
v  Pressure            -1.232e+06      6.5649e+05      3.4446e+05      3.1077e+05
v  k                   1.0149e-05          79.807         0.27479         0.19055
v  epsilon               0.026198      1.2929e+07           18930          212.52
v  TurbVisc            8.6076e-11         0.78443        0.010932        0.059287
v  total_pressure     -7.3203e+05      1.1565e+06      8.4446e+05      8.1077e+05


 TIME FOR THE TIME STEP              769:        0.69066E+02

===============================================================


 INSTANT    0.770000000E+03   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.107854237E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160615E+01
Free inlet               13           0  
  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.246          54.661          3.4276         0.37534
v  Velocity[Y]            -45.335           42.38           1.162         0.86909
v  Velocity[Z]            -86.838          75.642         -1.7133      -0.0013467
v  ǁVelocityǁ           0.0021496          101.36          10.274           8.152
v  Pressure            -1.234e+06      6.5745e+05      3.4397e+05      3.1044e+05
v  k                    1.013e-05          81.964         0.27278         0.18834
v  epsilon               0.025949      1.2942e+07           18919           209.5
v  TurbVisc            8.5825e-11         0.76398        0.010799        0.058956
v  total_pressure     -7.3398e+05      1.1574e+06      8.4397e+05      8.1044e+05


 TIME FOR THE TIME STEP              767:        0.63570E+02

===============================================================


 INSTANT    0.768000000E+03   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         0.746476894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160611E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13011E+03 0.38954E+02
   Friction velocity        uet   :  0.32510E-01 0.73471E+01
   Friction velocity        uk    :  0.35076E-01 0.77600E+01
   Dimensionless distance   yplus :  0.51533E-03 0.52895E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18281
   Nb of faces within the viscous sub-layer     :       7196
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15552E+02     116   0.19468E+00   0.18593E+04 0.98854E+03 
c  Velocity[X]                                      0.60089E+03 
c  Velocity[Y]                                      0.57534E+03 
c  Velocity[Z]    -  -------  --------------  --------------  ------------  ------------
a  k           -0.00010837                             1
a  epsilon         -840.02                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.527          63.092           3.432         0.37514
v  Velocity[Y]            -44.765          42.232          1.1633         0.86861
v  Velocity[Z]            -116.32          93.268         -1.7118      -0.0013516
v  ǁVelocityǁ           0.0022099          133.23          10.277          8.1512
v  Pressure            -1.232e+06      6.5649e+05      3.4446e+05      3.1077e+05
v  k                   1.0149e-05          79.807         0.27479         0.19055
v  epsilon               0.026198      1.2929e+07           18930          212.52
v  TurbVisc            8.6076e-11         0.78443        0.010932        0.059287
v  total_pressure     -7.3203e+05      1.1565e+06      8.4446e+05      8.1077e+05


 TIME FOR THE TIME STEP              769:        0.72592E+02

===============================================================


 INSTANT    0.770000000E+03   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.107854237E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160615E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17308E+03 0.42509E+02
   Friction velocity        u
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00293                             2
a  epsilon         -948.89                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.792          52.706          3.4362         0.37485
v  Velocity[Y]            -43.492           41.83          1.1767         0.86864
v  Velocity[Z]            -98.043          84.666         -1.7146      -0.0014042
v  ǁVelocityǁ           0.0021729          112.19          10.294          8.1518
v  Pressure           -1.2358e+06      6.5609e+05      3.4538e+05      3.1134e+05
v  k                   1.0399e-05          88.004         0.27627         0.19242
v  epsilon               0.026842      1.2986e+07           18979          213.43
v  TurbVisc            8.6753e-11         0.76192        0.010992        0.059586
v  total_pressure     -7.3583e+05      1.1561e+06      8.4538e+05      8.1134e+05


 TIME FOR THE TIME STEP              771:        0.68392E+02

===============================================================


 INSTANT    0.772000000E+03   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        -0.537609525E-17
Rough wall                6           0        -  -------  --------------  --------------  ------------  ------------
a  k           -0.00010837                             1
a  epsilon         -840.02                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.527          63.092           3.432         0.37514
v  Velocity[Y]            -44.765          42.232          1.1633         0.86861
v  Velocity[Z]            -116.32          93.268         -1.7118      -0.0013516
v  ǁVelocityǁ           0.0022099          133.23          10.277          8.1512
v  Pressure            -1.232e+06      6.5649e+05      3.4446e+05      3.1077e+05
v  k                   1.0149e-05          79.807         0.27479         0.19055
v  epsilon               0.026198      1.2929e+07           18930          212.52
v  TurbVisc            8.6076e-11         0.78443        0.010932        0.059287
v  total_pressure     -7.3203e+05      1.1565e+06      8.4446e+05      8.1077e+05


 TIME FOR THE TIME STEP              769:        0.65172E+02

===============================================================


 INSTANT    0.770000000E+03   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.107854237E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160615E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17308E+03 0.42509E+02
   Friction velocity        uet   :  0.39290E-01 0.99658E+01
   Friction velocity        uk    :  0.45098E-01 0.77435E+01
   Dimensionless distance   yplus :  0.52214E-03 0.50389E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18265
   Nb of faces within the viscous sub-layer     :       7200
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15533E+02     116   0.19295E+00   0.18560E+04 0.99210E+03 
c  Ve
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00293                             2
a  epsilon         -948.89                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.792          52.706          3.4362         0.37485
v  Velocity[Y]            -43.492           41.83          1.1767         0.86864
v  Velocity[Z]            -98.043          84.666         -1.7146      -0.0014042
v  ǁVelocityǁ           0.0021729          112.19          10.294          8.1518
v  Pressure           -1.2358e+06      6.5609e+05      3.4538e+05      3.1134e+05
v  k                   1.0399e-05          88.004         0.27627         0.19242
v  epsilon               0.026842      1.2986e+07           18979          213.43
v  TurbVisc            8.6753e-11         0.76192        0.010992        0.059586
v  total_pressure     -7.3583e+05      1.1561e+06      8.4538e+05      8.1134e+05


 TIME FOR THE TIME STEP              771:        0.67515E+02

===============================================================


 INSTANT    0.772000000E+03   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        -0.537609525E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         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  epsilon      0.45889E+05      57   0.64117E-02   0.41944E+10 0.82947E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0031028                             3
a  epsilon         -858.26                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.538          54.712          3.4419          0.3748
v  Velocity[Y]            -44.406          42.365          1.1972         0.86849
v  Velocity[Z]             -88.41           74.32         -1.7202      -0.0010228
v  ǁVelocityǁ           0.0021266           102.8          10.313          8.1513
v  Pressure           -1.2306e+06      6.5842e+05      3.4656e+05      3.1206e+05
v  k                   1.0901e-05          81.184         0.27746         0.19351
v  epsilon               0.028227        1.29e+07           19009           212.2
v  TurbVisc            5.2262e-11         0.75292        0.011033        0.059846
v  total_pressure     -7.3055e+05      1.1584e+06      8.4656e+05      8.1206e+05


 TIME FOR THE TIME STEP              773:        0.69160E+02

===============================================================


 INSTANT    0.774000000E+03   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2     
  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00293                             2
a  epsilon         -948.89                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.792          52.706          3.4362         0.37485
v  Velocity[Y]            -43.492           41.83          1.1767         0.86864
v  Velocity[Z]            -98.043          84.666         -1.7146      -0.0014042
v  ǁVelocityǁ           0.0021729          112.19          10.294          8.1518
v  Pressure           -1.2358e+06      6.5609e+05      3.4538e+05      3.1134e+05
v  k                   1.0399e-05          88.004         0.27627         0.19242
v  epsilon               0.026842      1.2986e+07           18979          213.43
v  TurbVisc            8.6753e-11         0.76192        0.010992        0.059586
v  total_pressure     -7.3583e+05      1.1561e+06      8.4538e+05      8.1134e+05


 TIME FOR THE TIME STEP              771:        0.75472E+02

===============================================================


 INSTANT    0.772000000E+03   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        -0.537609525E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160617E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.16028E+03 0.41903E+02
   Friction velocity        uet   :  0.34802E-01 0.82586E+01
   Friction velocity        uk    :  0.50360E-01 0.77563E+01
   Dimensionless distance   yplus :  0.51786E-03 0.51294E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18239
   Nb of faces within the viscous sub-layer     :       7162
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residualc  epsilon      0.45889E+05      57   0.64117E-02   0.41944E+10 0.82947E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0031028                             3
a  epsilon         -858.26                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.538          54.712          3.4419          0.3748
v  Velocity[Y]            -44.406          42.365          1.1972         0.86849
v  Velocity[Z]             -88.41           74.32         -1.7202      -0.0010228
v  ǁVelocityǁ           0.0021266           102.8          10.313          8.1513
v  Pressure           -1.2306e+06      6.5842e+05      3.4656e+05      3.1206e+05
v  k                   1.0901e-05          81.184         0.27746         0.19351
v  epsilon               0.028227        1.29e+07           19009           212.2
v  TurbVisc            5.2262e-11         0.75292        0.011033        0.059846
v  total_pressure     -7.3055e+05      1.1584e+06      8.4656e+05      8.1206e+05


 TIME FOR THE TIME STEP              773:        0.71010E+02

===============================================================


 INSTANT    0.774000000E+03   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.143167170E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
 c  Pressure     0.22450E+00     988   0.57731E-02   0.34054E+00 0.61144E+03 
c  k            0.24418E+01      83   0.11134E-01   0.72916E+02 0.24825E+04 
c  epsilon      0.46907E+05      58   0.87558E-02   0.72022E+10 0.78729E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026882                             3
a  epsilon         -900.62                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.616          53.409          3.4473         0.37433
v  Velocity[Y]            -43.863          41.845          1.2228         0.86845
v  Velocity[Z]            -83.355          87.849         -1.7254      -0.0010885
v  ǁVelocityǁ           0.0021907          96.927          10.335          8.1509
v  Pressure           -1.2267e+06      6.6094e+05      3.4639e+05      3.1196e+05
v  k                   1.1705e-05          88.075         0.27897          0.1947
v  epsilon               0.030518      1.2888e+07           19037          213.14
v  TurbVisc              8.66e-11         0.74326        0.011091        0.060068
v  total_pressure     -7.2671e+05      1.1609e+06      8.4639e+05      8.1196e+05


 TIME FOR THE TIME STEP              775:        0.83894E+02

===============================================================


 INSTANT    0.776000000E+03   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

-----------------------------------------------------------c  epsilon      0.45889E+05      57   0.64117E-02   0.41944E+10 0.82947E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0031028                             3
a  epsilon         -858.26                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.538          54.712          3.4419          0.3748
v  Velocity[Y]            -44.406          42.365          1.1972         0.86849
v  Velocity[Z]             -88.41           74.32         -1.7202      -0.0010228
v  ǁVelocityǁ           0.0021266           102.8          10.313          8.1513
v  Pressure           -1.2306e+06      6.5842e+05      3.4656e+05      3.1206e+05
v  k                   1.0901e-05          81.184         0.27746         0.19351
v  epsilon               0.028227        1.29e+07           19009           212.2
v  TurbVisc            5.2262e-11         0.75292        0.011033        0.059846
v  total_pressure     -7.3055e+05      1.1584e+06      8.4656e+05      8.1206e+05


 TIME FOR THE TIME STEP              773:        0.68902E+02

===============================================================


 INSTANT    0.774000000E+03   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.143167170E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15120E+03 0.42887E+02
   Friction velocity        uet   :  0.10636E-01 0.74644E+01
   Friction velocity        uk    :  0.46318E-01 0.77502E+01
   Dimensionless distance   yplus :  0.51213E-03 0.50291E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18250
   Nb of faces within the viscous sub-layer     :       7155
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-c  Pressure     0.22450E+00     988   0.57731E-02   0.34054E+00 0.61144E+03 
c  k            0.24418E+01      83   0.11134E-01   0.72916E+02 0.24825E+04 
c  epsilon      0.46907E+05      58   0.87558E-02   0.72022E+10 0.78729E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026882                             3
a  epsilon         -900.62                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.616          53.409          3.4473         0.37433
v  Velocity[Y]            -43.863          41.845          1.2228         0.86845
v  Velocity[Z]            -83.355          87.849         -1.7254      -0.0010885
v  ǁVelocityǁ           0.0021907          96.927          10.335          8.1509
v  Pressure           -1.2267e+06      6.6094e+05      3.4639e+05      3.1196e+05
v  k                   1.1705e-05          88.075         0.27897          0.1947
v  epsilon               0.030518      1.2888e+07           19037          213.14
v  TurbVisc              8.66e-11         0.74326        0.011091        0.060068
v  total_pressure     -7.2671e+05      1.1609e+06      8.4639e+05      8.1196e+05


 TIME FOR THE TIME STEP              775:        0.81415E+02

===============================================================


 INSTANT    0.776000000E+03   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        -0.894658419E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160612E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0    c  Velocity[X]                                      0.59236E+03 
c  Velocity[Y]                                      0.60245E+03 
c  Velocity[Z]                                      0.69513E+03 
c  Pressure     0.23727E+00     840   0.64367E-02   0.35908E+00 0.69533E+03 
c  k            0.20359E+01      85   0.14547E-01   0.98275E+02 0.31362E+04 
c  epsilon      0.43133E+05      58   0.13508E-01   0.11361E+11 0.13250E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028222                             3
a  epsilon         -830.16                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.493          54.536          3.4512         0.37487
v  Velocity[Y]            -45.051          70.046          1.2438         0.86769
v  Velocity[Z]             -82.87          75.992         -1.7303      -0.0010586
v  ǁVelocityǁ            0.002109          96.496          10.351          8.1513
v  Pressure           -1.2288e+06      6.6246e+05      3.4651e+05       3.122e+05
v  k                   1.2713e-05          50.233         0.27923         0.19495
v  epsilon               0.033379      1.2886e+07           19073          207.74
v  TurbVisc            8.5099e-11         0.59165        0.011176        0.060293
v  total_pressure      -7.288e+05      1.1625e+06      8.4651e+05       8.122e+05


 TIME FOR THE TIME STEP              777:        0.64917E+02

===============================================================


 INSTANT    0.778000000E+03   TIME STEP NUMBER             778
 ===============================================c  Pressure     0.22450E+00     988   0.57731E-02   0.34054E+00 0.61144E+03 
c  k            0.24418E+01      83   0.11134E-01   0.72916E+02 0.24825E+04 
c  epsilon      0.46907E+05      58   0.87558E-02   0.72022E+10 0.78729E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0026882                             3
a  epsilon         -900.62                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.616          53.409          3.4473         0.37433
v  Velocity[Y]            -43.863          41.845          1.2228         0.86845
v  Velocity[Z]            -83.355          87.849         -1.7254      -0.0010885
v  ǁVelocityǁ           0.0021907          96.927          10.335          8.1509
v  Pressure           -1.2267e+06      6.6094e+05      3.4639e+05      3.1196e+05
v  k                   1.1705e-05          88.075         0.27897          0.1947
v  epsilon               0.030518      1.2888e+07           19037          213.14
v  TurbVisc              8.66e-11         0.74326        0.011091        0.060068
v  total_pressure     -7.2671e+05      1.1609e+06      8.4639e+05      8.1196e+05


 TIME FOR THE TIME STEP              775:        0.87414E+02

===============================================================


 INSTANT    0.776000000E+03   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        -0.894658419E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160612E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19791E+03 0.40643E+02
   Friction velocity        uet   :  0.41616E-01 0.71285E+01
   Friction velocity        uk    :  0.73608E-01 0.77569E+01
   Dimensionless distance   yplus :  0.52080E-03 0.48819E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18229
   Nb of faces within the viscous sub-layer     :       71c  Velocity[X]                                      0.59236E+03 
c  Velocity[Y]                                      0.60245E+03 
c  Velocity[Z]                                      0.69513E+03 
c  Pressure     0.23727E+00     840   0.64367E-02   0.35908E+00 0.69533E+03 
c  k            0.20359E+01      85   0.14547E-01   0.98275E+02 0.31362E+04 
c  epsilon      0.43133E+05      58   0.13508E-01   0.11361E+11 0.13250E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028222                             3
a  epsilon         -830.16                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.493          54.536          3.4512         0.37487
v  Velocity[Y]            -45.051          70.046          1.2438         0.86769
v  Velocity[Z]             -82.87          75.992         -1.7303      -0.0010586
v  ǁVelocityǁ            0.002109          96.496          10.351          8.1513
v  Pressure           -1.2288e+06      6.6246e+05      3.4651e+05       3.122e+05
v  k                   1.2713e-05          50.233         0.27923         0.19495
v  epsilon               0.033379      1.2886e+07           19073          207.74
v  TurbVisc            8.5099e-11         0.59165        0.011176        0.060293
v  total_pressure      -7.288e+05      1.1625e+06      8.4651e+05       8.122e+05


 TIME FOR THE TIME STEP              777:        0.77876E+02

===============================================================


 INSTANT    0.778000000E+03   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        -0.742959126E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160612E+01
Free inlet      -----------------------------------------------------------------------------
c  Velocity     0.15504E+02     121   0.19216E+00   0.20348E+04 0.10213E+04 
c  Velocity[X]                                      0.61746E+03 
c  Velocity[Y]                                      0.65148E+03 
c  Velocity[Z]                                      0.76584E+03 
c  Pressure     0.24782E+00     728   0.71403E-02   0.37627E+00 0.70815E+03 
c  k            0.17246E+01      86   0.12274E-01   0.51887E+02 0.25930E+04 
c  epsilon      0.40061E+05      61   0.99429E-02   0.76315E+10 0.84562E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028047                             3
a  epsilon         -785.61                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.611          61.364          3.4522         0.37445
v  Velocity[Y]            -43.234          62.112          1.2592         0.86835
v  Velocity[Z]            -95.335          99.646         -1.7358     -0.00089454
v  ǁVelocityǁ           0.0020908          110.05          10.362          8.1518
v  Pressure           -1.2294e+06      6.6284e+05      3.4633e+05      3.1213e+05
v  k                   1.3696e-05          54.316           0.279          0.1951
v  epsilon               0.036182      1.2955e+07           19122           202.6
v  TurbVisc            8.4819e-11          0.5237        0.011224        0.060524
v  total_pressure     -7.2935e+05      1.1628e+06      8.4633e+05      8.1213e+05


 TIME FOR THE TIME STEP              779:   c  Velocity[X]                                      0.59236E+03 
c  Velocity[Y]                                      0.60245E+03 
c  Velocity[Z]                                      0.69513E+03 
c  Pressure     0.23727E+00     840   0.64367E-02   0.35908E+00 0.69533E+03 
c  k            0.20359E+01      85   0.14547E-01   0.98275E+02 0.31362E+04 
c  epsilon      0.43133E+05      58   0.13508E-01   0.11361E+11 0.13250E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028222                             3
a  epsilon         -830.16                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.493          54.536          3.4512         0.37487
v  Velocity[Y]            -45.051          70.046          1.2438         0.86769
v  Velocity[Z]             -82.87          75.992         -1.7303      -0.0010586
v  ǁVelocityǁ            0.002109          96.496          10.351          8.1513
v  Pressure           -1.2288e+06      6.6246e+05      3.4651e+05       3.122e+05
v  k                   1.2713e-05          50.233         0.27923         0.19495
v  epsilon               0.033379      1.2886e+07           19073          207.74
v  TurbVisc            8.5099e-11         0.59165        0.011176        0.060293
v  total_pressure      -7.288e+05      1.1625e+06      8.4651e+05       8.122e+05


 TIME FOR THE TIME STEP              777:        0.86376E+02

===============================================================


 INSTANT    0.778000000E+03   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        -0.742959126E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160612E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19272E+03 0.35542E+02
   Friction velocity        uet   :  0.42577E-01 0.78159E+01
   Friction velocity        uk    :  0.48516E-01 0.77748E+01
   Dimensionless distance   yplus :  0.51008E-03 0.41407E+02
   ------------------------------------------------------------------------------------------------
c  Velocity     0.15504E+02     121   0.19216E+00   0.20348E+04 0.10213E+04 
c  Velocity[X]                                      0.61746E+03 
c  Velocity[Y]                                      0.65148E+03 
c  Velocity[Z]                                      0.76584E+03 
c  Pressure     0.24782E+00     728   0.71403E-02   0.37627E+00 0.70815E+03 
c  k            0.17246E+01      86   0.12274E-01   0.51887E+02 0.25930E+04 
c  epsilon      0.40061E+05      61   0.99429E-02   0.76315E+10 0.84562E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028047                             3
a  epsilon         -785.61                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.611          61.364          3.4522         0.37445
v  Velocity[Y]            -43.234          62.112          1.2592         0.86835
v  Velocity[Z]            -95.335          99.646         -1.7358     -0.00089454
v  ǁVelocityǁ           0.0020908          110.05          10.362          8.1518
v  Pressure           -1.2294e+06      6.6284e+05      3.4633e+05      3.1213e+05
v  k                   1.3696e-05          54.316           0.279          0.1951
v  epsilon               0.036182      1.2955e+07           19122           202.6
v  TurbVisc            8.4819e-11          0.5237        0.011224        0.060524
v  total_pressure     -7.2935e+05      1.1628e+06      8.4633e+05      8.1213e+05


 TIME FOR THE TIME STEP              779:        0.72786E+02

===============================================================


 INSTANT    0.780000000E+03   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.111748087E-16
Rough wall                6           0         0.00-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     120   0.19240E+00   0.23763E+04 0.10735E+04 
c  Velocity[X]                                      0.62459E+03 
c  Velocity[Y]                                      0.78506E+03 
c  Velocity[Z]                                      0.96662E+03 
c  Pressure     0.28692E+00     771   0.67751E-02   0.43255E+00 0.19455E+04 
c  k            0.17120E+01      86   0.71969E-02   0.23892E+02 0.20947E+04 
c  epsilon      0.40092E+05      60   0.63469E-02   0.47557E+11 0.10370E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028342                             2
a  epsilon         -571.81                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.756          53.853          3.4522         0.37215
v  Velocity[Y]            -45.748          69.727          1.2644         0.86879
v  Velocity[Z]            -92.612          70.146         -1.7401       -0.001319
v  ǁVelocityǁ           0.0020978          108.06           10.37          8.1524
v  Pressure           -1.2325e+06      6.6187e+05      3.4532e+05      3.1155e+05
v  k                   1.4478e-05          62.222           0.277         0.19524
v  epsilon               0.038458      1.2909e+07           19152          199.97
v  TurbVisc            8.4416e-11         0.55325      -----------------------------------------------------------------------------
c  Velocity     0.15504E+02     121   0.19216E+00   0.20348E+04 0.10213E+04 
c  Velocity[X]                                      0.61746E+03 
c  Velocity[Y]                                      0.65148E+03 
c  Velocity[Z]                                      0.76584E+03 
c  Pressure     0.24782E+00     728   0.71403E-02   0.37627E+00 0.70815E+03 
c  k            0.17246E+01      86   0.12274E-01   0.51887E+02 0.25930E+04 
c  epsilon      0.40061E+05      61   0.99429E-02   0.76315E+10 0.84562E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028047                             3
a  epsilon         -785.61                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.611          61.364          3.4522         0.37445
v  Velocity[Y]            -43.234          62.112          1.2592         0.86835
v  Velocity[Z]            -95.335          99.646         -1.7358     -0.00089454
v  ǁVelocityǁ           0.0020908          110.05          10.362          8.1518
v  Pressure           -1.2294e+06      6.6284e+05      3.4633e+05      3.1213e+05
v  k                   1.3696e-05          54.316           0.279          0.1951
v  epsilon               0.036182      1.2955e+07           19122           202.6
v  TurbVisc            8.4819e-11          0.5237        0.011224        0.060524
v  total_pressure     -7.2935e+05      1.1628e+06      8.4633e+05      8.1213e+05


 TIME FOR THE TIME STEP              779:        0.65553E+02

===============================================================


 INSTANT    0.780000000E+03   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.111748087E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.24186E+03 0.36888E+02
   Friction velocity        uet   :  0.44790E-01 0.80586E+01
   Friction velocity        uk    :  0.52129E-01 0.77743E+01
   Dimensionless distance   yplus :  0.50792E-03 0.40262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18224
   Nb of faces within the viscous sub-layer     :       7124
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     121   0.19521E+00   0.21679E+04 0.10212E+04 
c  Velocity[X]                                      0.59836E+03 
c  Velocity[Y]                                      0.67217E+03 
c  Velocity[Z]                                      0.89738E+03 
c  Pressure     0.29714E+00     611   0.69999E-02   0.45220E+00 0.60915E+03 
c  k            0.17057E+01      87   0.98943E-02   0.33659E+02 0.22194E+04 
c  epsilon      0.40134E+05      61   0.79489E-02   0.13512E+11 0.94524E+05 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010113                             1
a  epsilon         -743.48                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -30.242          56.323          3.4523         0.37362
v  Velocity[Y]            -44.745          96.779           1.264         0.86834
v  Velocity[Z]            -104.99          74.128         -1.7386      -0.0014827
v  ǁVelocityǁ           0.0020746          136.85          10.368          8.1536
v  Pressure           -1.2291e+06      6.6311e+05      3.4638e+05      3.1223e+05
v  k                   1.4118e-05          57.794          0.2782         0.19522
v  epsilon               0.037405      1.2847e+07           19109          201.18
v  TurbVisc            8.5271e-11         0.54858        0.011226        0.060653
v  total_pressure     -7.2908e+05      1.1631e+06      8.4638e+05      8.1223e+05


 TIME    Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15541E+02     121   0.19753E+00   0.19420E+04 0.99468E+03 
c  Velocity[X]                                      0.66014E+03 
c  Velocity[Y]                                      0.58842E+03 
c  Velocity[Z]                                      0.69344E+03 
c  Pressure     0.29958E+00     621   0.70102E-02   0.45729E+00 0.91580E+03 
c  k            0.18356E+01      86   0.81338E-02   0.24559E+02 0.18892E+04 
c  epsilon      0.40896E+05      59   0.61814E-02   0.13676E+11 0.19562E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027942                             2
a  epsilon         -711.83                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.919          62.965          3.4455         0.37111
v  Velocity[Y]            -44.859          42.714          1.2576          0.8679
v  Velocity[Z]            -97.666          92.144         -1.7383     -0.00082479
v  ǁVelocityǁ           0.0021065          112.93          10.368          8.1509
v  Pressure            -1.235e+06      6.6222e+05       3.455e+05      3.1172e+05
v  k                   1.5006e-05          71.895         0.273-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15520E+02     120   0.19240E+00   0.23763E+04 0.10735E+04 
c  Velocity[X]                                      0.62459E+03 
c  Velocity[Y]                                      0.78506E+03 
c  Velocity[Z]                                      0.96662E+03 
c  Pressure     0.28692E+00     771   0.67751E-02   0.43255E+00 0.19455E+04 
c  k            0.17120E+01      86   0.71969E-02   0.23892E+02 0.20947E+04 
c  epsilon      0.40092E+05      60   0.63469E-02   0.47557E+11 0.10370E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028342                             2
a  epsilon         -571.81                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.756          53.853          3.4522         0.37215
v  Velocity[Y]            -45.748          69.727          1.2644         0.86879
v  Velocity[Z]            -92.612          70.146         -1.7401       -0.001319
v  ǁVelocityǁ           0.0020978          108.06           10.37          8.1524
v  Pressure           -1.2325e+06      6.6187e+05      3.4532e+05      3.1155e+05
v  k                   1.4478e-05          62.222           0.277         0.19524
v  epsilon               0.038458      1.2909e+07           19152          199.97
v  TurbVisc            8.4416e-11         0.55325        0.011194        0.060797
v  total_pressure     -7.3247e+05      1.1619e+06      8.4532e+05      8.1155e+05


 TIME FOR THE TIME STEP              781:        0.78709E+02

===============================================================


 INSTANT    0.782000000E+03   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        -0.190691805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160619E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                            Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15541E+02     121   0.19753E+00   0.19420E+04 0.99468E+03 
c  Velocity[X]                                      0.66014E+03 
c  Velocity[Y]                                      0.58842E+03 
c  Velocity[Z]                                      0.69344E+03 
c  Pressure     0.29958E+00     621   0.70102E-02   0.45729E+00 0.91580E+03 
c  k            0.18356E+01      86   0.81338E-02   0.24559E+02 0.18892E+04 
c  epsilon      0.40896E+05      59   0.61814E-02   0.13676E+11 0.19562E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027942                             2
a  epsilon         -711.83                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.919          62.965          3.4455         0.37111
v  Velocity[Y]            -44.859          42.714          1.2576          0.8679
v  Velocity[Z]            -97.666          92.144         -1.7383     -0.00082479
v  ǁVelocityǁ           0.0021065          112.93          10.368          8.1509
v  Pressure            -1.235e+06      6.6222e+05       3.455e+05      3.1172e+05
v  k                   1.5006e-05          71.895         0.27331         0.19509
v  epsilon                0.04006      1.2871e+07           19112          198.26
v  TurbVisc            8.4434e-11         0.59275        0.011044        0.061088
v  total_pressure       -7.35e+05      1.1622e+06       8.455e+05      8.1172e+05


 TIME FOR THE TIME STEP              783:        0.67325E+02

===============================================================


 INSTANT    0.784000000E+03   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      -----------------------------   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18239
   Nb of faces within the viscous sub-layer     :       7078
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15559E+02     122   0.19269E+00   0.20143E+04 0.10009E+04 
c  Velocity[X]                                      0.62513E+03 
c  Velocity[Y]                                      0.58518E+03 
c  Velocity[Z]                                      0.80397E+03 
c  Pressure     0.26938E+00     861   0.66159E-02   0.41057E+00 0.60895E+03 
c  k            0.18876E+01      86   0.73667E-02   0.19254E+02 0.16598E+04 
c  epsilon      0.41677E+05      57   0.51719E-02   0.34356E+10 0.10304E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025737                             2
a  epsilon         -808.09                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.917          53.438          3.4302          0.3697
v  Velocity[Y]            -44.474          42.866          1.2471          0.8679
v  Velocity[Z]            -82.529          77.019         -1.7344      -0.0013063
v  ǁVelocityǁ           0.0020994      Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15541E+02     121   0.19753E+00   0.19420E+04 0.99468E+03 
c  Velocity[X]                                      0.66014E+03 
c  Velocity[Y]                                      0.58842E+03 
c  Velocity[Z]                                      0.69344E+03 
c  Pressure     0.29958E+00     621   0.70102E-02   0.45729E+00 0.91580E+03 
c  k            0.18356E+01      86   0.81338E-02   0.24559E+02 0.18892E+04 
c  epsilon      0.40896E+05      59   0.61814E-02   0.13676E+11 0.19562E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0027942                             2
a  epsilon         -711.83                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.919          62.965          3.4455         0.37111
v  Velocity[Y]            -44.859          42.714          1.2576          0.8679
v  Velocity[Z]            -97.666          92.144         -1.7383     -0.00082479
v  ǁVelocityǁ           0.0021065          112.93          10.368          8.1509
v  Pressure            -1.235e+06      6.6222e+05       3.455e+05      3.1172e+05
v  k                   1.5006e-05          71.895         0.27331         0.19509
v  epsilon                0.04006      1.2871e+07           19112          198.26
v  TurbVisc            8.4434e-11         0.59275        0.011044        0.061088
v  total_pressure       -7.35e+05      1.1622e+06       8.455e+05      8.1172e+05


 TIME FOR THE TIME STEP              783:        0.59998E+02

===============================================================


 INSTANT    0.784000000E+03   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.203274305E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BO   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18239
   Nb of faces within the viscous sub-layer     :       7078
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15559E+02     122   0.19269E+00   0.20143E+04 0.10009E+04 
c  Velocity[X]                                      0.62513E+03 
c  Velocity[Y]                                      0.58518E+03 
c  Velocity[Z]                                      0.80397E+03 
c  Pressure     0.26938E+00     861   0.66159E-02   0.41057E+00 0.60895E+03 
c  k            0.18876E+01      86   0.73667E-02   0.19254E+02 0.16598E+04 
c  epsilon      0.41677E+05      57   0.51719E-02   0.34356E+10 0.10304E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025737                             2
a  epsilon         -808.09                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.917          53.438          3.4302          0.3697
v  Velocity[Y]            -44.474          42.866          1.2471          0.8679
v  Velocity[Z]            -82.529          77.019         -1.7344      -0.0013063
v  ǁVelocityǁ           0.0020994           99.09          10.359          8.1471
v  Pressure           -1.2363e+06      6.6191e+05      3.4528e+05       3.114e+05
v  k                   1.5364e-05          75.176         0.26914         0.19471
v  epsilon               0.041238       1.285e+07           19097          196.79
v  TurbVisc            8.3459e-11         0.64115        0.010811        0.061332
v  total_pressure     -7.3634e+05      1.1619e+06      8.4528e+05       8.114e+05


 TIME FOR THE TIME STEP              785:        0.79192E+02

===============================================================


 INSTANT    0.786000   Friction velocity        uet   :  0.34127E-01 0.80148E+01
   Friction velocity        uk    :  0.42645E-01 0.77364E+01
   Dimensionless distance   yplus :  0.50948E-03 0.43321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18260
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     121   0.18984E+00   0.23008E+04 0.10303E+04 
c  Velocity[X]                                      0.64989E+03 
c  Velocity[Y]                                      0.65144E+03 
c  Velocity[Z]                                      0.99949E+03 
c  Pressure     0.27710E+00     692   0.69395E-02   0.41962E+00 0.11525E+04 
c  k            0.19453E+01      85   0.94115E-02   0.39338E+02 0.18289E+04 
c  epsilon      0.41591E+05      57   0.63581E-02   0.46305E+10 0.20365E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025947                             3
a  epsilon          -820.7                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.555          62.076          3.4091         0.36898
v  Velocity[Y]           ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18239
   Nb of faces within the viscous sub-layer     :       7078
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15559E+02     122   0.19269E+00   0.20143E+04 0.10009E+04 
c  Velocity[X]                                      0.62513E+03 
c  Velocity[Y]                                      0.58518E+03 
c  Velocity[Z]                                      0.80397E+03 
c  Pressure     0.26938E+00     861   0.66159E-02   0.41057E+00 0.60895E+03 
c  k            0.18876E+01      86   0.73667E-02   0.19254E+02 0.16598E+04 
c  epsilon      0.41677E+05      57   0.51719E-02   0.34356E+10 0.10304E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025737                             2
a  epsilon         -808.09                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.917          53.438          3.4302          0.3697
v  Velocity[Y]            -44.474          42.866          1.2471          0.8679
v  Velocity[Z]            -82.529          77.019         -1.7344      -0.0013063
v  ǁVelocityǁ           0.0020994           99.09          10.359          8.1471
v  Pressure           -1.2363e+06      6.6191e+05      3.4528e+05       3.114e+05
v  k                   1.5364e-05          75.176         0.26914         0.19471
v  epsilon               0.041238       1.285e+07           19097          196.79
v  TurbVisc            8.3459e-11         0.64115        0.010811        0.061332
v  total_pressure     -7.3634e+05      1.1619e+06      8.4528e+05       8.114e+05


 TIME FOR THE TIME STEP              785:        0.72716E+02

===============================================================


 INSTANT    0.786000000E+03   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000        -0.185181547E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160615E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface          Friction velocity        uet   :  0.34127E-01 0.80148E+01
   Friction velocity        uk    :  0.42645E-01 0.77364E+01
   Dimensionless distance   yplus :  0.50948E-03 0.43321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18260
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     121   0.18984E+00   0.23008E+04 0.10303E+04 
c  Velocity[X]                                      0.64989E+03 
c  Velocity[Y]                                      0.65144E+03 
c  Velocity[Z]                                      0.99949E+03 
c  Pressure     0.27710E+00     692   0.69395E-02   0.41962E+00 0.11525E+04 
c  k            0.19453E+01      85   0.94115E-02   0.39338E+02 0.18289E+04 
c  epsilon      0.41591E+05      57   0.63581E-02   0.46305E+10 0.20365E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025947                             3
a  epsilon          -820.7                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.555          62.076          3.4091         0.36898
v  Velocity[Y]            -41.404          55.194          1.2411          0.8677
v  Velocity[Z]            -94.678          72.218         -1.7249     -0.00097001
v  ǁVelocityǁ           0.0020951          109.33          10.347          8.1452
v  Pressure           -1.2313e+06      6.6532e+05      3.4595e+05      3.1168e+05
v  k                   1.5753e-05          75.782         0.26553         0.19486
v  epsilon               0.042606      1.2901e+07           19013          197.31
v  TurbVisc            8.3696e-11         0.65011        0.010569        0.061558
v  total_pressure      -7.313e+05      1.1653e+06                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14451E+03 0.43694E+02
   Friction velocity        uet   :  0.26252E-01 0.73202E+01
   Friction velocity        uk    :  0.55899E-01 0.77334E+01
   Dimensionless distance   yplus :  0.50743E-03 0.44286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18277
   Nb of faces within the viscous sub-layer     :       7044
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15605E+02     122   0.19747E+00   0.20636E+04 0.10107E+04 
c  Velocity[X]                                      0.63606E+03 
c  Velocity[Y]                                      0.60686E+03 
c  Velocity[Z]                                      0.82067E+03 
c  Pressure     0.29633E+00     891   0.91626E-02   0.44848E+00 0.23335E+04 
c  k            0.22663E+01      83   0.11136E-01   0.93805E+02 0.23416E+04 
c  epsilon      0.43502E+05      57   0.91410E-02   0.85465E+10 0.11619E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024653                             3
a  epsilon         -832.01                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-     Friction velocity        uet   :  0.34127E-01 0.80148E+01
   Friction velocity        uk    :  0.42645E-01 0.77364E+01
   Dimensionless distance   yplus :  0.50948E-03 0.43321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18260
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     121   0.18984E+00   0.23008E+04 0.10303E+04 
c  Velocity[X]                                      0.64989E+03 
c  Velocity[Y]                                      0.65144E+03 
c  Velocity[Z]                                      0.99949E+03 
c  Pressure     0.27710E+00     692   0.69395E-02   0.41962E+00 0.11525E+04 
c  k            0.19453E+01      85   0.94115E-02   0.39338E+02 0.18289E+04 
c  epsilon      0.41591E+05      57   0.63581E-02   0.46305E+10 0.20365E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025947                             3
a  epsilon          -820.7                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.555          62.076          3.4091         0.36898
v  Velocity[Y]            -41.404          55.194          1.2411          0.8677
v  Velocity[Z]            -94.678          72.218         -1.7249     -0.00097001
v  ǁVelocityǁ           0.0020951          109.33          10.347          8.1452
v  Pressure           -1.2313e+06      6.6532e+05      3.4595e+05      3.1168e+05
v  k                   1.5753e-05          75.782         0.26553         0.19486
v  epsilon               0.042606      1.2901e+07           19013          197.31
v  TurbVisc            8.3696e-11         0.65011        0.010569        0.061558
v  total_pressure      -7.313e+05      1.1653e+06      8.4595e+05      8.1168e+05


 TIME FOR THE TIME STEP              787:        0.66604E+02

===============================================================


 INSTANT    0.788000000E+03   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        -0.175211518E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3                                          Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14451E+03 0.43694E+02
   Friction velocity        uet   :  0.26252E-01 0.73202E+01
   Friction velocity        uk    :  0.55899E-01 0.77334E+01
   Dimensionless distance   yplus :  0.50743E-03 0.44286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18277
   Nb of faces within the viscous sub-layer     :       7044
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15605E+02     122   0.19747E+00   0.20636E+04 0.10107E+04 
c  Velocity[X]                                      0.63606E+03 
c  Velocity[Y]                                      0.60686E+03 
c  Velocity[Z]                                      0.82067E+03 
c  Pressure     0.29633E+00     891   0.91626E-02   0.44848E+00 0.23335E+04 
c  k            0.22663E+01      83   0.11136E-01   0.93805E+02 0.23416E+04 
c  epsilon      0.43502E+05      57   0.91410E-02   0.85465E+10 0.11619E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024653                             3
a  epsilon         -832.01                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.924          54.423          3.3825         0.36865
v  Velocity[Y]            -43.814          48.551          1.2364           0.867
v  Velocity[Z]            -86.278          73.077         -1.7129     -0.00091444
v  ǁVelocityǁ           0.0021191          101.38           10.33          8.1432
v  Pressure             -1.23e+06      6.6043e+05      3.4459e+05      3.1068e+05
v  k                   1.6405e-05          75.422         0.26387         0.19677
v  epsilon               0.044787      1.2811e+07           18899    ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20995E+03 0.35081E+02
   Friction velocity        uet   :  0.45467E-01 0.78501E+01
   Friction velocity        uk    :  0.56863E-01 0.77205E+01
   Dimensionless distance   yplus :  0.51105E-03 0.48459E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18281
   Nb of faces within the viscous sub-layer     :       7071
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15590E+02     123   0.18997E+00   0.22150E+04 0.10353E+04 
c  Velocity[X]                                      0.63598E+03 
c  Velocity[Y]                                      0.63210E+03 
c  Velocity[Z]                                      0.94695E+03 
c  Pressure     0.26676E+00     819   0.78972E-02   0.41028E+00 0.12554E+04 
c  k            0.24166E+01      82   0.10973E-01   0.91070E+02 0.23391E+04 
c  epsilon      0.44226E+05      58   0.94009E-02   0.10813E+11 0.18741E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00243                             3
a  epsilon         -96                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14451E+03 0.43694E+02
   Friction velocity        uet   :  0.26252E-01 0.73202E+01
   Friction velocity        uk    :  0.55899E-01 0.77334E+01
   Dimensionless distance   yplus :  0.50743E-03 0.44286E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18277
   Nb of faces within the viscous sub-layer     :       7044
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15605E+02     122   0.19747E+00   0.20636E+04 0.10107E+04 
c  Velocity[X]                                      0.63606E+03 
c  Velocity[Y]                                      0.60686E+03 
c  Velocity[Z]                                      0.82067E+03 
c  Pressure     0.29633E+00     891   0.91626E-02   0.44848E+00 0.23335E+04 
c  k            0.22663E+01      83   0.11136E-01   0.93805E+02 0.23416E+04 
c  epsilon      0.43502E+05      57   0.91410E-02   0.85465E+10 0.11619E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0024653                             3
a  epsilon         -832.01                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.924          54.423          3.3825         0.36865
v  Velocity[Y]            -43.814          48.551          1.2364           0.867
v  Velocity[Z]            -86.278          73.077         -1.7129     -0.00091444
v  ǁVelocityǁ           0.0021191          101.38           10.33          8.1432
v  Pressure             -1.23e+06      6.6043e+05      3.4459e+05      3.1068e+05
v  k                   1.6405e-05          75.422         0.26387         0.19677
v  epsilon               0.044787      1.2811e+07           18899             205
v  TurbVisc            2.2637e-11         0.73275        0.010365        0.061803
v  total_pressure     -7.2997e+05      1.1604e+06      8.4459e+05      8.1068e+05


 TIME FOR THE TIME STEP              789:        0.82145E+02

===============================================================


 INSTANT    0.790000000E+03   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.895322338E-17
Rough wal   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20995E+03 0.35081E+02
   Friction velocity        uet   :  0.45467E-01 0.78501E+01
   Friction velocity        uk    :  0.56863E-01 0.77205E+01
   Dimensionless distance   yplus :  0.51105E-03 0.48459E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18281
   Nb of faces within the viscous sub-layer     :       7071
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15590E+02     123   0.18997E+00   0.22150E+04 0.10353E+04 
c  Velocity[X]                                      0.63598E+03 
c  Velocity[Y]                                      0.63210E+03 
c  Velocity[Z]                                      0.94695E+03 
c  Pressure     0.26676E+00     819   0.78972E-02   0.41028E+00 0.12554E+04 
c  k            0.24166E+01      82   0.10973E-01   0.91070E+02 0.23391E+04 
c  epsilon      0.44226E+05      58   0.94009E-02   0.10813E+11 0.18741E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00243                             3
a  epsilon         -965.49                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.472          63.072          3.3557         0.36796
v  Velocity[Y]            -52.513          51.671          1.2308         0.86598
v  Velocity[Z]            -100.41          73.148          -1.707      -0.0021944
v  ǁVelocityǁ           0.0021272          115.62          10.316            8.14
v  Pressure           -1.2253e+06   Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12015E+03 0.56744E+02
   Friction velocity        uet   :  0.38458E-01 0.83463E+01
   Friction velocity        uk    :  0.43520E-01 0.77113E+01
   Dimensionless distance   yplus :  0.50878E-03 0.45676E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18258
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15584E+02     124   0.19389E+00   0.22746E+04 0.10323E+04 
c  Velocity[X]                                      0.66619E+03 
c  Velocity[Y]                                      0.64460E+03 
c  Velocity[Z]                                      0.96379E+03 
c  Pressure     0.25527E+00     715   0.88713E-02   0.39557E+00 0.18950E+04 
c  k            0.22613E+01      83   0.94559E-02   0.41988E+02 0.18146E+04 
c  epsilon      0.43189E+05      57   0.82071E-02   0.51342E+10 0.11676E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-     ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.20995E+03 0.35081E+02
   Friction velocity        uet   :  0.45467E-01 0.78501E+01
   Friction velocity        uk    :  0.56863E-01 0.77205E+01
   Dimensionless distance   yplus :  0.51105E-03 0.48459E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18281
   Nb of faces within the viscous sub-layer     :       7071
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15590E+02     123   0.18997E+00   0.22150E+04 0.10353E+04 
c  Velocity[X]                                      0.63598E+03 
c  Velocity[Y]                                      0.63210E+03 
c  Velocity[Z]                                      0.94695E+03 
c  Pressure     0.26676E+00     819   0.78972E-02   0.41028E+00 0.12554E+04 
c  k            0.24166E+01      82   0.10973E-01   0.91070E+02 0.23391E+04 
c  epsilon      0.44226E+05      58   0.94009E-02   0.10813E+11 0.18741E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.00243                             3
a  epsilon         -965.49                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.472          63.072          3.3557         0.36796
v  Velocity[Y]            -52.513          51.671          1.2308         0.86598
v  Velocity[Z]            -100.41          73.148          -1.707      -0.0021944
v  ǁVelocityǁ           0.0021272          115.62          10.316            8.14
v  Pressure           -1.2253e+06      6.6152e+05      3.4436e+05      3.1046e+05
v  k                   1.7399e-05          80.645         0.26331         0.19851
v  epsilon               0.047953      1.2841e+07           18839          211.92
v  TurbVisc            8.3844e-11         0.94575        0.010246        0.062069
v  total_pressure      -7.253e+05      1.1615e+06      8.4436e+05      8.1046e+05


 TIME FOR THE TIME STEP              791:        0.73285E+02

===============================================================


 INSTANT    0.792000000E+03   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
-------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12015E+03 0.56744E+02
   Friction velocity        uet   :  0.38458E-01 0.83463E+01
   Friction velocity        uk    :  0.43520E-01 0.77113E+01
   Dimensionless distance   yplus :  0.50878E-03 0.45676E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18258
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15584E+02     124   0.19389E+00   0.22746E+04 0.10323E+04 
c  Velocity[X]                                      0.66619E+03 
c  Velocity[Y]                                      0.64460E+03 
c  Velocity[Z]                                      0.96379E+03 
c  Pressure     0.25527E+00     715   0.88713E-02   0.39557E+00 0.18950E+04 
c  k            0.22613E+01      83   0.94559E-02   0.41988E+02 0.18146E+04 
c  epsilon      0.43189E+05      57   0.82071E-02   0.51342E+10 0.11676E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021254                             3
a  epsilon         -925.28                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.184          55.679          3.3383         0.36792
v  Velocity[Y]            -62.869          88.703          1.2244         0.86598
v  VelocitFree outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39340E+03 0.23675E+02
   Friction velocity        uet   :  0.38321E-01 0.10642E+02
   Friction velocity        uk    :  0.57301E-01 0.77266E+01
   Dimensionless distance   yplus :  0.52103E-03 0.43531E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18241
   Nb of faces within the viscous sub-layer     :       7043
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     123   0.19210E+00   0.25890E+04 0.10832E+04 
c  Velocity[X]                                      0.68131E+03 
c  Velocity[Y]                                      0.71331E+03 
c  Velocity[Z]                                      0.11944E+04 
c  Pressure     0.28104E+00     790   0.93592E-02   0.44026E+00 0.48669E+03 
c  k            0.20772E+01      84   0.64654E-02   0.17326E+02 0.12691E+04 
c  epsilon      0.41089E+05      57   0.67220E-02   0.57227E+10 0.20954E+06 
------------------------------------Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12015E+03 0.56744E+02
   Friction velocity        uet   :  0.38458E-01 0.83463E+01
   Friction velocity        uk    :  0.43520E-01 0.77113E+01
   Dimensionless distance   yplus :  0.50878E-03 0.45676E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18258
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15584E+02     124   0.19389E+00   0.22746E+04 0.10323E+04 
c  Velocity[X]                                      0.66619E+03 
c  Velocity[Y]                                      0.64460E+03 
c  Velocity[Z]                                      0.96379E+03 
c  Pressure     0.25527E+00     715   0.88713E-02   0.39557E+00 0.18950E+04 
c  k            0.22613E+01      83   0.94559E-02   0.41988E+02 0.18146E+04 
c  epsilon      0.43189E+05      57   0.82071E-02   0.51342E+10 0.11676E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0021254                             3
a  epsilon         -925.28                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -21.184          55.679          3.3383         0.36792
v  Velocity[Y]            -62.869          88.703          1.2244         0.86598
v  Velocity[Z]            -85.979          86.628         -1.7089      -0.0023916
v  ǁVelocityǁ           0.0021642          108.78          10.311           8.137
v  Pressure           -1.2253e+06       6.636e+05      3.4481e+05      3.1085e+05
v  k                   1.8615e-05          81.354         0.26245         0.19786
v  epsilon               0.051745      1.2833e+07           18769          209.15
v  TurbVisc             8.477e-11         0.92915        0.010189        0.062244
v  total_pressure     -7.2528e+05      1.1636e+06      8.4481e+05      8.1085e+05


 TIME FOR THE TIME STEP              793:        0.68305E+02

===============================================================


 INSTANT    0.794000000E+03   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARYFree outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39340E+03 0.23675E+02
   Friction velocity        uet   :  0.38321E-01 0.10642E+02
   Friction velocity        uk    :  0.57301E-01 0.77266E+01
   Dimensionless distance   yplus :  0.52103E-03 0.43531E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18241
   Nb of faces within the viscous sub-layer     :       7043
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     123   0.19210E+00   0.25890E+04 0.10832E+04 
c  Velocity[X]                                      0.68131E+03 
c  Velocity[Y]                                      0.71331E+03 
c  Velocity[Z]                                      0.11944E+04 
c  Pressure     0.28104E+00     790   0.93592E-02   0.44026E+00 0.48669E+03 
c  k            0.20772E+01      84   0.64654E-02   0.17326E+02 0.12691E+04 
c  epsilon      0.41089E+05      57   0.67220E-02   0.57227E+10 0.20954E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011647                             1
a  epsilon         -954.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  -------------Smooth wall               5       41000        -0.137637383E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23773E+03 0.53283E+02
   Friction velocity        uet   :  0.29578E-01 0.91065E+01
   Friction velocity        uk    :  0.71242E-01 0.77100E+01
   Dimensionless distance   yplus :  0.52302E-03 0.41543E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18257
   Nb of faces within the viscous sub-layer     :       7047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     124   0.18985E+00   0.24938E+04 0.10916E+04 
c  Velocity[X]                                      0.64753E+03 
c  Velocity[Y]                                      0.69439E+03 
c  Velocity[Z]                                      0.11519E+04 
c  Pressure     0.27941E+00     789   0.98221E-02   0.43524E+00 0.13270E+04Free outlet               3          46         0.328160622E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39340E+03 0.23675E+02
   Friction velocity        uet   :  0.38321E-01 0.10642E+02
   Friction velocity        uk    :  0.57301E-01 0.77266E+01
   Dimensionless distance   yplus :  0.52103E-03 0.43531E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18241
   Nb of faces within the viscous sub-layer     :       7043
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     123   0.19210E+00   0.25890E+04 0.10832E+04 
c  Velocity[X]                                      0.68131E+03 
c  Velocity[Y]                                      0.71331E+03 
c  Velocity[Z]                                      0.11944E+04 
c  Pressure     0.28104E+00     790   0.93592E-02   0.44026E+00 0.48669E+03 
c  k            0.20772E+01      84   0.64654E-02   0.17326E+02 0.12691E+04 
c  epsilon      0.41089E+05      57   0.67220E-02   0.57227E+10 0.20954E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011647                             1
a  epsilon         -954.32                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.591          64.467          3.3362         0.36843
v  Velocity[Y]            -51.358          72.049          1.2198         0.86625
v  Velocity[Z]            -127.78          87.311         -1.7199      -0.0024159
v  ǁVelocityǁ           0.0022159          143.97          10.319          8.1377
v  Pressure           -1.2207e+06      6.6158e+05      3.4508e+05      3.1107e+05
v  k                   1.9847e-05          76.909         0.26161         0.19606
v  epsilon               0.055581      1.2818e+07           18715          202.53
v  TurbVisc            8.6758e-11         0.79651        0.010154         0.06231
v  total_pressure     -7.2072e+05      1.1616e+06      8.4508e+05      8.1107e+05


 TIME FOR THE TIME STEP              795:        0.75246E+02

===================Smooth wall               5       41000        -0.137637383E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23773E+03 0.53283E+02
   Friction velocity        uet   :  0.29578E-01 0.91065E+01
   Friction velocity        uk    :  0.71242E-01 0.77100E+01
   Dimensionless distance   yplus :  0.52302E-03 0.41543E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18257
   Nb of faces within the viscous sub-layer     :       7047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     124   0.18985E+00   0.24938E+04 0.10916E+04 
c  Velocity[X]                                      0.64753E+03 
c  Velocity[Y]                                      0.69439E+03 
c  Velocity[Z]                                      0.11519E+04 
c  Pressure     0.27941E+00     789   0.98221E-02   0.43524E+00 0.13270E+04 
c  k            0.19470E+01      83   0.46157E-02   0.10040E+02 0.12722E+04 
c  epsilon      0.40297E+05      56   0.46031E-02   0.28220E+10 0.11388E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012349                             1
a  epsilon         -933.54                             1


  ** Computed fieldBoundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.109773752E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160613E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14419E+03 0.27587E+02
   Friction velocity        uet   :  0.38999E-01 0.93133E+01
   Friction velocity        uk    :  0.55860E-01 0.77275E+01
   Dimensionless distance   yplus :  0.52302E-03 0.42032E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18277
   Nb of faces within the viscous sub-layer     :       7056
   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.                     
@                     Smooth wall               5       41000        -0.137637383E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160618E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.23773E+03 0.53283E+02
   Friction velocity        uet   :  0.29578E-01 0.91065E+01
   Friction velocity        uk    :  0.71242E-01 0.77100E+01
   Dimensionless distance   yplus :  0.52302E-03 0.41543E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18257
   Nb of faces within the viscous sub-layer     :       7047
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     124   0.18985E+00   0.24938E+04 0.10916E+04 
c  Velocity[X]                                      0.64753E+03 
c  Velocity[Y]                                      0.69439E+03 
c  Velocity[Z]                                      0.11519E+04 
c  Pressure     0.27941E+00     789   0.98221E-02   0.43524E+00 0.13270E+04 
c  k            0.19470E+01      83   0.46157E-02   0.10040E+02 0.12722E+04 
c  epsilon      0.40297E+05      56   0.46031E-02   0.28220E+10 0.11388E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012349                             1
a  epsilon         -933.54                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.414          55.064          3.3456         0.36876
v  Velocity[Y]            -45.531          50.883          1.2157         0.86528
v  Velocity[Z]            -90.837          76.499         -1.7284      -0.0027319
v  ǁVelocityǁ            0.002202          106.86          10.333          8.1422
v  Pressure           -1.2195e+06      6.5762e+05       3.431e+05      3.0978e+05
v  k                   2.0897e-05          69.906         0.26172         0.19482
v  epsilon               0.058876      1.2791e+07           18712          198.49
v  TurbVisc            8.6972e-11         0.67915        0.010148        0.062286
v  total_pressure     -7.1954e+05      1.1576e+06       8.431e+05      8.0978e+05


 TIME FOR THE TIME STEP              797:        0.69247E+02

===============================================================


 INSTANT    0.798000000E+03   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        -0.140883616E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160650E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13402E+03 0.31266E+02
   Friction velocity        uet   :  0.24256E-01 0.77161E+01
   Friction velocity        uk    :  0.63090E-01 0.77692E+01
   Dimensionless distance   yplus :  0.52129E-03 0.41566E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18268
   Nb of faces within the viscous sub-layer     :       7051
   Total number of wall faces                   :      41000
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15581E+02     122   0.19235E+00   0.23311E+04 0.10710E+04 
c  Velocity[X]                                      0.68826E+03 
c  Velocity[Y]                                      0.62868E+03 
c  Velocity[Z]                                      0.10142E+04 
c  Pressure     0.29459E+00     754   0.10574E-01   0.46429E+00 0.11414E+04 
c  k            0.19774E+01      83   0.44024E-02   0.13614E+02 0.13412E+04 
c  epsilon      0.40273E+05      56   0.40092E-02   0.21671E+11 0.15916E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0017661                             2
a  epsilon         -880.27                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.471           64.67          3.3548         0.36908
v  Velocity[Y]            -44.008          41.997          1.2153         0.86459
v  Velocity[Z]            -88.165          119.17         -1.7305      -0.0014424
v  ǁVelocityǁ           0.0022149          135.95          10.343          8.1429
v  Pressure           -1.2191e+06      6.5771e+05       3.423e+05      3.0933e+05
v  k                   2.1323e-05          73.207         0.26252         0.19471
v  epsilon               0.021664      1.2766e+07           18779          198.22
v  TurbVisc            8.7715e-11         0.67822        0.010173        0.062288
v  total_pressure      -7.191e+05      1.1577e+06       8.423e+05      8.0933e+05


 TIME FOR THE TIME STEP              798:        0.62712E+02

===============================================================


 INSTANT    0.799000000E+03   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2          46        -0.328160635E+01
Smooth wall               5       41000         0.109773752E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160613E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14419E+03 0.27587E+02
   Friction velocity        uet   :  0.38999E-01 0.93133E+01
   Friction velocity        uk    :  0.55860E-01 0.77275E+01
   Dimensionless distance   yplus :  0.52302E-03 0.42032E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18277
   Nb of faces within the viscous sub-layer     :       7056
   Total number of wall faces                   :      41000
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step        799
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15562E+02     120   0.18900E+00   0.22350E+04 0.10617E+04 
c  Velocity[X]                                      0.64641E+03 
c  Velocity[Y]                                      0.63445E+03 
c  Velocity[Z]                                      0.95414E+03 
c  Pressure     0.28860E+00     694   0.82266E-02   0.45311E+00 0.12758E+04 
c  k            0.19610E+01      82   0.51268E-02   0.10470E+02 0.10287E+04 
c  epsilon      0.40261E+05      56   0.72027E-02   0.17579E+11 0.15102E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0029919                             2
a  epsilon         -917.51                             2


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.347          62.879          3.3636         0.36902
v  Velocity[Y]            -45.426          65.581          1.2152         0.86455
v  Velocity[Z]            -92.507          72.424         -1.7342      -0.0023386
v  ǁVelocityǁ           0.0021614          109.86          10.351          8.1423
v  Pressure           -1.2191e+06      6.5692e+05      3.4172e+05      3.0881e+05
v  k                   2.1197e-05          71.383         0.26344         0.19468
v  epsilon               0.061308      1.2828e+07           18772          198.31
v  TurbVisc            8.7734e-11         0.70839        0.010213        0.062287
v  total_pressure     -7.1913e+05      1.1569e+06      8.4172e+05      8.0881e+05


 TIME FOR THE TIME STEP              799:        0.32970E+02

===============================================================


 INSTANT    0.800000000E+03   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        -0.105613342E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3          46         0.328160650E+01
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.18818E+03 0.27006E+02
   Friction velocity        uet   :  0.42266E-01 0.78761E+01
   Friction velocity        uk    :  0.65184E-01 0.77497E+01
   Dimensionless distance   yplus :  0.51640E-03 0.42764E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18315
   Nb of faces within the viscous sub-layer     :       7049
   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+03


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.11735E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15546E+02     121   0.18646E+00   0.20195E+04 0.10153E+04 
c  Velocity[X]                                      0.60808E+03 
c  Velocity[Y]                                      0.63677E+03 
c  Velocity[Z]                                      0.77469E+03 
c  Pressure     0.30156E+00     658   0.83006E-02   0.47594E+00 0.16077E+04 
c  k            0.19956E+01      82   0.56333E-02   0.12514E+02 0.11308E+04 
c  epsilon      0.40651E+05      57   0.74837E-02   0.14979E+11 0.10930E+06 
-----------------------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0020828                             2
a  epsilon         -884.53                             1


  ** Computed fields on cells
     ------------------------

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -20.427          60.567          3.3742         0.37027
v  Velocity[Y]            -44.478           54.27          1.2171         0.86429
v  Velocity[Z]            -117.48          86.827         -1.7373       -0.002059
v  ǁVelocityǁ           0.0022236          132.49          10.362          8.1421
v  Pressure           -1.2159e+06      6.5651e+05      3.4202e+05      3.0909e+05
v  k                    2.196e-05           74.68         0.26462         0.19475
v  epsilon              0.0042217      1.2757e+07           18836          198.88
v  TurbVisc            8.7709e-11         0.69303        0.010266        0.062285
v  total_pressure     -7.1595e+05      1.1565e+06      8.4202e+05      8.0909e+05


 TIME FOR THE TIME STEP              800:        0.28921E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.13823E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

e+06      8.4202e+05      8.0909e+05


 TIME FOR THE TIME STEP              800:        0.30046E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.17088E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation

e+06      8.4202e+05      8.0909e+05


 TIME FOR THE TIME STEP              800:        0.59836E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.12013E-03
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          57837.289 s
  System CPU time:           31.808 s

  Elapsed time:           57898.018 s
  CPU / elapsed time          1.000

Memory use summary:

  Total memory used:                             696.441 MiB
  Theoretical instrumented dynamic memory:       346.483 MiB

Calculation time summary:

  User CPU time:          57839.789 s
  System CPU time:           31.336 s

  Elapsed time:           57904.834 s
  CPU / elapsed time          0.999

Memory use summary:

  Total memory used:                             696.441 MiB
  Theoretical instrumented dynamic memory:       346.483 MiB

Calculation time summary:

  User CPU time:          57884.984 s
  System CPU time:           31.456 s

  Elapsed time:           57947.318 s
  CPU / elapsed time          0.999

Memory use summary:

  Total memory used:                             696.441 MiB
  Theoretical instrumented dynamic memory:       346.483 MiB

Calculation time summary:

  User CPU time:          57886.520 s
  System CPU time:           30.856 s

  Elapsed time:           57951.454 s
  CPU / elapsed time          0.999

Memory use summary:

  Total memory used:                             696.441 MiB
  Theoretical instrumented dynamic memory:       346.483 MiB
