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

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

                                  (R)
                      Code_Saturne

                      Version 4.0.0


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

  revision 4.0.0
  build Thu 28 May 2015 10:25:02 PM MSK
  MPI version 2.1 (Open MPI 1.4.3)


  The Code_Saturne CFD tool  is free software;
  you can redistribute it and/or modify it under the terms
  of the GNU General Public License as published by the
  Free Software Foundation; either version 2 of the License,
  or (at your option) any later version.

  The Code_Saturne CFD tool is distributed in the hope that
  it will be useful, but WITHOUT ANY WARRANTY; without even
  the implied warranty of MERCHANTABILITY or FITNESS FOR A
  PARTICULAR PURPOSE.  See the GNU General Public License
  for more details.

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


Local case configuration:

  Date:                Tue 16 Jun 2015 09:14:44 PM MSK
  System:              Linux 3.11.0-26-generic
  Machine:             AntechPC
  Processor:           model name	: Intel(R) Core(TM) i7-2600K CPU @ 3.40GHz
  Memory:              15964 MB
  User:                antech (Antech)
  Directory:           /home/antech/CodeSaturne/CASE3/RESU/20150616-2114
  MPI ranks:           4 (appnum attribute: 0)
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

 Reading metadata from file: "mesh_input"

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

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


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




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


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

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

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


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

 --- Physics
       NVAR   =              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     =   -0.98060E+01 (Gravity y component         )
       GZ     =    0.00000E+00 (Gravity z component         )

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18300E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+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  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       ICLKEP =              0 (k-epsilon clipping model    )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (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 =    0.50000E+00 (Reference relaxation coeff. )


 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per variable relaxation coefficient

-----------------------------
 Variable          RELAXV
-----------------------------
 Velocity          0.5000E+00
 Pressure          0.5000E+00
 k                 0.5000E+00
 epsilon           0.5000E+00
----------------------------

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


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


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

---------------------------------------------------------------------
 Variable          ICONV  IDIFF IDIFFT ISCHCV ISSTPC   BLENCV  THETAV
---------------------------------------------------------------------
 Velocity              1      1      1      1      0 0.00E+00 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 =              0 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-03  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-03  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-03  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-03  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              0     -1  0.1500E+01
 Pressure              1     -1  0.1500E+01
 k                     0     -1  0.1500E+01
 epsilon               0     -1  0.1500E+01
-----------------------------------

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


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


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


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


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

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

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


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


 ** CALCULATION MANAGEMENT
    ----------------------

 --- Restarted calculation
       ISUITE =              1 (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 =          10000 (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  =              0 (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 =              1 (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: EnSight Gold
      options: binary
      time dependency: fixed mesh
      output: at calculation end


 Reading file:        mesh_input
 Finished reading:    mesh_input

 Reading file:        partition_input/domain_number_4
 Finished reading:    partition_input/domain_number_4


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

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

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

 Histogram of the number of cells per rank:

    minimum value =            1389251
    maximum value =            1389251

      1 : [    1389251 ;    1389251 ] =          4

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

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

    minimum value =            1410442
    maximum value =            1427452

      1 : [    1410442 ;    1413844 [ =          1
      2 : [    1413844 ;    1417246 [ =          1
      3 : [    1417246 ;    1420648 [ =          0
      4 : [    1420648 ;    1424050 [ =          1
      5 : [    1424050 ;    1427452 ] =          1

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

 Histogram of the number of ghost cells per rank:

    minimum value =              21191
    maximum value =              38201

      1 : [      21191 ;      24593 [ =          1
      2 : [      24593 ;      27995 [ =          1
      3 : [      27995 ;      31397 [ =          0
      4 : [      31397 ;      34799 [ =          1
      5 : [      34799 ;      38201 ] =          1

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

 Histogram of the number of interior faces per rank:

    minimum value =            2769917
    maximum value =            2785373

      1 : [    2769917 ;    2773008 [ =          2
      2 : [    2773008 ;    2776099 [ =          0
      3 : [    2776099 ;    2779190 [ =          0
      4 : [    2779190 ;    2782281 [ =          0
      5 : [    2782281 ;    2785373 ] =          2

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

 Histogram of the number of boundary faces per rank:

    minimum value =              35619
    maximum value =              49640

      1 : [      35619 ;      38423 [ =          2
      2 : [      38423 ;      41227 [ =          0
      3 : [      41227 ;      44031 [ =          0
      4 : [      44031 ;      46835 [ =          1
      5 : [      46835 ;      49640 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  1
    maximum value =                  4

      1 : [          1 ;          2 [ =         31
      2 : [          2 ;          3 [ =       2734
      3 : [          3 ;          4 ] =    5554239

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  3
    maximum value =                  3

      1 : [          3 ;          3 ] =          4

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

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

 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.42109e-14

      1 : [ 0.00000e+00 ; 1.42109e-15 [ =     166611
      2 : [ 1.42109e-15 ; 2.84217e-15 [ =          0
      3 : [ 2.84217e-15 ; 4.26326e-15 [ =          0
      4 : [ 4.26326e-15 ; 5.68434e-15 [ =          0
      5 : [ 5.68434e-15 ; 7.10543e-15 [ =          0
      6 : [ 7.10543e-15 ; 8.52651e-15 [ =          0
      7 : [ 8.52651e-15 ; 9.94760e-15 [ =          0
      8 : [ 9.94760e-15 ; 1.13687e-14 [ =          0
      9 : [ 1.13687e-14 ; 1.27898e-14 [ =          0
     10 : [ 1.27898e-14 ; 1.42109e-14 ] =        213

  Histogram of the interior faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.42109e-14

      1 : [ 0.00000e+00 ; 1.77636e-15 [ =   11001984
      2 : [ 1.77636e-15 ; 3.55271e-15 [ =          0
      3 : [ 3.55271e-15 ; 5.32907e-15 [ =          0
      4 : [ 5.32907e-15 ; 7.10543e-15 [ =          0
      5 : [ 7.10543e-15 ; 8.88178e-15 [ =          0
      6 : [ 8.88178e-15 ; 1.06581e-14 [ =          0
      7 : [ 1.06581e-14 ; 1.24345e-14 [ =          0
      8 : [ 1.24345e-14 ; 1.42109e-14 ] =      28612

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.42109e-14

      1 : [ 0.00000e+00 ; 1.42109e-15 [ =     166638
      2 : [ 1.42109e-15 ; 2.84217e-15 [ =          0
      3 : [ 2.84217e-15 ; 4.26326e-15 [ =          0
      4 : [ 4.26326e-15 ; 5.68434e-15 [ =          0
      5 : [ 5.68434e-15 ; 7.10543e-15 [ =          0
      6 : [ 7.10543e-15 ; 8.52651e-15 [ =          0
      7 : [ 8.52651e-15 ; 9.94760e-15 [ =          0
      8 : [ 9.94760e-15 ; 1.13687e-14 [ =          0
      9 : [ 1.13687e-14 ; 1.27898e-14 [ =          0
     10 : [ 1.27898e-14 ; 1.42109e-14 ] =        186

  Histogram of the interior faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.42109e-14

      1 : [ 0.00000e+00 ; 1.77636e-15 [ =   11017589
      2 : [ 1.77636e-15 ; 3.55271e-15 [ =          0
      3 : [ 3.55271e-15 ; 5.32907e-15 [ =          0
      4 : [ 5.32907e-15 ; 7.10543e-15 [ =          0
      5 : [ 7.10543e-15 ; 8.88178e-15 [ =          0
      6 : [ 8.88178e-15 ; 1.06581e-14 [ =          0
      7 : [ 1.06581e-14 ; 1.24345e-14 [ =          0
      8 : [ 1.24345e-14 ; 1.42109e-14 ] =      13007

 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

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

 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =            1408882
    maximum value =            1425516

      1 : [    1408882 ;    1412208 [ =          1
      2 : [    1412208 ;    1415535 [ =          1
      3 : [    1415535 ;    1418862 [ =          0
      4 : [    1418862 ;    1422189 [ =          0
      5 : [    1422189 ;    1425516 ] =          2

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =             758903
    maximum value =             761037

      1 : [     758903 ;     759329 [ =          2
      2 : [     759329 ;     759756 [ =          0
      3 : [     759756 ;     760183 [ =          0
      4 : [     760183 ;     760610 [ =          1
      5 : [     760610 ;     761037 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -4.5729100e+00  4.5729100e+00
                       Y : -2.6013671e-16  3.0600000e+01
                       Z : -4.2380892e+00  4.2380892e+00
 Mesh
     Number of cells:          5557004
     Number of interior faces: 11030596
     Number of boundary faces: 166824
     Number of vertices:       989861

 Groups:
    "Group_Of_All_Faces"
       boundary faces:       166824
    "Group_Of_All_Volumes"
       cells:               5557004
    "Inlet"
       boundary faces:        15836
    "Outlet"
       boundary faces:         9303

 --- Information on the volumes
       Minimum control volume      =  7.2694928e-07
       Maximum control volume      =  3.0163680e-03
       Total volume for the domain =  1.5646180e+03

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

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 15 -->   0 %

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

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

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

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

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

 Computing geometric quantities (3.75 s)
                                                             
       ALMAX  =    0.11581E+02 (Characteristic length       )
       ALMAX is the cubic root of the domain volume.

       ALMAX is the length used to initialize the turbulence.

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

   ** READING MAIN AND AUXILIARY RESTART FILES
      ----------------------------------------


      READING THE MAIN RESTART FILE

 Start reading
 Reading dimensions complete
  Reading the previous time step number (restarting computation)  NTPABS =          125
  Reading the previous time step number (restarting computation)  TTPABS =   0.1250E+01
 Reading options complete
  Read variables from restart: restart/main
 Reading complete

         READING THE AUXILIARY RESTART FILE             

 Start reading                                          
   Fin de la lecture des options                        

   Apdatation of the reference point for the total pressure  
       by reading the restart file                           
    XYZP0 =    0.80870E+00   0.20650E+02  -0.91539E-02

   Fin de la lecture des proprietes physiques           
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: WHEN READING THE AUXILIARY RESTART FILE        
@    =======                                                 
@      THE RUN RESTARTED            WITH IDTVAR =         -1
@      FROM RUN CONDUCTED WITH            IDTVAR =          0
@                                                            
@    The variable time step method has been modified.        
@    The (uniform) value of the time step is                 
@      DTREF =   0.1000E+01
@                                                            
@    It is advised however in this case to                   
@      verify the value of IDTVAR.                           
@                                                            
@    Verify that the auxiliary restart file being used       
@      corresponds  to the present case.                     
@                                                            
@    The run will continue...                                
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

   Fin de la lecture du pas de temps                    
   Fin de la lecture des flux de masse                  
   Fin de la lecture des conditions aux limites         
  restart/auxiliary: section "time_moments:sizes" not present.
  restart/auxiliary: section "nombre_moyennes_temps" not present.
 End reading                                            

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


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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity         -0.2319E+02  0.2245E+02
  Velocity         -0.1043E+02  0.1177E+02
  Velocity         -0.1701E+02  0.1745E+02
  Pressure         -0.1235E+03  0.7002E+02
  k                 0.1858E-04  0.4539E+02
  epsilon           0.7502E-07  0.2774E+05
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.225000000E+01   TIME STEP NUMBER             126
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.1568E-08  0.2042E+01
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2       15836
Smooth wall               5      141685
Rough wall                6           0
Symmetry                  4           0
Free outlet               3        9303
Free inlet               13           0
Convective inlet         15           0
Free surface             14           0
Undefined                 1           0
-------------------------------------------------------------------------



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.217136991E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083857E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30365E+01 0.12536E+02
   Friction velocity        uet   :  0.41469E-04 0.67850E+00
   Friction velocity        uk    :  0.46870E-02 0.36085E+01
   Dimensionless distance   yplus :  0.35083E+01 0.33054E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         81
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        672 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10838E+04       6   0.67560E-03   0.35608E+01 0.18096E+02 
c  Velocity[X]                                      0.16364E+01 
c  Velocity[Y]                                      0.74599E+00 
c  Velocity[Z]                                      0.11783E+01 
c  Pressure     0.11106E+01     228   0.11958E-01   0.53364E+00 0.34572E+03 
c  k            0.41693E+03       4   0.36637E-03   0.23037E+00 0.81884E+01 
c  epsilon      0.53522E+04       4   0.10534E-01   0.63594E+03 0.40747E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -22.098          21.859        0.050948        0.087474
v  Velocity[Y]            -10.132          11.532          1.0435           1.314
v  Velocity[Z]            -16.556          16.519      -0.0069184      -8.908e-05
v  ǁVelocityǁ           0.0053134          23.438          4.0737          2.5692
v  Pressure               -281.58          68.679         -5.3218          3.2096
v  k                   6.9774e-05          53.771          1.3539         0.57792
v  epsilon             1.2316e-07           35825           46.53          4.2115
v  TurbVisc            1.5677e-09          2.0422        0.058812        0.091557
v  total_pressure      1.0115e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              126:        0.15394E+03

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


 INSTANT    0.325000000E+01   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.563196237E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152088424E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.14784E+01 0.12501E+02
   Friction velocity        uet   :  0.24487E-03 0.69227E+00
   Friction velocity        uk    :  0.43158E-02 0.40164E+01
   Dimensionless distance   yplus :  0.47919E+01 0.33288E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         72
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        627 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10805E+04       5   0.32987E-03   0.19529E+01 0.11693E+02 
c  Velocity[X]                                      0.83973E+00 
c  Velocity[Y]                                      0.48767E+00 
c  Velocity[Z]                                      0.62549E+00 
c  Pressure     0.64760E+00     188   0.51075E-02   0.31966E+00 0.76570E+02 
c  k            0.41876E+03       5   0.49404E-03   0.25583E+00 0.95051E+01 
c  epsilon      0.51995E+04       5   0.22371E-01   0.20466E+04 0.66615E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -21.663          21.202        0.051024        0.087746
v  Velocity[Y]             -10.17          10.668          1.0431          1.3143
v  Velocity[Z]            -16.285          15.977      -0.0068772      -0.0001415
v  ǁVelocityǁ           0.0063401          23.047          4.0744           2.571
v  Pressure               -239.24           68.49           -4.83          3.5603
v  k                   5.2379e-05          44.164          1.3565         0.58305
v  epsilon             1.2319e-07           31593          46.341           4.221
v  TurbVisc            1.4197e-08         0.39487        0.058667        0.091237
v  total_pressure      1.0119e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              127:        0.14243E+03

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


 INSTANT    0.425000000E+01   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.903075258E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078625E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.66463E+00 0.12387E+02
   Friction velocity        uet   :  0.46302E-03 0.68600E+00
   Friction velocity        uk    :  0.38176E-02 0.36399E+01
   Dimensionless distance   yplus :  0.48351E+01 0.33368E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         53
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        620 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10775E+04       6   0.18836E-03   0.15508E+01 0.96479E+01 
c  Velocity[X]                                      0.63629E+00 
c  Velocity[Y]                                      0.42903E+00 
c  Velocity[Z]                                      0.48552E+00 
c  Pressure     0.46040E+00     210   0.40306E-02   0.22893E+00 0.61229E+02 
c  k            0.42090E+03       5   0.49897E-03   0.24830E+00 0.93830E+01 
c  epsilon      0.50752E+04       5   0.25561E-01   0.23398E+04 0.70269E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]              -21.4          20.936        0.051095        0.088028
v  Velocity[Y]            -10.095          10.027          1.0428          1.3147
v  Velocity[Z]            -16.059          15.826      -0.0068444      -0.0001879
v  ǁVelocityǁ           0.0040915          22.661          4.0754           2.573
v  Pressure                -215.1          68.738         -4.0196          4.1554
v  k                   3.8138e-05           32.28          1.3584         0.58799
v  epsilon             1.2321e-07           21693           46.08          4.2269
v  TurbVisc            1.2284e-07         0.39487        0.058447        0.090798
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              128:        0.14989E+03

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


 INSTANT    0.525000000E+01   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.219869568E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078091E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61593E+00 0.12271E+02
   Friction velocity        uet   :  0.66158E-03 0.68135E+00
   Friction velocity        uk    :  0.31855E-02 0.30001E+01
   Dimensionless distance   yplus :  0.49440E+01 0.33396E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         44
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        617 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10747E+04       4   0.13436E-03   0.13836E+01 0.87850E+01 
c  Velocity[X]                                      0.55431E+00 
c  Velocity[Y]                                      0.40097E+00 
c  Velocity[Z]                                      0.42836E+00 
c  Pressure     0.37284E+00     193   0.34527E-02   0.18681E+00 0.45341E+02 
c  k            0.42293E+03       4   0.44840E-03   0.23622E+00 0.91343E+01 
c  epsilon      0.49798E+04       4   0.21966E-01   0.17899E+04 0.63805E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -21.175          20.745        0.051164        0.088307
v  Velocity[Y]            -9.9964          9.9661          1.0425           1.315
v  Velocity[Z]            -15.825          15.744      -0.0068127     -0.00023028
v  ǁVelocityǁ           0.0045329          22.297          4.0766           2.575
v  Pressure               -214.01          68.751          -3.399          4.6227
v  k                   2.3788e-05          33.681            1.36         0.59277
v  epsilon             1.2324e-07           13385          45.798          4.2304
v  TurbVisc            1.7629e-06         0.39487        0.058199        0.090317
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              129:        0.14342E+03

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


 INSTANT    0.625000000E+01   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.213361124E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078294E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42135E+00 0.12158E+02
   Friction velocity        uet   :  0.45035E-03 0.67755E+00
   Friction velocity        uk    :  0.26023E-02 0.26695E+01
   Dimensionless distance   yplus :  0.51660E+01 0.33381E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         34
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        608 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10721E+04       4   0.11324E-03   0.12850E+01 0.83022E+01 
c  Velocity[X]                                      0.50796E+00 
c  Velocity[Y]                                      0.38155E+00 
c  Velocity[Z]                                      0.39554E+00 
c  Pressure     0.30157E+00     191   0.30249E-02   0.15230E+00 0.37921E+02 
c  k            0.42486E+03       4   0.39089E-03   0.22595E+00 0.89398E+01 
c  epsilon      0.49089E+04       4   0.16177E-01   0.11714E+04 0.54991E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.953          20.544        0.051234        0.088581
v  Velocity[Y]            -9.9083          9.9773          1.0422          1.3152
v  Velocity[Z]            -15.636          15.682      -0.0067815     -0.00027046
v  ǁVelocityǁ            0.005875           21.97          4.0777          2.5771
v  Pressure               -214.74          68.659         -2.8644          5.0342
v  k                   1.5843e-05          37.283          1.3613         0.59741
v  epsilon             1.2326e-07           12202          45.513          4.2321
v  TurbVisc            5.8333e-06         0.39487        0.057952        0.089843
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              130:        0.14360E+03

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


 INSTANT    0.725000000E+01   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.132954253E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078901E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.22849E+00 0.12053E+02
   Friction velocity        uet   :  0.38206E-03 0.67432E+00
   Friction velocity        uk    :  0.23141E-02 0.24005E+01
   Dimensionless distance   yplus :  0.43287E+01 0.33335E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         20
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        599 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10696E+04       4   0.10390E-03   0.12140E+01 0.79729E+01 
c  Velocity[X]                                      0.47568E+00 
c  Velocity[Y]                                      0.36590E+00 
c  Velocity[Z]                                      0.37242E+00 
c  Pressure     0.26406E+00     190   0.27876E-02   0.13442E+00 0.33312E+02 
c  k            0.42670E+03       4   0.34807E-03   0.21852E+00 0.88233E+01 
c  epsilon      0.48529E+04       4   0.11207E-01   0.77138E+03 0.47943E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]             -20.74          20.356        0.051308        0.088849
v  Velocity[Y]            -9.8373          9.9838          1.0419          1.3155
v  Velocity[Z]            -15.495          15.615      -0.0067506     -0.00030753
v  ǁVelocityǁ           0.0047745          21.686          4.0789          2.5793
v  Pressure               -215.46          68.517          -2.385          5.4098
v  k                   1.1782e-05          40.993          1.3623          0.6019
v  epsilon             1.2329e-07           13507          45.232          4.2323
v  TurbVisc            4.3513e-06         0.39488        0.057689        0.089341
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              131:        0.14219E+03

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


 INSTANT    0.825000000E+01   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.109999855E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079251E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.17984E+00 0.11956E+02
   Friction velocity        uet   :  0.16850E-03 0.67162E+00
   Friction velocity        uk    :  0.22097E-02 0.23627E+01
   Dimensionless distance   yplus :  0.31531E+01 0.33267E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         17
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        582 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10672E+04       4   0.98385E-04   0.11571E+01 0.77206E+01 
c  Velocity[X]                                      0.45055E+00 
c  Velocity[Y]                                      0.35232E+00 
c  Velocity[Z]                                      0.35426E+00 
c  Pressure     0.23154E+00     173   0.25852E-02   0.11876E+00 0.30230E+02 
c  k            0.42848E+03       4   0.32078E-03   0.21309E+00 0.87580E+01 
c  epsilon      0.48052E+04       4   0.77057E-02   0.54301E+03 0.43040E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.577          20.352        0.051387        0.089113
v  Velocity[Y]            -9.7811          9.9861          1.0416          1.3157
v  Velocity[Z]            -15.426           15.56      -0.0067205     -0.00034182
v  ǁVelocityǁ           0.0061555          21.445          4.0801          2.5814
v  Pressure               -215.94          68.442         -1.9395          5.7638
v  k                   1.0338e-05          44.267          1.3631         0.60625
v  epsilon             1.2331e-07           14738          44.955           4.231
v  TurbVisc            3.7697e-06         0.39488        0.057417        0.088824
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              132:        0.13748E+03

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


 INSTANT    0.925000000E+01   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.127394856E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079049E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15671E+00 0.11868E+02
   Friction velocity        uet   :  0.48098E-03 0.66944E+00
   Friction velocity        uk    :  0.21994E-02 0.23978E+01
   Dimensionless distance   yplus :  0.36842E+01 0.33183E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         14
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        562 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10649E+04       4   0.94324E-04   0.11091E+01 0.75138E+01 
c  Velocity[X]                                      0.42979E+00 
c  Velocity[Y]                                      0.34015E+00 
c  Velocity[Z]                                      0.33914E+00 
c  Pressure     0.21234E+00     173   0.24450E-02   0.10970E+00 0.27738E+02 
c  k            0.43020E+03       4   0.30395E-03   0.20886E+00 0.87201E+01 
c  epsilon      0.47617E+04       4   0.54518E-02   0.41364E+03 0.39708E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.449           20.37        0.051474        0.089374
v  Velocity[Y]            -9.7367          9.9958          1.0414          1.3159
v  Velocity[Z]            -15.421          15.521      -0.0066931     -0.00037332
v  ǁVelocityǁ           0.0062032          21.243          4.0813          2.5836
v  Pressure               -215.92          68.344         -1.5214          6.1005
v  k                   1.1243e-05          46.644          1.3637         0.61048
v  epsilon             1.2334e-07           15716          44.681          4.2284
v  TurbVisc            4.0412e-06         0.39488        0.057143          0.0883
v  total_pressure      1.0122e+05      1.0157e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              133:        0.13763E+03

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


 INSTANT    0.102500000E+02   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.971013970E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079056E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12530E+00 0.11847E+02
   Friction velocity        uet   :  0.42004E-03 0.66772E+00
   Friction velocity        uk    :  0.22416E-02 0.24186E+01
   Dimensionless distance   yplus :  0.37431E+01 0.33092E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         12
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        538 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10627E+04       4   0.90960E-04   0.10671E+01 0.73374E+01 
c  Velocity[X]                                      0.41203E+00 
c  Velocity[Y]                                      0.32899E+00 
c  Velocity[Z]                                      0.32611E+00 
c  Pressure     0.18422E+00     175   0.22431E-02   0.95820E-01 0.25882E+02 
c  k            0.43187E+03       4   0.29292E-03   0.20531E+00 0.86942E+01 
c  epsilon      0.47205E+04       4   0.40536E-02   0.33669E+03 0.37360E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.347          20.386        0.051569        0.089632
v  Velocity[Y]            -9.7014          10.003          1.0411          1.3161
v  Velocity[Z]            -15.415          15.492      -0.0066702     -0.00040176
v  ǁVelocityǁ           0.0064994          21.142          4.0826          2.5859
v  Pressure               -215.53           68.26         -1.1194          6.4284
v  k                   1.5047e-05           48.07          1.3641         0.61459
v  epsilon             1.2337e-07           16393           44.41          4.2246
v  TurbVisc            5.5136e-06         0.39489        0.056868        0.087769
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              134:        0.13819E+03

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


 INSTANT    0.112500000E+02   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.997034241E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079172E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.87227E-01 0.11875E+02
   Friction velocity        uet   :  0.37418E-03 0.66643E+00
   Friction velocity        uk    :  0.23643E-02 0.24294E+01
   Dimensionless distance   yplus :  0.45887E+01 0.32998E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          6
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        527 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10606E+04       4   0.88018E-04   0.10298E+01 0.71829E+01 
c  Velocity[X]                                      0.39649E+00 
c  Velocity[Y]                                      0.31864E+00 
c  Velocity[Z]                                      0.31464E+00 
c  Pressure     0.17072E+00     169   0.21109E-02   0.89361E-01 0.24049E+02 
c  k            0.43351E+03       4   0.28474E-03   0.20212E+00 0.86714E+01 
c  epsilon      0.46805E+04       4   0.31996E-02   0.28805E+03 0.35626E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.315            20.4        0.051675        0.089891
v  Velocity[Y]            -9.6734          10.006          1.0408          1.3163
v  Velocity[Z]            -15.407          15.472      -0.0066532     -0.00042834
v  ǁVelocityǁ           0.0069941          21.155          4.0839          2.5881
v  Pressure               -215.01          68.238         -0.7372          6.7436
v  k                   2.1535e-05          48.712          1.3643         0.61858
v  epsilon             1.2339e-07           16801          44.142          4.2197
v  TurbVisc            9.0119e-06         0.39489        0.056595        0.087238
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              135:        0.13680E+03

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


 INSTANT    0.122500000E+02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.858961479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079504E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44356E-01 0.11903E+02
   Friction velocity        uet   :  0.22609E-03 0.66549E+00
   Friction velocity        uk    :  0.26028E-02 0.24334E+01
   Dimensionless distance   yplus :  0.43523E+01 0.32906E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        522 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10586E+04       4   0.85436E-04   0.99607E+00 0.70453E+01 
c  Velocity[X]                                      0.38271E+00 
c  Velocity[Y]                                      0.30900E+00 
c  Velocity[Z]                                      0.30436E+00 
c  Pressure     0.16049E+00     156   0.20071E-02   0.84505E-01 0.21650E+02 
c  k            0.43511E+03       4   0.27803E-03   0.19912E+00 0.86471E+01 
c  epsilon      0.46414E+04       4   0.26786E-02   0.25510E+03 0.34272E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.329          20.411        0.051791        0.090149
v  Velocity[Y]            -9.6514          10.012          1.0405          1.3164
v  Velocity[Z]            -15.395          15.457      -0.0066438     -0.00045389
v  ǁVelocityǁ           0.0073303          21.165          4.0852          2.5904
v  Pressure               -214.53          68.178        -0.39486          7.0289
v  k                   3.0526e-05          48.993          1.3644         0.62247
v  epsilon             1.2342e-07           17076          43.876          4.2139
v  TurbVisc            1.4726e-05         0.39489        0.056323        0.086707
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              136:        0.13262E+03

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


 INSTANT    0.132500000E+02   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.515128403E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077522E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11978E-02 0.11931E+02
   Friction velocity        uet   :  0.36869E-03 0.66484E+00
   Friction velocity        uk    :  0.29510E-02 0.24325E+01
   Dimensionless distance   yplus :  0.41892E+01 0.32821E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        521 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10566E+04       4   0.83103E-04   0.96539E+00 0.69211E+01 
c  Velocity[X]                                      0.37036E+00 
c  Velocity[Y]                                      0.29999E+00 
c  Velocity[Z]                                      0.29504E+00 
c  Pressure     0.15398E+00     156   0.19405E-02   0.81533E-01 0.20595E+02 
c  k            0.43667E+03       4   0.27215E-03   0.19621E+00 0.86192E+01 
c  epsilon      0.46030E+04       4   0.23417E-02   0.23083E+03 0.33144E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.341          20.418        0.051918        0.090412
v  Velocity[Y]            -9.6341          10.012          1.0402          1.3166
v  Velocity[Z]            -15.396          15.446      -0.0066418     -0.00047814
v  ǁVelocityǁ           0.0060257          21.173          4.0866          2.5927
v  Pressure               -214.14          68.118       -0.058433          7.3133
v  k                   4.1328e-05          49.173          1.3643         0.62625
v  epsilon             1.2345e-07           17313          43.614          4.2071
v  TurbVisc            1.6612e-05          0.3949        0.056053        0.086178
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              137:        0.13373E+03

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


 INSTANT    0.142500000E+02   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.736935218E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077469E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11580E-02 0.11959E+02
   Friction velocity        uet   :  0.11582E-03 0.66444E+00
   Friction velocity        uk    :  0.33727E-02 0.24277E+01
   Dimensionless distance   yplus :  0.40116E+01 0.32746E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        519 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10546E+04       4   0.80993E-04   0.93725E+00 0.68080E+01 
c  Velocity[X]                                      0.35922E+00 
c  Velocity[Y]                                      0.29151E+00 
c  Velocity[Z]                                      0.28652E+00 
c  Pressure     0.15114E+00     155   0.18848E-02   0.80459E-01 0.18908E+02 
c  k            0.43821E+03       4   0.26692E-03   0.19338E+00 0.85871E+01 
c  epsilon      0.45653E+04       4   0.21185E-02   0.21168E+03 0.32155E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.349          20.422        0.052055        0.090681
v  Velocity[Y]            -9.6208          10.007            1.04          1.3167
v  Velocity[Z]            -15.387          15.437      -0.0066478     -0.00050077
v  ǁVelocityǁ           0.0047137          21.178           4.088          2.5949
v  Pressure               -213.89          68.033         0.25171          7.5781
v  k                   5.3365e-05          49.316          1.3641         0.62994
v  epsilon             1.2348e-07           17542          43.354          4.1996
v  TurbVisc            1.6184e-05          0.3949        0.055785        0.085653
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              138:        0.13056E+03

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


 INSTANT    0.152500000E+02   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.160061840E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077585E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.25932E-02 0.11987E+02
   Friction velocity        uet   :  0.38841E-03 0.66424E+00
   Friction velocity        uk    :  0.38197E-02 0.24199E+01
   Dimensionless distance   yplus :  0.37615E+01 0.32682E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        517 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10527E+04       4   0.79035E-04   0.91138E+00 0.67042E+01 
c  Velocity[X]                                      0.34911E+00 
c  Velocity[Y]                                      0.28356E+00 
c  Velocity[Z]                                      0.27870E+00 
c  Pressure     0.15187E+00     154   0.18548E-02   0.81261E-01 0.17605E+02 
c  k            0.43973E+03       4   0.26200E-03   0.19057E+00 0.85505E+01 
c  epsilon      0.45282E+04       4   0.19623E-02   0.19583E+03 0.31260E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.356          20.424        0.052203        0.090956
v  Velocity[Y]            -9.6107          9.9962          1.0397          1.3168
v  Velocity[Z]            -15.369          15.429      -0.0066609      -0.0005214
v  ǁVelocityǁ           0.0043937          21.182          4.0895          2.5972
v  Pressure               -213.75          67.936         0.54344          7.8295
v  k                   6.5659e-05          49.408          1.3639         0.63354
v  epsilon              1.235e-07           17759          43.099          4.1914
v  TurbVisc            1.2451e-05          0.3949        0.055519        0.085132
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              139:        0.13202E+03

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


 INSTANT    0.162500000E+02   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.104998686E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078012E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.18070E-02 0.12015E+02
   Friction velocity        uet   :  0.23665E-03 0.66421E+00
   Friction velocity        uk    :  0.42468E-02 0.24099E+01
   Dimensionless distance   yplus :  0.33771E+01 0.32630E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        533 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10509E+04       4   0.77216E-04   0.88736E+00 0.66082E+01 
c  Velocity[X]                                      0.33986E+00 
c  Velocity[Y]                                      0.27606E+00 
c  Velocity[Z]                                      0.27144E+00 
c  Pressure     0.14631E+00     153   0.17918E-02   0.78656E-01 0.16244E+02 
c  k            0.44123E+03       3   0.25774E-03   0.18778E+00 0.85093E+01 
c  epsilon      0.44917E+04       4   0.18386E-02   0.18214E+03 0.30425E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]             -20.36          20.424         0.05236        0.091238
v  Velocity[Y]            -9.6034          9.9924          1.0394          1.3169
v  Velocity[Z]            -15.346          15.421      -0.0066811     -0.00054069
v  ǁVelocityǁ           0.0045683          21.184           4.091          2.5995
v  Pressure                -213.7          67.888         0.81159          8.0635
v  k                   7.7464e-05          49.343          1.3635         0.63705
v  epsilon             1.2353e-07           17918          42.849          4.1827
v  TurbVisc            8.9484e-06         0.39491        0.055254        0.084615
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              140:        0.13088E+03

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


 INSTANT    0.172500000E+02   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.102497994E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078193E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.25239E-02 0.12043E+02
   Friction velocity        uet   :  0.57731E-03 0.66431E+00
   Friction velocity        uk    :  0.46303E-02 0.23982E+01
   Dimensionless distance   yplus :  0.28531E+01 0.32592E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        526 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10490E+04       4   0.75471E-04   0.86512E+00 0.65188E+01 
c  Velocity[X]                                      0.33139E+00 
c  Velocity[Y]                                      0.26903E+00 
c  Velocity[Z]                                      0.26470E+00 
c  Pressure     0.14376E+00     141   0.17496E-02   0.77636E-01 0.14843E+02 
c  k            0.44272E+03       3   0.25321E-03   0.18502E+00 0.84641E+01 
c  epsilon      0.44557E+04       4   0.17347E-02   0.17004E+03 0.29638E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.363          20.423        0.052526        0.091528
v  Velocity[Y]            -9.5984          10.012          1.0392           1.317
v  Velocity[Z]            -15.321          15.412      -0.0067076     -0.00055854
v  ǁVelocityǁ           0.0061507          21.185          4.0925          2.6018
v  Pressure               -213.72           67.81          1.0514           8.275
v  k                   8.8236e-05          49.122          1.3631         0.64049
v  epsilon             1.2357e-07           18015          42.604          4.1734
v  TurbVisc            6.2123e-06         0.39491        0.054992        0.084103
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              141:        0.12841E+03

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


 INSTANT    0.182500000E+02   TIME STEP NUMBER             142
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.691378179E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077582E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.21777E-02 0.12070E+02
   Friction velocity        uet   :  0.21848E-03 0.66453E+00
   Friction velocity        uk    :  0.49600E-02 0.23853E+01
   Dimensionless distance   yplus :  0.25399E+01 0.32565E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        530 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10473E+04       4   0.73872E-04   0.84433E+00 0.64353E+01 
c  Velocity[X]                                      0.32356E+00 
c  Velocity[Y]                                      0.26239E+00 
c  Velocity[Z]                                      0.25839E+00 
c  Pressure     0.13956E+00     141   0.17195E-02   0.75689E-01 0.14333E+02 
c  k            0.44419E+03       3   0.24891E-03   0.18227E+00 0.84150E+01 
c  epsilon      0.44203E+04       4   0.16465E-02   0.15926E+03 0.28892E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.364          20.421          0.0527        0.091825
v  Velocity[Y]            -9.5956          10.027          1.0389          1.3171
v  Velocity[Z]            -15.297          15.404      -0.0067395     -0.00057515
v  ǁVelocityǁ           0.0052112          21.186          4.0941           2.604
v  Pressure               -213.77          67.739          1.2906          8.4878
v  k                   9.7717e-05          48.795          1.3627         0.64385
v  epsilon              1.236e-07           18061          42.364          4.1636
v  TurbVisc             5.752e-06         0.39491        0.054732        0.083597
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              142:        0.12687E+03

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


 INSTANT    0.192500000E+02   TIME STEP NUMBER             143
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.795992830E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077336E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28629E-01 0.12097E+02
   Friction velocity        uet   :  0.21383E-04 0.66485E+00
   Friction velocity        uk    :  0.52049E-02 0.23719E+01
   Dimensionless distance   yplus :  0.31913E+01 0.32549E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          1
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        532 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10455E+04       4   0.72404E-04   0.82490E+00 0.63568E+01 
c  Velocity[X]                                      0.31631E+00 
c  Velocity[Y]                                      0.25611E+00 
c  Velocity[Z]                                      0.25248E+00 
c  Pressure     0.13782E+00     140   0.16698E-02   0.75052E-01 0.13506E+02 
c  k            0.44565E+03       3   0.24484E-03   0.17955E+00 0.83623E+01 
c  epsilon      0.43855E+04       4   0.15771E-02   0.14964E+03 0.28182E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.365          20.419        0.052882         0.09213
v  Velocity[Y]            -9.5944          10.037          1.0386          1.3172
v  Velocity[Z]            -15.276          15.394      -0.0067764     -0.00059096
v  ǁVelocityǁ           0.0048176          21.186          4.0957          2.6063
v  Pressure               -213.85          67.664          1.5173          8.6917
v  k                   0.00010081          48.414          1.3622         0.64713
v  epsilon             1.2363e-07           18076          42.132          4.1535
v  TurbVisc            6.5834e-06         0.39492        0.054474        0.083096
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              143:        0.12667E+03

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


 INSTANT    0.202500000E+02   TIME STEP NUMBER             144
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.186102970E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077622E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.13573E+00 0.12124E+02
   Friction velocity        uet   :  0.18537E-03 0.66653E+00
   Friction velocity        uk    :  0.53564E-02 0.23582E+01
   Dimensionless distance   yplus :  0.33570E+01 0.32541E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          2
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        540 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10438E+04       4   0.71022E-04   0.80663E+00 0.62828E+01 
c  Velocity[X]                                      0.30956E+00 
c  Velocity[Y]                                      0.25017E+00 
c  Velocity[Z]                                      0.24690E+00 
c  Pressure     0.13448E+00     139   0.16683E-02   0.73523E-01 0.12576E+02 
c  k            0.44710E+03       3   0.24068E-03   0.17685E+00 0.83064E+01 
c  epsilon      0.43513E+04       4   0.15148E-02   0.14096E+03 0.27503E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.365          20.417         0.05307        0.092443
v  Velocity[Y]            -9.5946          10.044          1.0384          1.3172
v  Velocity[Z]            -15.259          15.384       -0.006817     -0.00060566
v  ǁVelocityǁ           0.0053493          21.186          4.0973          2.6086
v  Pressure               -213.94          67.573           1.725          8.8813
v  k                   7.1844e-05           48.03          1.3617         0.65035
v  epsilon             1.2366e-07           18077          41.906          4.1431
v  TurbVisc            8.3829e-06         0.39492         0.05422        0.082601
v  total_pressure      1.0122e+05      1.0158e+05      1.0142e+05       1.014e+05


 TIME FOR THE TIME STEP              144:        0.12748E+03

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


 INSTANT    0.212500000E+02   TIME STEP NUMBER             145
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.160915728E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152077875E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25854E+00 0.12149E+02
   Friction velocity        uet   :  0.52319E-03 0.66829E+00
   Friction velocity        uk    :  0.55263E-02 0.23446E+01
   Dimensionless distance   yplus :  0.34659E+01 0.32538E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          4
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        554 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10422E+04       4   0.69812E-04   0.78946E+00 0.62128E+01 
c  Velocity[X]                                      0.30325E+00 
c  Velocity[Y]                                      0.24456E+00 
c  Velocity[Z]                                      0.24165E+00 
c  Pressure     0.13307E+00     137   0.15934E-02   0.73031E-01 0.11824E+02 
c  k            0.44855E+03       3   0.23671E-03   0.17418E+00 0.82475E+01 
c  epsilon      0.43178E+04       4   0.14638E-02   0.13303E+03 0.26851E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.365          20.415        0.053264        0.092765
v  Velocity[Y]            -9.5957          10.047          1.0381          1.3172
v  Velocity[Z]            -15.252          15.373      -0.0068607     -0.00062021
v  ǁVelocityǁ           0.0052136          21.186           4.099          2.6108
v  Pressure               -214.03          67.466          1.9185          9.0604
v  k                   5.1491e-05          47.679          1.3612         0.65351
v  epsilon             1.2369e-07           18080          41.687          4.1325
v  TurbVisc            7.6703e-06         0.39492         0.05397        0.082112
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              145:        0.12698E+03

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


 INSTANT    0.222500000E+02   TIME STEP NUMBER             146
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.620091533E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078228E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39459E+00 0.12174E+02
   Friction velocity        uet   :  0.27456E-03 0.67000E+00
   Friction velocity        uk    :  0.56999E-02 0.23315E+01
   Dimensionless distance   yplus :  0.36779E+01 0.32537E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          4
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        552 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10405E+04       4   0.68770E-04   0.77327E+00 0.61464E+01 
c  Velocity[X]                                      0.29732E+00 
c  Velocity[Y]                                      0.23927E+00 
c  Velocity[Z]                                      0.23668E+00 
c  Pressure     0.12712E+00     136   0.15676E-02   0.70022E-01 0.11202E+02 
c  k            0.44999E+03       3   0.23277E-03   0.17154E+00 0.81860E+01 
c  epsilon      0.42850E+04       4   0.14190E-02   0.12576E+03 0.26222E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.364          20.413        0.053461        0.093093
v  Velocity[Y]            -9.5977          10.049          1.0379          1.3172
v  Velocity[Z]            -15.246          15.361      -0.0069062     -0.00063485
v  ǁVelocityǁ            0.002876          21.185          4.1006          2.6131
v  Pressure               -214.13          67.349          2.1007          9.2314
v  k                   3.7125e-05          47.393          1.3607          0.6566
v  epsilon             1.2372e-07           18097          41.476          4.1216
v  TurbVisc             5.555e-06         0.39493        0.053724        0.081626
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              146:        0.12526E+03

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


 INSTANT    0.232500000E+02   TIME STEP NUMBER             147
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.843268800E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078714E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53839E+00 0.12197E+02
   Friction velocity        uet   :  0.29840E-03 0.67166E+00
   Friction velocity        uk    :  0.58641E-02 0.23190E+01
   Dimensionless distance   yplus :  0.40547E+01 0.32534E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          9
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        578 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10389E+04       4   0.67774E-04   0.75793E+00 0.60831E+01 
c  Velocity[X]                                      0.29174E+00 
c  Velocity[Y]                                      0.23423E+00 
c  Velocity[Z]                                      0.23196E+00 
c  Pressure     0.12266E+00     135   0.15411E-02   0.67806E-01 0.10526E+02 
c  k            0.45142E+03       3   0.22898E-03   0.16894E+00 0.81223E+01 
c  epsilon      0.42530E+04       4   0.13843E-02   0.11909E+03 0.25616E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.364          20.411        0.053661        0.093426
v  Velocity[Y]            -9.6005          10.048          1.0376          1.3172
v  Velocity[Z]             -15.24          15.347      -0.0069528     -0.00064969
v  ǁVelocityǁ          0.00097385          21.184          4.1024          2.6154
v  Pressure               -214.22          67.213          2.2675          9.3907
v  k                   2.6972e-05          47.197          1.3603         0.65963
v  epsilon             1.2375e-07           18142          41.273          4.1106
v  TurbVisc            4.0513e-06         0.39493        0.053482        0.081146
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              147:        0.12481E+03

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


 INSTANT    0.242500000E+02   TIME STEP NUMBER             148
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.311635373E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078775E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68122E+00 0.12219E+02
   Friction velocity        uet   :  0.10780E-03 0.67325E+00
   Friction velocity        uk    :  0.57362E-02 0.23073E+01
   Dimensionless distance   yplus :  0.45950E+01 0.32525E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         14
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        577 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10374E+04       4   0.66805E-04   0.74338E+00 0.60227E+01 
c  Velocity[X]                                      0.28646E+00 
c  Velocity[Y]                                      0.22944E+00 
c  Velocity[Z]                                      0.22748E+00 
c  Pressure     0.11797E+00     135   0.14971E-02   0.65437E-01 0.10073E+02 
c  k            0.45284E+03       3   0.22519E-03   0.16639E+00 0.80567E+01 
c  epsilon      0.42217E+04       5   0.13508E-02   0.11294E+03 0.25027E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.363           20.41        0.053862        0.093764
v  Velocity[Y]            -9.6039          10.046          1.0374          1.3172
v  Velocity[Z]            -15.234          15.333      -0.0070003     -0.00066429
v  ǁVelocityǁ           0.0017657          21.183          4.1041          2.6176
v  Pressure                -214.3          67.066          2.4268          9.5453
v  k                   1.9903e-05           47.12          1.3598         0.66261
v  epsilon             1.2379e-07           18224          41.078          4.0995
v  TurbVisc             2.982e-06         0.39494        0.053254        0.080689
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              148:        0.12528E+03

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


 INSTANT    0.252500000E+02   TIME STEP NUMBER             149
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.626076204E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078541E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.81235E+00 0.12240E+02
   Friction velocity        uet   :  0.20990E-03 0.67478E+00
   Friction velocity        uk    :  0.55596E-02 0.22966E+01
   Dimensionless distance   yplus :  0.48930E+01 0.32506E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         22
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        579 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10358E+04       4   0.65865E-04   0.72954E+00 0.59649E+01 
c  Velocity[X]                                      0.28146E+00 
c  Velocity[Y]                                      0.22487E+00 
c  Velocity[Z]                                      0.22321E+00 
c  Pressure     0.11627E+00     135   0.14849E-02   0.64700E-01 0.98694E+01 
c  k            0.45426E+03       3   0.22200E-03   0.16389E+00 0.79893E+01 
c  epsilon      0.41913E+04       4   0.13366E-02   0.10726E+03 0.24457E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.362          20.409        0.054063        0.094105
v  Velocity[Y]            -9.6077          10.042          1.0372          1.3171
v  Velocity[Z]            -15.228          15.318      -0.0070487     -0.00067896
v  ǁVelocityǁ           0.0060034          21.183          4.1059          2.6199
v  Pressure               -214.35          66.926          2.5891          9.7033
v  k                   1.5359e-05          47.179          1.3594         0.66554
v  epsilon             1.2382e-07           18354          40.891          4.0883
v  TurbVisc            2.2362e-06         0.39494        0.053014        0.080207
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              149:        0.12482E+03

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


 INSTANT    0.262500000E+02   TIME STEP NUMBER             150
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.881573849E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078673E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.92006E+00 0.12259E+02
   Friction velocity        uet   :  0.36960E-03 0.67625E+00
   Friction velocity        uk    :  0.55320E-02 0.22869E+01
   Dimensionless distance   yplus :  0.49475E+01 0.32472E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         27
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        584 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10343E+04       4   0.64968E-04   0.71635E+00 0.59094E+01 
c  Velocity[X]                                      0.27671E+00 
c  Velocity[Y]                                      0.22051E+00 
c  Velocity[Z]                                      0.21913E+00 
c  Pressure     0.12061E+00     135   0.14267E-02   0.67329E-01 0.95166E+01 
c  k            0.45567E+03       3   0.21943E-03   0.16144E+00 0.79206E+01 
c  epsilon      0.41616E+04       4   0.13555E-02   0.10198E+03 0.23907E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.361          20.409        0.054265        0.094448
v  Velocity[Y]            -9.6117          10.038          1.0369          1.3171
v  Velocity[Z]            -15.222          15.302      -0.0070975     -0.00069329
v  ǁVelocityǁ           0.0068573          21.182          4.1077          2.6221
v  Pressure               -214.37          66.785          2.7464          9.8586
v  k                   1.8844e-05          47.342           1.359         0.66841
v  epsilon             1.2386e-07           18522          40.712           4.077
v  TurbVisc            1.7661e-06         0.39494        0.052779        0.079731
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05       1.014e+05


 TIME FOR THE TIME STEP              150:        0.12484E+03

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


 INSTANT    0.272500000E+02   TIME STEP NUMBER             151
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.521355249E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078934E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.94590E+00 0.12277E+02
   Friction velocity        uet   :  0.50858E-03 0.67763E+00
   Friction velocity        uk    :  0.56270E-02 0.22782E+01
   Dimensionless distance   yplus :  0.50047E+01 0.32421E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         32
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        591 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10328E+04       4   0.64143E-04   0.70375E+00 0.58559E+01 
c  Velocity[X]                                      0.27217E+00 
c  Velocity[Y]                                      0.21634E+00 
c  Velocity[Z]                                      0.21524E+00 
c  Pressure     0.11285E+00     135   0.14318E-02   0.63191E-01 0.90274E+01 
c  k            0.45708E+03       3   0.21786E-03   0.15904E+00 0.78508E+01 
c  epsilon      0.41328E+04       4   0.14422E-02   0.97136E+02 0.23374E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.359          20.409        0.054463        0.094791
v  Velocity[Y]            -9.6159          10.033          1.0367           1.317
v  Velocity[Z]            -15.216          15.286      -0.0071457      -0.0007069
v  ǁVelocityǁ           0.0056029          21.181          4.1095          2.6244
v  Pressure               -214.39          66.635          2.8913          10.004
v  k                   1.4258e-05          47.562          1.3587         0.67124
v  epsilon              1.239e-07           18715          40.541          4.0658
v  TurbVisc             1.842e-06         0.39495        0.052554        0.079271
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              151:        0.12493E+03

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


 INSTANT    0.282500000E+02   TIME STEP NUMBER             152
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.293584778E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078887E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.86971E+00 0.12294E+02
   Friction velocity        uet   :  0.27988E-03 0.67894E+00
   Friction velocity        uk    :  0.57842E-02 0.22706E+01
   Dimensionless distance   yplus :  0.50487E+01 0.32348E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         37
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        607 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10314E+04       4   0.63274E-04   0.69171E+00 0.58042E+01 
c  Velocity[X]                                      0.26783E+00 
c  Velocity[Y]                                      0.21237E+00 
c  Velocity[Z]                                      0.21151E+00 
c  Pressure     0.11309E+00     135   0.14362E-02   0.63505E-01 0.89051E+01 
c  k            0.45848E+03       3   0.21653E-03   0.15670E+00 0.77800E+01 
c  epsilon      0.41046E+04       4   0.15533E-02   0.92345E+02 0.22841E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.358          20.409        0.054658        0.095133
v  Velocity[Y]            -9.6201          10.028          1.0365          1.3169
v  Velocity[Z]             -15.21          15.269      -0.0071929     -0.00071994
v  ǁVelocityǁ           0.0054985           21.18          4.1113          2.6266
v  Pressure               -214.37          66.496          3.0407          10.155
v  k                   9.8745e-06          47.767          1.3584         0.67402
v  epsilon             1.2394e-07           18904          40.378          4.0545
v  TurbVisc            1.4358e-06         0.39495        0.052336        0.078822
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              152:        0.12492E+03

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


 INSTANT    0.292500000E+02   TIME STEP NUMBER             153
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.165320599E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078988E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.76594E+00 0.12309E+02
   Friction velocity        uet   :  0.40212E-03 0.68016E+00
   Friction velocity        uk    :  0.51737E-02 0.22639E+01
   Dimensionless distance   yplus :  0.50798E+01 0.32249E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         41
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        612 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10299E+04       4   0.62469E-04   0.68019E+00 0.57542E+01 
c  Velocity[X]                                      0.26369E+00 
c  Velocity[Y]                                      0.20856E+00 
c  Velocity[Z]                                      0.20794E+00 
c  Pressure     0.11575E+00     135   0.14597E-02   0.65181E-01 0.86226E+01 
c  k            0.45988E+03       3   0.21435E-03   0.15440E+00 0.77085E+01 
c  epsilon      0.40772E+04       4   0.16135E-02   0.87772E+02 0.22317E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.357          20.409        0.054849        0.095474
v  Velocity[Y]            -9.6242          10.022          1.0363          1.3167
v  Velocity[Z]            -15.204          15.251      -0.0072386     -0.00073198
v  ǁVelocityǁ           0.0057407          21.179          4.1132          2.6288
v  Pressure               -214.33          66.358          3.1859          10.303
v  k                   6.9549e-06           47.88          1.3582         0.67675
v  epsilon             1.2398e-07           19056          40.224          4.0433
v  TurbVisc            1.1422e-06         0.39496        0.052124         0.07838
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              153:        0.12496E+03

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


 INSTANT    0.302500000E+02   TIME STEP NUMBER             154
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.189370125E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079063E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.70425E+00 0.12322E+02
   Friction velocity        uet   :  0.72799E-03 0.68130E+00
   Friction velocity        uk    :  0.46071E-02 0.22582E+01
   Dimensionless distance   yplus :  0.50928E+01 0.32124E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         44
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        612 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10285E+04       4   0.61750E-04   0.66922E+00 0.57060E+01 
c  Velocity[X]                                      0.25974E+00 
c  Velocity[Y]                                      0.20497E+00 
c  Velocity[Z]                                      0.20451E+00 
c  Pressure     0.12657E+00     135   0.15311E-02   0.71472E-01 0.83343E+01 
c  k            0.46128E+03       3   0.21079E-03   0.15214E+00 0.76368E+01 
c  epsilon      0.40504E+04       4   0.15798E-02   0.83480E+02 0.21808E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.356           20.41        0.055034        0.095811
v  Velocity[Y]            -9.6281          10.016          1.0361          1.3166
v  Velocity[Z]            -15.199          15.233      -0.0072827     -0.00074368
v  ǁVelocityǁ           0.0044094          21.178           4.115           2.631
v  Pressure               -214.27          66.223           3.327          10.447
v  k                    6.984e-06          47.882           1.358         0.67945
v  epsilon             1.2402e-07           19161          40.076          4.0322
v  TurbVisc            8.3335e-07         0.39496        0.051917        0.077945
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              154:        0.12584E+03

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


 INSTANT    0.312500000E+02   TIME STEP NUMBER             155
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.140281752E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079130E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56710E+00 0.12333E+02
   Friction velocity        uet   :  0.54665E-03 0.68234E+00
   Friction velocity        uk    :  0.61809E-02 0.22533E+01
   Dimensionless distance   yplus :  0.50848E+01 0.31970E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         46
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        620 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10272E+04       4   0.61054E-04   0.65863E+00 0.56593E+01 
c  Velocity[X]                                      0.25592E+00 
c  Velocity[Y]                                      0.20150E+00 
c  Velocity[Z]                                      0.20121E+00 
c  Pressure     0.13388E+00     135   0.16247E-02   0.75808E-01 0.81235E+01 
c  k            0.46267E+03       3   0.20644E-03   0.14994E+00 0.75647E+01 
c  epsilon      0.40245E+04       4   0.14697E-02   0.79450E+02 0.21317E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.355           20.41        0.055211        0.096142
v  Velocity[Y]            -9.6318           10.01          1.0359          1.3164
v  Velocity[Z]            -15.193          15.214      -0.0073255     -0.00075495
v  ǁVelocityǁ           0.0032254          21.177          4.1169          2.6333
v  Pressure               -214.19          66.098          3.4662          10.591
v  k                   6.0969e-06          47.793          1.3579          0.6821
v  epsilon             1.2406e-07           19226          39.936          4.0211
v  TurbVisc            9.6626e-07         0.39496        0.051715        0.077518
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              155:        0.12753E+03

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


 INSTANT    0.322500000E+02   TIME STEP NUMBER             156
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.106940040E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079202E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54358E+00 0.12344E+02
   Friction velocity        uet   :  0.37950E-03 0.68330E+00
   Friction velocity        uk    :  0.55847E-02 0.22493E+01
   Dimensionless distance   yplus :  0.50601E+01 0.31786E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         45
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        629 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10258E+04       4   0.60360E-04   0.64840E+00 0.56139E+01 
c  Velocity[X]                                      0.25226E+00 
c  Velocity[Y]                                      0.19814E+00 
c  Velocity[Z]                                      0.19800E+00 
c  Pressure     0.16719E+00     135   0.22282E-02   0.94905E-01 0.79632E+01 
c  k            0.46406E+03       3   0.20198E-03   0.14779E+00 0.74928E+01 
c  epsilon      0.39993E+04       4   0.13217E-02   0.75632E+02 0.20840E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.353          20.411        0.055381        0.096467
v  Velocity[Y]            -9.6351          10.004          1.0357          1.3163
v  Velocity[Z]            -15.188          15.196       -0.007367      -0.0007663
v  ǁVelocityǁ            0.004672          21.176          4.1188          2.6355
v  Pressure               -214.09          66.028           3.606          10.736
v  k                   4.2517e-06          47.648          1.3579         0.68471
v  epsilon             1.2411e-07           19264          39.804          4.0101
v  TurbVisc            7.7707e-07         0.39497        0.051518          0.0771
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              156:        0.12684E+03

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


 INSTANT    0.332500000E+02   TIME STEP NUMBER             157
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.244117243E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079125E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43643E+00 0.12352E+02
   Friction velocity        uet   :  0.19851E-03 0.68416E+00
   Friction velocity        uk    :  0.41093E-02 0.22459E+01
   Dimensionless distance   yplus :  0.50240E+01 0.31571E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         42
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        632 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10245E+04       4   0.59670E-04   0.63864E+00 0.55700E+01 
c  Velocity[X]                                      0.24874E+00 
c  Velocity[Y]                                      0.19497E+00 
c  Velocity[Z]                                      0.19493E+00 
c  Pressure     0.15691E+00     134   0.18151E-02   0.89292E-01 0.77985E+01 
c  k            0.46545E+03       3   0.19807E-03   0.14569E+00 0.74210E+01 
c  epsilon      0.39750E+04       4   0.11921E-02   0.72020E+02 0.20376E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.352          20.412        0.055542        0.096784
v  Velocity[Y]            -9.6381           9.998          1.0355          1.3161
v  Velocity[Z]            -15.183          15.178      -0.0074071     -0.00077735
v  ǁVelocityǁ           0.0059763          21.175          4.1208          2.6377
v  Pressure               -213.97          65.963          3.7466          10.881
v  k                   3.5215e-06          47.486          1.3579         0.68728
v  epsilon             1.2417e-07           19290          39.678          3.9992
v  TurbVisc            5.5185e-07         0.39498        0.051325        0.076692
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              157:        0.12685E+03

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


 INSTANT    0.342500000E+02   TIME STEP NUMBER             158
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.187254352E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079473E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51438E+00 0.12359E+02
   Friction velocity        uet   :  0.48433E-04 0.68492E+00
   Friction velocity        uk    :  0.55871E-02 0.22432E+01
   Dimensionless distance   yplus :  0.49841E+01 0.31325E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         40
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        629 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10233E+04       4   0.59030E-04   0.62918E+00 0.55274E+01 
c  Velocity[X]                                      0.24534E+00 
c  Velocity[Y]                                      0.19189E+00 
c  Velocity[Z]                                      0.19195E+00 
c  Pressure     0.15781E+00     134   0.19446E-02   0.90022E-01 0.74686E+01 
c  k            0.46683E+03       3   0.19471E-03   0.14363E+00 0.73496E+01 
c  epsilon      0.39514E+04       4   0.10976E-02   0.68620E+02 0.19925E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.351          20.412        0.055693        0.097092
v  Velocity[Y]            -9.6407          9.9918          1.0353          1.3159
v  Velocity[Z]            -15.187          15.165      -0.0074457      -0.0007875
v  ǁVelocityǁ           0.0090289          21.174          4.1227          2.6399
v  Pressure               -213.84          65.888          3.8784           11.02
v  k                   1.3888e-05          47.338          1.3579         0.68982
v  epsilon             1.2424e-07           19319           39.56          3.9884
v  TurbVisc            4.8582e-07         0.39498        0.051137        0.076294
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              158:        0.12683E+03

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


 INSTANT    0.352500000E+02   TIME STEP NUMBER             159
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.242298421E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079414E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.79992E+00 0.12364E+02
   Friction velocity        uet   :  0.25246E-03 0.68557E+00
   Friction velocity        uk    :  0.53017E-02 0.22410E+01
   Dimensionless distance   yplus :  0.49474E+01 0.31050E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         35
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        626 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10220E+04       4   0.58398E-04   0.62008E+00 0.54860E+01 
c  Velocity[X]                                      0.24206E+00 
c  Velocity[Y]                                      0.18893E+00 
c  Velocity[Z]                                      0.18908E+00 
c  Pressure     0.15086E+00     135   0.21535E-02   0.86260E-01 0.72976E+01 
c  k            0.46821E+03       3   0.19173E-03   0.14162E+00 0.72787E+01 
c  epsilon      0.39286E+04       4   0.10326E-02   0.65399E+02 0.19486E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]             -20.35          20.413        0.055835        0.097391
v  Velocity[Y]            -9.6428          9.9857          1.0351          1.3156
v  Velocity[Z]            -15.191          15.159      -0.0074828     -0.00079685
v  ǁVelocityǁ           0.0085348          21.174          4.1247          2.6421
v  Pressure                -213.7          65.815          4.0098          11.158
v  k                   2.9879e-05          47.227           1.358         0.69232
v  epsilon             1.2436e-07           19360          39.447          3.9778
v  TurbVisc             1.494e-06         0.39499        0.050952        0.075904
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              159:        0.12581E+03

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


 INSTANT    0.362500000E+02   TIME STEP NUMBER             160
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.881548025E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079269E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40020E+00 0.12367E+02
   Friction velocity        uet   :  0.12853E-03 0.68613E+00
   Friction velocity        uk    :  0.60133E-02 0.22393E+01
   Dimensionless distance   yplus :  0.49191E+01 0.30748E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         31
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        618 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10208E+04       4   0.57778E-04   0.61125E+00 0.54457E+01 
c  Velocity[X]                                      0.23887E+00 
c  Velocity[Y]                                      0.18609E+00 
c  Velocity[Z]                                      0.18628E+00 
c  Pressure     0.12263E+00     135   0.16493E-02   0.70272E-01 0.72681E+01 
c  k            0.46959E+03       3   0.18906E-03   0.13966E+00 0.72084E+01 
c  epsilon      0.39065E+04       4   0.99624E-03   0.62395E+02 0.19060E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.348          20.414        0.055968         0.09768
v  Velocity[Y]            -9.6445          9.9795          1.0348          1.3154
v  Velocity[Z]            -15.195          15.154      -0.0075189     -0.00080626
v  ǁVelocityǁ           0.0073031          21.173          4.1266          2.6443
v  Pressure               -213.55           65.75          4.1472          11.301
v  k                   2.3089e-05          47.163          1.3582         0.69479
v  epsilon             1.2446e-07           19418          39.341          3.9673
v  TurbVisc            3.1319e-06         0.39499         0.05077        0.075522
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              160:        0.12493E+03

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


 INSTANT    0.372500000E+02   TIME STEP NUMBER             161
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.201174711E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079434E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33928E+00 0.12369E+02
   Friction velocity        uet   :  0.20956E-03 0.68657E+00
   Friction velocity        uk    :  0.65398E-02 0.22380E+01
   Dimensionless distance   yplus :  0.49004E+01 0.30422E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         18
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        596 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10196E+04       4   0.57178E-04   0.60275E+00 0.54065E+01 
c  Velocity[X]                                      0.23580E+00 
c  Velocity[Y]                                      0.18336E+00 
c  Velocity[Z]                                      0.18358E+00 
c  Pressure     0.11590E+00     134   0.15035E-02   0.66558E-01 0.69580E+01 
c  k            0.47097E+03       3   0.18656E-03   0.13775E+00 0.71390E+01 
c  epsilon      0.38852E+04       4   0.97923E-03   0.59590E+02 0.18650E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.347          20.414        0.056092        0.097959
v  Velocity[Y]            -9.6456          9.9735          1.0346          1.3151
v  Velocity[Z]            -15.198          15.149      -0.0075537     -0.00081507
v  ǁVelocityǁ           0.0088893          21.173          4.1286          2.6465
v  Pressure               -213.39          65.676          4.2761          11.437
v  k                    1.776e-05          47.134          1.3585         0.69723
v  epsilon             1.2459e-07           19490          39.241           3.957
v  TurbVisc            5.3164e-06           0.395        0.050591        0.075149
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              161:        0.12480E+03

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


 INSTANT    0.382500000E+02   TIME STEP NUMBER             162
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.677753782E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079401E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19054E+00 0.12368E+02
   Friction velocity        uet   :  0.17914E-03 0.68691E+00
   Friction velocity        uk    :  0.65249E-02 0.22371E+01
   Dimensionless distance   yplus :  0.48984E+01 0.30075E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          7
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        583 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10184E+04       4   0.56578E-04   0.59450E+00 0.53685E+01 
c  Velocity[X]                                      0.23283E+00 
c  Velocity[Y]                                      0.18070E+00 
c  Velocity[Z]                                      0.18096E+00 
c  Pressure     0.11260E+00     134   0.13574E-02   0.64798E-01 0.68278E+01 
c  k            0.47235E+03       3   0.18434E-03   0.13588E+00 0.70705E+01 
c  epsilon      0.38647E+04       4   0.98626E-03   0.56941E+02 0.18249E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.346          20.415        0.056207        0.098228
v  Velocity[Y]            -9.6462          9.9676          1.0344          1.3149
v  Velocity[Z]            -15.201          15.145       -0.007588     -0.00082404
v  ǁVelocityǁ           0.0060905          21.172          4.1306          2.6486
v  Pressure               -213.23          65.605          4.4058          11.573
v  k                   1.3619e-05          47.042          1.3587         0.69963
v  epsilon             1.2473e-07           19540          39.146          3.9468
v  TurbVisc            4.9619e-06           0.395        0.050415        0.074781
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              162:        0.12507E+03

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


 INSTANT    0.392500000E+02   TIME STEP NUMBER             163
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.169457481E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079328E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.21694E-02 0.12367E+02
   Friction velocity        uet   :  0.28029E-03 0.68714E+00
   Friction velocity        uk    :  0.65018E-02 0.22365E+01
   Dimensionless distance   yplus :  0.49196E+01 0.29712E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        585 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10172E+04       4   0.55966E-04   0.58654E+00 0.53316E+01 
c  Velocity[X]                                      0.22996E+00 
c  Velocity[Y]                                      0.17816E+00 
c  Velocity[Z]                                      0.17842E+00 
c  Pressure     0.10827E+00     134   0.13099E-02   0.62431E-01 0.66401E+01 
c  k            0.47372E+03       3   0.18210E-03   0.13405E+00 0.70031E+01 
c  epsilon      0.38447E+04       4   0.99550E-03   0.54443E+02 0.17862E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.345          20.415        0.056313        0.098487
v  Velocity[Y]            -9.6463          9.9619          1.0342          1.3146
v  Velocity[Z]            -15.204          15.141      -0.0076214     -0.00083247
v  ǁVelocityǁ           0.0084804          21.172          4.1326          2.6508
v  Pressure               -213.05          65.533          4.5333          11.708
v  k                   1.0445e-05          46.834          1.3591         0.70201
v  epsilon             1.2488e-07           19544          39.057          3.9367
v  TurbVisc            3.7324e-06         0.39501        0.050243        0.074421
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              163:        0.12504E+03

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


 INSTANT    0.402500000E+02   TIME STEP NUMBER             164
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.832486754E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079443E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.34400E-02 0.12363E+02
   Friction velocity        uet   :  0.44501E-03 0.68726E+00
   Friction velocity        uk    :  0.64702E-02 0.22363E+01
   Dimensionless distance   yplus :  0.49668E+01 0.29339E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        578 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10161E+04       4   0.55355E-04   0.57877E+00 0.52956E+01 
c  Velocity[X]                                      0.22715E+00 
c  Velocity[Y]                                      0.17567E+00 
c  Velocity[Z]                                      0.17595E+00 
c  Pressure     0.10839E+00     134   0.12529E-02   0.62619E-01 0.64824E+01 
c  k            0.47510E+03       3   0.17969E-03   0.13227E+00 0.69367E+01 
c  epsilon      0.38254E+04       4   0.99018E-03   0.52094E+02 0.17490E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.343          20.415        0.056411        0.098736
v  Velocity[Y]            -9.6458          9.9562          1.0339          1.3143
v  Velocity[Z]            -15.207          15.142      -0.0076544     -0.00084005
v  ǁVelocityǁ           0.0055808          21.171          4.1346           2.653
v  Pressure               -212.87          65.459          4.6594           11.84
v  k                   8.0083e-06          46.463          1.3595         0.70436
v  epsilon             1.2505e-07           19476          38.973          3.9269
v  TurbVisc            2.8025e-06         0.39502        0.050075        0.074068
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              164:        0.12510E+03

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


 INSTANT    0.412500000E+02   TIME STEP NUMBER             165
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.251878338E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079529E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.36112E-02 0.12358E+02
   Friction velocity        uet   :  0.40774E-03 0.68727E+00
   Friction velocity        uk    :  0.64287E-02 0.22362E+01
   Dimensionless distance   yplus :  0.50401E+01 0.29207E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        594 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10150E+04       4   0.54787E-04   0.57124E+00 0.52606E+01 
c  Velocity[X]                                      0.22442E+00 
c  Velocity[Y]                                      0.17328E+00 
c  Velocity[Z]                                      0.17355E+00 
c  Pressure     0.10020E+00     132   0.11944E-02   0.57997E-01 0.62755E+01 
c  k            0.47647E+03       3   0.17727E-03   0.13052E+00 0.68713E+01 
c  epsilon      0.38066E+04       4   0.98134E-03   0.49900E+02 0.17135E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.342          20.416          0.0565        0.098974
v  Velocity[Y]            -9.6449          9.9508          1.0337           1.314
v  Velocity[Z]             -15.21          15.143      -0.0076883     -0.00084761
v  ǁVelocityǁ           0.0058169          21.171          4.1366          2.6551
v  Pressure               -212.69          65.384          4.7819          11.969
v  k                   6.1623e-06          45.958            1.36         0.70669
v  epsilon              1.252e-07           19346          38.894          3.9172
v  TurbVisc            2.0913e-06         0.39502        0.049911        0.073722
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              165:        0.12459E+03

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


 INSTANT    0.422500000E+02   TIME STEP NUMBER             166
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.184867865E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079704E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45575E-01 0.12351E+02
   Friction velocity        uet   :  0.58900E-03 0.68716E+00
   Friction velocity        uk    :  0.63752E-02 0.22364E+01
   Dimensionless distance   yplus :  0.51399E+01 0.29083E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          3
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        600 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10139E+04       4   0.54194E-04   0.56395E+00 0.52265E+01 
c  Velocity[X]                                      0.22177E+00 
c  Velocity[Y]                                      0.17097E+00 
c  Velocity[Z]                                      0.17121E+00 
c  Pressure     0.11843E+00     121   0.12038E-02   0.68673E-01 0.58535E+01 
c  k            0.47785E+03       3   0.17475E-03   0.12880E+00 0.68068E+01 
c  epsilon      0.37884E+04       4   0.95591E-03   0.47807E+02 0.16791E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.341          20.416        0.056582        0.099201
v  Velocity[Y]            -9.6433          9.9455          1.0334          1.3137
v  Velocity[Z]            -15.213          15.143      -0.0077233     -0.00085403
v  ǁVelocityǁ           0.0045062          21.171          4.1386          2.6572
v  Pressure               -212.53          65.293           4.888          12.083
v  k                   4.7385e-06          45.378          1.3605         0.70898
v  epsilon             1.2543e-07           19175           38.82          3.9077
v  TurbVisc            1.5484e-06         0.39503         0.04975        0.073382
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              166:        0.12080E+03

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


 INSTANT    0.432500000E+02   TIME STEP NUMBER             167
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.913439139E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152078964E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.98628E-01 0.12342E+02
   Friction velocity        uet   :  0.21164E-03 0.68694E+00
   Friction velocity        uk    :  0.63089E-02 0.22367E+01
   Dimensionless distance   yplus :  0.52613E+01 0.28927E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          6
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        618 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10128E+04       4   0.53615E-04   0.55682E+00 0.51933E+01 
c  Velocity[X]                                      0.21917E+00 
c  Velocity[Y]                                      0.16872E+00 
c  Velocity[Z]                                      0.16893E+00 
c  Pressure     0.96662E-01     132   0.11573E-02   0.56147E-01 0.60825E+01 
c  k            0.47922E+03       3   0.17224E-03   0.12712E+00 0.67432E+01 
c  epsilon      0.37708E+04       4   0.92575E-03   0.45799E+02 0.16456E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.339          20.416        0.056657        0.099419
v  Velocity[Y]            -9.6413          9.9405          1.0332          1.3134
v  Velocity[Z]            -15.215          15.144      -0.0077602     -0.00085965
v  ǁVelocityǁ           0.0068276          21.171          4.1407          2.6593
v  Pressure               -212.34          65.225          5.0132          12.214
v  k                   3.6605e-06          44.752          1.3611         0.71126
v  epsilon             1.2571e-07           18979           38.75          3.8983
v  TurbVisc            1.1387e-06         0.39503        0.049594        0.073048
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              167:        0.12447E+03

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


 INSTANT    0.442500000E+02   TIME STEP NUMBER             168
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.271492766E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079736E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15350E+00 0.12331E+02
   Friction velocity        uet   :  0.25514E-03 0.68661E+00
   Friction velocity        uk    :  0.62271E-02 0.22371E+01
   Dimensionless distance   yplus :  0.53972E+01 0.28744E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         10
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        633 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10118E+04       4   0.53081E-04   0.54992E+00 0.51608E+01 
c  Velocity[X]                                      0.21664E+00 
c  Velocity[Y]                                      0.16656E+00 
c  Velocity[Z]                                      0.16672E+00 
c  Pressure     0.90533E-01     120   0.11309E-02   0.52673E-01 0.55011E+01 
c  k            0.48059E+03       3   0.16981E-03   0.12547E+00 0.66804E+01 
c  epsilon      0.37539E+04       4   0.89700E-03   0.43876E+02 0.16129E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.338          20.416        0.056724        0.099626
v  Velocity[Y]            -9.6389          9.9357          1.0329          1.3131
v  Velocity[Z]            -15.217          15.145      -0.0077992     -0.00086449
v  ǁVelocityǁ           0.0055615          21.171          4.1427          2.6614
v  Pressure               -212.18          65.125           5.113          12.321
v  k                   2.8578e-06          44.112          1.3617         0.71351
v  epsilon             1.2602e-07           18772          38.684          3.8892
v  TurbVisc            8.3408e-07         0.39504        0.049442        0.072721
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              168:        0.12071E+03

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


 INSTANT    0.452500000E+02   TIME STEP NUMBER             169
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.189680271E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079228E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.21008E+00 0.12319E+02
   Friction velocity        uet   :  0.60028E-03 0.68616E+00
   Friction velocity        uk    :  0.59137E-02 0.22376E+01
   Dimensionless distance   yplus :  0.55520E+01 0.28534E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         11
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        647 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10107E+04       4   0.52554E-04   0.54321E+00 0.51291E+01 
c  Velocity[X]                                      0.21418E+00 
c  Velocity[Y]                                      0.16447E+00 
c  Velocity[Z]                                      0.16456E+00 
c  Pressure     0.87884E-01     120   0.11085E-02   0.51213E-01 0.55087E+01 
c  k            0.48196E+03       3   0.16749E-03   0.12386E+00 0.66185E+01 
c  epsilon      0.37375E+04       4   0.88452E-03   0.42083E+02 0.15814E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.336          20.416        0.056787        0.099825
v  Velocity[Y]             -9.636          9.9312          1.0326          1.3127
v  Velocity[Z]            -15.219          15.145        -0.00784     -0.00086833
v  ǁVelocityǁ            0.001768          21.171          4.1448          2.6635
v  Pressure                  -212          65.033          5.2197          12.434
v  k                   2.0284e-06          43.432          1.3624         0.71574
v  epsilon             1.2623e-07           18542          38.623          3.8802
v  TurbVisc            6.1014e-07         0.39504        0.049294          0.0724
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              169:        0.12060E+03

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


 INSTANT    0.462500000E+02   TIME STEP NUMBER             170
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.316422724E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079279E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27093E+00 0.12305E+02
   Friction velocity        uet   :  0.61886E-03 0.68561E+00
   Friction velocity        uk    :  0.54837E-02 0.22382E+01
   Dimensionless distance   yplus :  0.57102E+01 0.28298E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         12
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        654 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10097E+04       4   0.52033E-04   0.53666E+00 0.50980E+01 
c  Velocity[X]                                      0.21176E+00 
c  Velocity[Y]                                      0.16243E+00 
c  Velocity[Z]                                      0.16246E+00 
c  Pressure     0.85873E-01     120   0.11026E-02   0.50119E-01 0.52956E+01 
c  k            0.48332E+03       3   0.16528E-03   0.12228E+00 0.65574E+01 
c  epsilon      0.37217E+04       4   0.88747E-03   0.40420E+02 0.15513E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.335          20.415        0.056846         0.10002
v  Velocity[Y]            -9.6327          9.9269          1.0323          1.3124
v  Velocity[Z]            -15.221          15.146      -0.0078823     -0.00087128
v  ǁVelocityǁ           0.0060144          21.171          4.1469          2.6656
v  Pressure               -211.83          64.933          5.3207          12.541
v  k                   1.4447e-06          42.697          1.3631         0.71795
v  epsilon             1.2651e-07           18282          38.565          3.8715
v  TurbVisc             4.467e-07         0.39505         0.04915        0.072084
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              170:        0.12065E+03

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


 INSTANT    0.472500000E+02   TIME STEP NUMBER             171
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.147525261E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079340E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34066E+00 0.12296E+02
   Friction velocity        uet   :  0.61668E-03 0.68494E+00
   Friction velocity        uk    :  0.52239E-02 0.22389E+01
   Dimensionless distance   yplus :  0.58025E+01 0.28038E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         15
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        665 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10087E+04       4   0.51528E-04   0.53028E+00 0.50676E+01 
c  Velocity[X]                                      0.20940E+00 
c  Velocity[Y]                                      0.16047E+00 
c  Velocity[Z]                                      0.16040E+00 
c  Pressure     0.82425E-01     118   0.10371E-02   0.48178E-01 0.51247E+01 
c  k            0.48469E+03       3   0.16316E-03   0.12074E+00 0.64973E+01 
c  epsilon      0.37064E+04       4   0.89955E-03   0.38867E+02 0.15223E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.334          20.415        0.056902          0.1002
v  Velocity[Y]            -9.6291          9.9229           1.032           1.312
v  Velocity[Z]            -15.223          15.146      -0.0079267     -0.00087348
v  ǁVelocityǁ           0.0056274          21.172           4.149          2.6677
v  Pressure               -211.67          64.827           5.418          12.644
v  k                   1.0356e-06          41.907          1.3639         0.72014
v  epsilon             1.2675e-07           17990          38.511          3.8629
v  TurbVisc            3.2779e-07         0.39506        0.049011        0.071774
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              171:        0.12031E+03

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


 INSTANT    0.482500000E+02   TIME STEP NUMBER             172
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.260673491E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079511E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40193E+00 0.12288E+02
   Friction velocity        uet   :  0.47648E-03 0.68423E+00
   Friction velocity        uk    :  0.50995E-02 0.22396E+01
   Dimensionless distance   yplus :  0.59520E+01 0.27757E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         19
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        681 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10077E+04       4   0.51059E-04   0.52405E+00 0.50377E+01 
c  Velocity[X]                                      0.20709E+00 
c  Velocity[Y]                                      0.15857E+00 
c  Velocity[Z]                                      0.15839E+00 
c  Pressure     0.83381E-01     117   0.10268E-02   0.48808E-01 0.49246E+01 
c  k            0.48605E+03       3   0.16109E-03   0.11923E+00 0.64380E+01 
c  epsilon      0.36916E+04       4   0.91358E-03   0.37406E+02 0.14943E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.332          20.415        0.056955         0.10038
v  Velocity[Y]            -9.6253          9.9193          1.0316          1.3116
v  Velocity[Z]            -15.224          15.146      -0.0079718      -0.0008743
v  ǁVelocityǁ           0.0086007          21.172          4.1511          2.6698
v  Pressure               -211.51          64.711          5.5089          12.741
v  k                   7.4916e-07          41.071          1.3647         0.72231
v  epsilon             1.2696e-07           17671          38.461          3.8545
v  TurbVisc            2.4131e-07         0.39506        0.048877        0.071469
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              172:        0.12003E+03

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


 INSTANT    0.492500000E+02   TIME STEP NUMBER             173
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.583456399E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079749E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39333E+00 0.12279E+02
   Friction velocity        uet   :  0.15784E-03 0.68374E+00
   Friction velocity        uk    :  0.50566E-02 0.22402E+01
   Dimensionless distance   yplus :  0.56745E+01 0.27456E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         22
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        696 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10067E+04       4   0.50578E-04   0.51798E+00 0.50084E+01 
c  Velocity[X]                                      0.20481E+00 
c  Velocity[Y]                                      0.15674E+00 
c  Velocity[Z]                                      0.15643E+00 
c  Pressure     0.79655E-01     116   0.10102E-02   0.46690E-01 0.47362E+01 
c  k            0.48741E+03       3   0.15910E-03   0.11776E+00 0.63792E+01 
c  epsilon      0.36774E+04       4   0.92744E-03   0.36026E+02 0.14672E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.331          20.414        0.057007         0.10055
v  Velocity[Y]            -9.6212           9.916          1.0312          1.3113
v  Velocity[Z]            -15.226          15.147      -0.0080175     -0.00087419
v  ǁVelocityǁ           0.0017944          21.173          4.1532          2.6718
v  Pressure               -211.37          64.587          5.5942          12.832
v  k                    5.487e-07          40.202          1.3656         0.72447
v  epsilon             1.0327e-07           17329          38.414          3.8464
v  TurbVisc            1.7834e-07         0.39507        0.048747        0.071168
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              173:        0.11968E+03

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


 INSTANT    0.502500000E+02   TIME STEP NUMBER             174
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.156747696E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152079883E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39814E+00 0.12268E+02
   Friction velocity        uet   :  0.52557E-03 0.68305E+00
   Friction velocity        uk    :  0.47600E-02 0.22410E+01
   Dimensionless distance   yplus :  0.57395E+01 0.27139E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         27
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        720 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10058E+04       4   0.50076E-04   0.51205E+00 0.49795E+01 
c  Velocity[X]                                      0.20257E+00 
c  Velocity[Y]                                      0.15496E+00 
c  Velocity[Z]                                      0.15452E+00 
c  Pressure     0.80803E-01     116   0.99426E-03   0.47424E-01 0.46035E+01 
c  k            0.48877E+03       3   0.15726E-03   0.11632E+00 0.63211E+01 
c  epsilon      0.36636E+04       4   0.94027E-03   0.34716E+02 0.14407E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]             -20.33          20.414        0.057058         0.10071
v  Velocity[Y]            -9.6169           9.913          1.0308          1.3109
v  Velocity[Z]            -15.227          15.147       -0.008063     -0.00087235
v  ǁVelocityǁ           0.0057593          21.173          4.1553          2.6739
v  Pressure               -211.22          64.459           5.677           12.92
v  k                   4.0823e-07          39.313          1.3666         0.72661
v  epsilon             7.6726e-08           16971          38.371          3.8384
v  TurbVisc            1.3239e-07         0.39507        0.048622        0.070872
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              174:        0.11971E+03

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


 INSTANT    0.512500000E+02   TIME STEP NUMBER             175
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.946499194E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080149E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39997E+00 0.12255E+02
   Friction velocity        uet   :  0.53498E-03 0.68219E+00
   Friction velocity        uk    :  0.43655E-02 0.22417E+01
   Dimensionless distance   yplus :  0.55505E+01 0.26810E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         30
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        740 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10048E+04       3   0.50681E-04   0.50619E+00 0.49506E+01 
c  Velocity[X]                                      0.20035E+00 
c  Velocity[Y]                                      0.15322E+00 
c  Velocity[Z]                                      0.15263E+00 
c  Pressure     0.74371E-01     115   0.96793E-03   0.43703E-01 0.44184E+01 
c  k            0.49012E+03       3   0.15565E-03   0.11491E+00 0.62633E+01 
c  epsilon      0.36504E+04       4   0.95485E-03   0.33471E+02 0.14148E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.328          20.413        0.057108         0.10087
v  Velocity[Y]            -9.6126          9.9103          1.0304          1.3105
v  Velocity[Z]            -15.228          15.147      -0.0081081     -0.00086874
v  ǁVelocityǁ           0.0067931          21.174          4.1575          2.6759
v  Pressure               -211.09          64.321          5.7531          13.001
v  k                   3.0956e-07          38.418          1.3675         0.72873
v  epsilon             5.8236e-08           16602           38.33          3.8306
v  TurbVisc            9.8765e-08         0.39508        0.048502        0.070583
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              175:        0.11863E+03

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


 INSTANT    0.522500000E+02   TIME STEP NUMBER             176
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.425756775E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080254E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41500E+00 0.12241E+02
   Friction velocity        uet   :  0.28021E-03 0.68114E+00
   Friction velocity        uk    :  0.38593E-02 0.22423E+01
   Dimensionless distance   yplus :  0.43448E+01 0.26651E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         32
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        760 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10039E+04       3   0.50128E-04   0.50053E+00 0.49224E+01 
c  Velocity[X]                                      0.19819E+00 
c  Velocity[Y]                                      0.15155E+00 
c  Velocity[Z]                                      0.15080E+00 
c  Pressure     0.73642E-01     114   0.96661E-03   0.43327E-01 0.42461E+01 
c  k            0.49148E+03       3   0.15422E-03   0.11353E+00 0.62059E+01 
c  epsilon      0.36377E+04       4   0.96657E-03   0.32283E+02 0.13894E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.327          20.413        0.057159         0.10102
v  Velocity[Y]            -9.6081          9.9172            1.03          1.3101
v  Velocity[Z]            -15.229          15.147      -0.0081524     -0.00086346
v  ǁVelocityǁ           0.0092373          21.175          4.1596          2.6779
v  Pressure               -210.96          64.175          5.8235          13.077
v  k                   2.4001e-07          37.531          1.3685         0.73084
v  epsilon             4.5371e-08           16230          38.293           3.823
v  TurbVisc            6.6189e-08         0.39508        0.048385        0.070299
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              176:        0.11852E+03

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


 INSTANT    0.532500000E+02   TIME STEP NUMBER             177
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.278841792E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080448E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42045E+00 0.12226E+02
   Friction velocity        uet   :  0.22766E-03 0.67993E+00
   Friction velocity        uk    :  0.32944E-02 0.22430E+01
   Dimensionless distance   yplus :  0.36246E+01 0.26583E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         33
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        778 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10030E+04       3   0.49664E-04   0.49500E+00 0.48946E+01 
c  Velocity[X]                                      0.19607E+00 
c  Velocity[Y]                                      0.14992E+00 
c  Velocity[Z]                                      0.14901E+00 
c  Pressure     0.68324E-01     113   0.92012E-03   0.40246E-01 0.40894E+01 
c  k            0.49283E+03       3   0.15273E-03   0.11217E+00 0.61487E+01 
c  epsilon      0.36254E+04       4   0.96817E-03   0.31140E+02 0.13644E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.326          20.412        0.057211         0.10116
v  Velocity[Y]            -9.6037          9.9384          1.0295          1.3096
v  Velocity[Z]             -15.23          15.146      -0.0081953     -0.00085672
v  ǁVelocityǁ            0.012914          21.175          4.1618          2.6799
v  Pressure               -210.84           64.02          5.8883          13.147
v  k                     2.01e-07          36.663          1.3696         0.73293
v  epsilon              3.562e-08           15859          38.258          3.8156
v  TurbVisc            4.2175e-08         0.39509        0.048271        0.070022
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              177:        0.11838E+03

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


 INSTANT    0.542500000E+02   TIME STEP NUMBER             178
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.928114775E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080521E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38667E+00 0.12210E+02
   Friction velocity        uet   :  0.48700E-03 0.67856E+00
   Friction velocity        uk    :  0.28727E-02 0.22437E+01
   Dimensionless distance   yplus :  0.39308E+01 0.26491E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         37
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        790 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10021E+04       3   0.49244E-04   0.48962E+00 0.48671E+01 
c  Velocity[X]                                      0.19399E+00 
c  Velocity[Y]                                      0.14836E+00 
c  Velocity[Z]                                      0.14727E+00 
c  Pressure     0.64787E-01     112   0.89615E-03   0.38208E-01 0.39657E+01 
c  k            0.49418E+03       3   0.15108E-03   0.11083E+00 0.60916E+01 
c  epsilon      0.36137E+04       4   0.96355E-03   0.30040E+02 0.13398E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.325          20.412        0.057265         0.10131
v  Velocity[Y]            -9.5993          9.9574           1.029          1.3092
v  Velocity[Z]            -15.231          15.146      -0.0082369     -0.00084881
v  ǁVelocityǁ            0.012489          21.176          4.1639          2.6819
v  Pressure               -210.72           63.86          5.9499          13.213
v  k                    1.365e-07          35.823          1.3707         0.73501
v  epsilon             2.6806e-08           15495          38.226          3.8083
v  TurbVisc            2.7304e-08         0.39509         0.04816        0.069753
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              178:        0.11849E+03

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


 INSTANT    0.552500000E+02   TIME STEP NUMBER             179
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.219788077E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080821E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36924E+00 0.12193E+02
   Friction velocity        uet   :  0.83506E-03 0.67704E+00
   Friction velocity        uk    :  0.27897E-02 0.22443E+01
   Dimensionless distance   yplus :  0.43490E+01 0.26374E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         37
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        802 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10012E+04       3   0.48794E-04   0.48435E+00 0.48398E+01 
c  Velocity[X]                                      0.19194E+00 
c  Velocity[Y]                                      0.14684E+00 
c  Velocity[Z]                                      0.14557E+00 
c  Pressure     0.62047E-01     109   0.85943E-03   0.36634E-01 0.37975E+01 
c  k            0.49553E+03       3   0.14912E-03   0.10952E+00 0.60347E+01 
c  epsilon      0.36025E+04       4   0.94468E-03   0.28971E+02 0.13157E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.323          20.411        0.057322         0.10145
v  Velocity[Y]            -9.5951          9.9741          1.0285          1.3088
v  Velocity[Z]            -15.232          15.151      -0.0082768     -0.00083997
v  ǁVelocityǁ            0.010775          21.177          4.1661          2.6838
v  Pressure               -210.61          63.689          6.0037          13.272
v  k                   8.8994e-08          35.672          1.3718         0.73708
v  epsilon             2.0235e-08           15141          38.196          3.8013
v  TurbVisc            1.7928e-08          0.3951         0.04805        0.069491
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              179:        0.11765E+03

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


 INSTANT    0.562500000E+02   TIME STEP NUMBER             180
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.160995646E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152080943E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34902E+00 0.12171E+02
   Friction velocity        uet   :  0.33939E-03 0.67539E+00
   Friction velocity        uk    :  0.28683E-02 0.22449E+01
   Dimensionless distance   yplus :  0.47474E+01 0.26230E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         37
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        813 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10003E+04       3   0.48420E-04   0.47921E+00 0.48129E+01 
c  Velocity[X]                                      0.18992E+00 
c  Velocity[Y]                                      0.14537E+00 
c  Velocity[Z]                                      0.14392E+00 
c  Pressure     0.60030E-01     108   0.83451E-03   0.35483E-01 0.36501E+01 
c  k            0.49687E+03       3   0.14714E-03   0.10823E+00 0.59780E+01 
c  epsilon      0.35918E+04       4   0.91798E-03   0.27982E+02 0.12929E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.322          20.411        0.057381         0.10159
v  Velocity[Y]             -9.591          9.9884          1.0279          1.3083
v  Velocity[Z]            -15.232          15.156      -0.0083148     -0.00083022
v  ǁVelocityǁ           0.0094506          21.178          4.1682          2.6858
v  Pressure               -210.52          63.508          6.0508          13.325
v  k                   5.8477e-08          35.681           1.373         0.73913
v  epsilon             1.5314e-08           14800          38.169          3.7944
v  TurbVisc            1.1905e-08          0.3951        0.047943        0.069237
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              180:        0.11742E+03

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


 INSTANT    0.572500000E+02   TIME STEP NUMBER             181
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.499157076E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152081092E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32733E+00 0.12148E+02
   Friction velocity        uet   :  0.80909E-03 0.67363E+00
   Friction velocity        uk    :  0.29095E-02 0.22455E+01
   Dimensionless distance   yplus :  0.49226E+01 0.26093E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         40
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        816 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99941E+03       3   0.48061E-04   0.47419E+00 0.47862E+01 
c  Velocity[X]                                      0.18794E+00 
c  Velocity[Y]                                      0.14395E+00 
c  Velocity[Z]                                      0.14230E+00 
c  Pressure     0.57613E-01     107   0.81595E-03   0.34092E-01 0.35594E+01 
c  k            0.49821E+03       3   0.14526E-03   0.10695E+00 0.59215E+01 
c  epsilon      0.35816E+04       4   0.90102E-03   0.27105E+02 0.12715E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.321           20.41        0.057445         0.10172
v  Velocity[Y]            -9.5872          10.001          1.0273          1.3079
v  Velocity[Z]            -15.233          15.161      -0.0083511     -0.00081991
v  ǁVelocityǁ           0.0086549          21.179          4.1704          2.6877
v  Pressure               -210.42          63.324          6.0957          13.374
v  k                   3.8651e-08          35.703          1.3742         0.74117
v  epsilon             1.1616e-08           14475          38.145          3.7877
v  TurbVisc            7.9747e-09         0.39511        0.047837         0.06899
v  total_pressure      1.0122e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              181:        0.11905E+03

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


 INSTANT    0.582500000E+02   TIME STEP NUMBER             182
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.550206540E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152081404E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30587E+00 0.12126E+02
   Friction velocity        uet   :  0.82433E-03 0.67177E+00
   Friction velocity        uk    :  0.29967E-02 0.22460E+01
   Dimensionless distance   yplus :  0.49107E+01 0.26195E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         42
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        821 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99855E+03       3   0.47717E-04   0.46927E+00 0.47597E+01 
c  Velocity[X]                                      0.18598E+00 
c  Velocity[Y]                                      0.14256E+00 
c  Velocity[Z]                                      0.14073E+00 
c  Pressure     0.56317E-01     107   0.79452E-03   0.33358E-01 0.34283E+01 
c  k            0.49955E+03       3   0.14353E-03   0.10570E+00 0.58651E+01 
c  epsilon      0.35718E+04       4   0.94091E-03   0.26513E+02 0.12522E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]             -20.32           20.41        0.057511         0.10185
v  Velocity[Y]            -9.5836           10.01          1.0267          1.3074
v  Velocity[Z]            -15.233          15.166      -0.0083859      -0.0008095
v  ǁVelocityǁ           0.0084906           21.18          4.1726          2.6896
v  Pressure               -210.33           63.13          6.1338          13.417
v  k                   2.5671e-08          35.739          1.3754          0.7432
v  epsilon             8.8289e-09           14166          38.122          3.7812
v  TurbVisc            5.3777e-09         0.39512        0.047733        0.068748
v  total_pressure      1.0123e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              182:        0.11892E+03

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


 INSTANT    0.592500000E+02   TIME STEP NUMBER             183
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.609993752E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152081597E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           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+00 0.12104E+02
   Friction velocity        uet   :  0.77981E-03 0.66985E+00
   Friction velocity        uk    :  0.33463E-02 0.22465E+01
   Dimensionless distance   yplus :  0.50340E+01 0.26313E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         42
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        822 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99770E+03       3   0.47401E-04   0.46447E+00 0.47334E+01 
c  Velocity[X]                                      0.18406E+00 
c  Velocity[Y]                                      0.14122E+00 
c  Velocity[Z]                                      0.13919E+00 
c  Pressure     0.54097E-01     107   0.77915E-03   0.32072E-01 0.33144E+01 
c  k            0.50088E+03       3   0.14190E-03   0.10448E+00 0.58089E+01 
c  epsilon      0.35623E+04       4   0.10327E-02   0.26187E+02 0.12345E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.319          20.409        0.057581         0.10199
v  Velocity[Y]            -9.5803          10.018          1.0261          1.3069
v  Velocity[Z]            -15.233          15.172      -0.0084193     -0.00079933
v  ǁVelocityǁ           0.0089198          21.181          4.1747          2.6915
v  Pressure               -210.25          62.928          6.1652          13.454
v  k                   1.7133e-08          35.785          1.3767         0.74522
v  epsilon             6.7282e-09           13874          38.102          3.7749
v  TurbVisc            3.6467e-09         0.39512        0.047632        0.068512
v  total_pressure      1.0123e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              183:        0.11886E+03

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


 INSTANT    0.602500000E+02   TIME STEP NUMBER             184
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.128503374E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152081842E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26390E+00 0.12084E+02
   Friction velocity        uet   :  0.59538E-03 0.66825E+00
   Friction velocity        uk    :  0.34391E-02 0.22470E+01
   Dimensionless distance   yplus :  0.51990E+01 0.26443E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         44
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        819 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99686E+03       3   0.47101E-04   0.45977E+00 0.47073E+01 
c  Velocity[X]                                      0.18216E+00 
c  Velocity[Y]                                      0.13992E+00 
c  Velocity[Z]                                      0.13769E+00 
c  Pressure     0.53062E-01     104   0.76199E-03   0.31486E-01 0.32287E+01 
c  k            0.50222E+03       3   0.14026E-03   0.10327E+00 0.57528E+01 
c  epsilon      0.35533E+04       4   0.11028E-02   0.25759E+02 0.12152E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.319          20.409        0.057655         0.10211
v  Velocity[Y]            -9.5773          10.023          1.0254          1.3065
v  Velocity[Z]            -15.234          15.177      -0.0084515     -0.00078987
v  ǁVelocityǁ           0.0098375          21.182          4.1769          2.6933
v  Pressure               -210.18          62.722          6.1932          13.487
v  k                   1.1496e-08          35.841           1.378         0.74723
v  epsilon             5.1471e-09           13598          38.083          3.7688
v  TurbVisc            2.4866e-09         0.39513        0.047532        0.068281
v  total_pressure      1.0123e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              184:        0.11920E+03

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


 INSTANT    0.612500000E+02   TIME STEP NUMBER             185
 ============================================================= 



 Options set or changed by "control_file":
 -----------------------------------------

  max_time_step                             185 (current: 185)

 Finished reading "control_file".



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.184804698E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152081953E+03
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26838E+00 0.12065E+02
   Friction velocity        uet   :  0.23767E-03 0.66871E+00
   Friction velocity        uk    :  0.33137E-02 0.22826E+01
   Dimensionless distance   yplus :  0.53368E+01 0.26580E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :         46
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        819 outlet faces on       9303


 Write final restart files
   checkpoint at iteration        185, Physical time    0.61250E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
  Wrote field names and types to checkpoint: checkpoint/main
   End writing the options                              
  Wrote main variables to checkpoint: checkpoint/main
 End writing

   ** Writing the auxiliary restart file
      ----------------------------------

 Start writing
   End writing the dimensions and options               
   End writing the physical properties                  
   End writing the time step                            
  Wrote boundary condition coefficients to checkpoint: checkpoint/auxiliary
 End writing


 Time for restart files:    0.94470E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.99603E+03       3   0.46777E-04   0.45516E+00 0.46814E+01 
c  Velocity[X]                                      0.18029E+00 
c  Velocity[Y]                                      0.13866E+00 
c  Velocity[Z]                                      0.13622E+00 
c  Pressure     0.52357E-01     102   0.74553E-03   0.31093E-01 0.31496E+01 
c  k            0.50355E+03       3   0.13859E-03   0.10207E+00 0.56970E+01 
c  epsilon      0.35447E+04       4   0.11136E-02   0.24999E+02 0.11925E+02 
-----------------------------------------------------------------------------
  
  

  ** 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]            -20.318          20.408        0.057733         0.10224
v  Velocity[Y]            -9.5747          10.026          1.0247           1.306
v  Velocity[Z]            -15.234          15.183      -0.0084821     -0.00078064
v  ǁVelocityǁ            0.011053          21.184          4.1791          2.6952
v  Pressure               -210.11           62.51          6.2175          13.516
v  k                   7.7607e-09          35.906          1.3793         0.74923
v  epsilon             3.9615e-09           13340          38.067          3.7628
v  TurbVisc            1.7059e-09         0.39514        0.047436        0.068055
v  total_pressure      1.0123e+05      1.0158e+05      1.0143e+05      1.0141e+05


 TIME FOR THE TIME STEP              185:        0.12036E+03

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



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



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


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




   ** TIME FOR FINAL WRITING:    0.44070E-02
      -----------------------                                



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




                      END OF CALCULATION                     
                      ==================                     


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           7429.100 s
  System CPU time:          228.642 s
  Total CPU time:         30613.020 s

  Elapsed time:            7721.749 s
  CPU / elapsed time          0.992

Memory use summary:

  Total memory used:                               8.532 GiB
                             local minimum:        2.109 GiB  (rank 3)
                             local maximum:        2.146 GiB  (rank 1)
  Theoretical instrumented dynamic memory:         5.344 GiB
                             local minimum:        1.330 GiB  (rank 0)
                             local maximum:        1.341 GiB  (rank 1)
