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:                Sat 13 Jun 2015 04:31:45 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/20150613-1631
  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         )
       RELAXV =    0.10000E+01 for k        (Relaxation)
       RELAXV =    0.10000E+01 for epsilon  (Relaxation)

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

 --- Constants

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

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


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

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

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

       RELAXV =    0.10000E+01 for pressure (relaxation)
       ARAK   =    0.10000E+01 (Arakawa factor              )

       ISTMPF =              1 (time scheme for flow
                               (0: explicit (THETFL = 0     )
                               (1: std scheme (Saturne 1.0  )
                               (2: 2nd-order (THETFL = 0.5  )
       THETFL =   -0.99900E+03 (theta for mass flow         )
       IROEXT =              0 (density extrapolation
                               (0: explicit
                               (1: n+thetro with thetro=1/2
                               (2: n+thetro with thetro=1
       THETRO =    0.00000E+00 (theta for density
                               ((1+theta).new-theta.old
       IVIEXT =              0 (total viscosity extrapolation
                               (0: explicit
                               (1: n+thetvi with thetro=1/2
                               (2: n+thetvi with thetro=1
       THETVI =    0.00000E+00 (theta for total viscosity
                               ((1+theta).new-theta.old
       ICPEXT =              0 (specific heat extrapolation
                               (0: explicit
                               (1: n+thetcp with thetro=1/2
                               (2: n+thetcp with thetro=1
       THETCP =    0.00000E+00 (specific heat theta-scheme
                               ((1+theta).new-theta.old
       THETSN =    0.00000E+00 (Nav-Stokes S.T. theta scheme)
                               ((1+theta).new-theta.old
       THETST =    0.00000E+00 (Turbulence S.T. theta-scheme)
                               ((1+theta).new-theta.old
       EPSUP  =    0.10000E-04 (Velocity/pressure coupling
                                stop test                   )


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


 ** GRADIENTS CALCULATION
    ---------------------

       IMRGRA =              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-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-06  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

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

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


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


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


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


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

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

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


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


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

 --- Restarted calculation
       ISUITE =              0 (1: restarted calculation    )
       ILEAUX =              1 (1: read  restart/auxiliary  )
       IECAUX =              1 (1: write checkpoint/auxiliary)


 --- Calculation time
     The numbering of time steps and the measure of simulated
       physical time are absolute values, and not values
       relative to the current calculation.

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =           1000 (Final time step required    )

 --- CPU time margin
       TMARUS =   -0.10000E+01 (CPU time margin before stop )


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


 ** INPUT-OUTPUT
    ------------

 --- Restart file
       NTSUIT =              0 (Checkpoint frequency )

 --- Post-processed variables


Velocity
Pressure
k
epsilon
TurbVisc
CourantNb
FourierNb
total_pressure
         --           --

 --- 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
        11 CourantNb                     -1
        12 FourierNb                     -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
        11 CourantNb                   -999
        12 FourierNb                   -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
 No "partition_input/domain_number_4" file available;

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

 Partitioning by space-filling curve: Morton (in bounding box).
  Number of cells per domain (histogramm):
    [    1389251 ;    1389251 ] =          4

 Partitioning finished (29.4 s)


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

 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 (3.77 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.

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


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

 -----------------------------------------
  Variable          Min. value  Max. value
 -----------------------------------------                   
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  epsilon           0.1142E-06  0.1142E-06
 ---------------------------------

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



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.3343E+00  0.3343E+00
 -----------------------------------------



   ** 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 faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.80870E+00   0.20650E+02  -0.91539E-02



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

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


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.00000E+00 0.00000E+00
   Friction velocity        uet   :  0.00000E+00 0.00000E+00
   Friction velocity        uk    :  0.84565E-02 0.13416E-01
   Dimensionless distance   yplus :  0.19228E+01 0.68621E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :         38
   Total number of wall faces                   :     141685
------------------------------------------------------------


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


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.50509E+02    1152   0.29845E+00   0.29711E+03 0.10000E+03 
c  Velocity[X]                                      0.64422E+02 
c  Velocity[Y]                                      0.21475E+03 
c  Velocity[Z]                                      0.17935E+02 
c  Pressure     0.52312E+00    1800   0.20806E+01   0.98095E+00 0.10000E+03 
c  k            0.10698E+02     975   0.17431E+00   0.20977E+00 0.99940E+02 
c  epsilon      0.60380E+03     858   0.15373E+00   0.12662E+04 0.10000E+03 
-----------------------------------------------------------------------------
  
  

  ** 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]            -41.429          39.761         0.04959        0.095146
v  Velocity[Y]            -23.979          26.697           1.018           1.113
v  Velocity[Z]            -22.711          25.309       0.0052483      2.7639e-05
v  ǁVelocityǁ          1.4767e-06          46.073          2.8523          1.3287
v  Pressure               0.27696          4583.4          2589.3            1943
v  k                   0.00033043          3.0078         0.10654       0.0024144
v  epsilon             1.1422e-07          201.08          8.8072         0.16032
v  TurbVisc               0.33434         0.33434         0.33434         0.33434
v  CourantNb                    0               0               0               0
v  FourierNb               1.5251          305.73          23.729          5.4935
v  total_pressure      1.0121e+05      1.0607e+05      1.0401e+05      1.0334e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.5251          305.73          23.729          5.4935


 TIME FOR THE TIME STEP                1:        0.13010E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.232676885E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083842E+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 : -0.11006E+03 0.71259E+01
   Friction velocity        uet   :  0.53444E-05 0.25038E+01
   Friction velocity        uk    :  0.86812E-02 0.68000E+00
   Dimensionless distance   yplus :  0.38336E+01 0.54323E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      63733
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17029E+03     163   0.64079E-01   0.27602E+01 0.95205E+01 
c  Velocity[X]                                      0.11704E+01 
c  Velocity[Y]                                      0.48109E+00 
c  Velocity[Z]                                      0.11087E+01 
c  Pressure     0.13951E+01    1205   0.81731E-01   0.11544E+01 0.10000E+03 
c  k            0.42256E+01      79   0.13692E-02   0.52126E-01 0.34523E+02 
c  epsilon      0.29939E+03      61   0.90951E-03   0.12642E+03 0.28134E+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]             -28.06          26.507        0.050307        0.096148
v  Velocity[Y]            -15.595          17.653          1.0076          1.1219
v  Velocity[Z]             -22.08          22.337       0.0047002     -3.2229e-05
v  ǁVelocityǁ           1.459e-05          31.866          2.9087          1.3402
v  Pressure               -149.04          44.627          15.594            20.7
v  k                   2.5313e-05          3.7149         0.15601       0.0032152
v  epsilon             1.1363e-07          279.12          8.9955         0.14941
v  TurbVisc            1.9023e-08         0.33434         0.15571         0.24422
v  CourantNb                    0          57.848          2.2052         0.37495
v  FourierNb           0.00028204          66.319          2.7626          3.3564
v  total_pressure      1.0121e+05       1.016e+05      1.0144e+05      1.0142e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036463           66.64          4.9678          3.7314


 TIME FOR THE TIME STEP                2:        0.50971E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.501684282E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083840E+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 : -0.97001E+02 0.10058E+02
   Friction velocity        uet   :  0.40321E-05 0.16044E+01
   Friction velocity        uk    :  0.46638E-02 0.98489E+00
   Dimensionless distance   yplus :  0.33670E+01 0.79657E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      54762
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17278E+03     179   0.35819E-01   0.22938E+01 0.85775E+01 
c  Velocity[X]                                      0.95118E+00 
c  Velocity[Y]                                      0.46771E+00 
c  Velocity[Z]                                      0.87494E+00 
c  Pressure     0.11708E+01    1136   0.24257E-01   0.68202E+00 0.13739E+03 
c  k            0.42223E+01      74   0.12672E-02   0.59795E-01 0.29471E+02 
c  epsilon      0.29343E+03      67   0.10524E-02   0.12395E+03 0.23669E+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]            -22.583          22.152        0.051124        0.096686
v  Velocity[Y]             -13.99          14.224         0.99301          1.1244
v  Velocity[Z]            -18.963          17.728       0.0044572     -4.6473e-05
v  ǁVelocityǁ          1.3257e-05          24.515          3.0302          1.3464
v  Pressure               -228.02          19.902          -1.715          8.0774
v  k                   2.4275e-06          4.5959         0.20946       0.0044364
v  epsilon             1.1412e-07          381.02          11.198         0.19185
v  TurbVisc            1.3669e-09         0.36518         0.15349         0.24135
v  CourantNb                    0          54.996          2.2273          0.3759
v  FourierNb           0.00027834          59.964          2.7528          3.3115
v  total_pressure      1.0121e+05      1.0158e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036424          60.287            4.98          3.6874


 TIME FOR THE TIME STEP                3:        0.50098E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.754174852E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083853E+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 : -0.11714E+03 0.11623E+02
   Friction velocity        uet   :  0.62914E-05 0.10268E+01
   Friction velocity        uk    :  0.20207E-02 0.10708E+01
   Dimensionless distance   yplus :  0.15797E+01 0.81799E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      42680
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step          4
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            


   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17201E+03     158   0.26980E-01   0.20367E+01 0.79831E+01 
c  Velocity[X]                                      0.88437E+00 
c  Velocity[Y]                                      0.39585E+00 
c  Velocity[Z]                                      0.75650E+00 
c  Pressure     0.10361E+01     974   0.21156E-01   0.55726E+00 0.29059E+02 
c  k            0.42117E+01      80   0.14924E-02   0.54677E-01 0.24660E+02 
c  epsilon      0.29022E+03      74   0.99891E-03   0.10874E+03 0.20418E+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]            -22.284          22.301        0.051922        0.097114
v  Velocity[Y]            -14.241          13.071          0.9794          1.1268
v  Velocity[Z]            -17.082          17.017       0.0035539     -4.6902e-05
v  ǁVelocityǁ          3.4646e-05          22.888          3.1237          1.3524
v  Pressure               -237.66          17.798         -5.9009          5.5831
v  k                    1.264e-06          5.5452         0.24686       0.0057225
v  epsilon             1.1426e-07          565.68          12.762         0.23647
v  TurbVisc            1.9377e-10         0.37127         0.15153         0.23879
v  CourantNb                    0          57.418          2.3656         0.37915
v  FourierNb           0.00027565          56.869          2.7422          3.2717
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036386          61.353          5.1078          3.6508


 TIME FOR THE TIME STEP                4:        0.45369E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.162347059E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083854E+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 : -0.64903E+02 0.11703E+02
   Friction velocity        uet   :  0.84705E-05 0.97830E+00
   Friction velocity        uk    :  0.38992E-02 0.12488E+01
   Dimensionless distance   yplus :  0.25082E+01 0.98905E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      34151
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17219E+03     157   0.27272E-01   0.16275E+01 0.70542E+01 
c  Velocity[X]                                      0.73682E+00 
c  Velocity[Y]                                      0.29201E+00 
c  Velocity[Z]                                      0.59866E+00 
c  Pressure     0.89917E+00     938   0.22748E-01   0.48416E+00 0.22002E+02 
c  k            0.43137E+01      84   0.22349E-02   0.54223E-01 0.21620E+02 
c  epsilon      0.29424E+03      76   0.15136E-02   0.14243E+03 0.21119E+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]            -22.753          22.906        0.052861        0.097506
v  Velocity[Y]            -12.588          11.952         0.96855           1.129
v  Velocity[Z]            -17.955          17.908       0.0030041      -4.291e-05
v  ǁVelocityǁ          2.5657e-05          24.712          3.1879          1.3584
v  Pressure               -215.71          17.531         -9.1085          3.9192
v  k                    1.294e-06          8.0279         0.27954       0.0070884
v  epsilon             1.1428e-07          816.74          14.202          0.2846
v  TurbVisc            5.6277e-10         0.37212         0.14975         0.23648
v  CourantNb                    0          59.072          2.4694         0.38234
v  FourierNb           0.00027689          55.704          2.7214          3.2357
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0003635          62.483          5.1908           3.618


 TIME FOR THE TIME STEP                5:        0.44506E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.163813925E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083854E+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 : -0.69798E+02 0.10906E+02
   Friction velocity        uet   :  0.70284E-05 0.89254E+00
   Friction velocity        uk    :  0.39385E-02 0.14675E+01
   Dimensionless distance   yplus :  0.24584E+01 0.11819E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      31101
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17248E+03     156   0.26054E-01   0.13771E+01 0.64124E+01 
c  Velocity[X]                                      0.62569E+00 
c  Velocity[Y]                                      0.24076E+00 
c  Velocity[Z]                                      0.51065E+00 
c  Pressure     0.73170E+00     918   0.19407E-01   0.40097E+00 0.17703E+02 
c  k            0.46413E+01      88   0.29786E-02   0.58690E-01 0.19481E+02 
c  epsilon      0.32120E+03      76   0.25043E-02   0.24401E+03 0.23484E+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]            -23.666          24.595         0.05396         0.09787
v  Velocity[Y]            -10.368          13.629         0.96014          1.1313
v  Velocity[Z]            -19.548          17.917       0.0028577     -3.9378e-05
v  ǁVelocityǁ          4.4454e-05          25.359          3.2491           1.365
v  Pressure               -209.63          18.381         -11.593          2.6729
v  k                   1.0429e-06          13.961         0.31796       0.0086358
v  epsilon              1.143e-07          1603.9          16.179         0.34497
v  TurbVisc            1.3562e-09         0.37279         0.14811         0.23434
v  CourantNb                    0          62.949           2.534         0.38522
v  FourierNb           0.00032355          54.402          2.6995          3.2025
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036313          65.643          5.2336          3.5877


 TIME FOR THE TIME STEP                6:        0.43831E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.100494773E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083854E+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 : -0.62950E+02 0.10378E+02
   Friction velocity        uet   :  0.45019E-05 0.78317E+00
   Friction velocity        uk    :  0.38206E-02 0.18554E+01
   Dimensionless distance   yplus :  0.19753E+01 0.14619E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      30184
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17282E+03     154   0.24511E-01   0.12802E+01 0.61057E+01 
c  Velocity[X]                                      0.57497E+00 
c  Velocity[Y]                                      0.23531E+00 
c  Velocity[Z]                                      0.46997E+00 
c  Pressure     0.58943E+00     898   0.15845E-01   0.32614E+00 0.13233E+02 
c  k            0.50818E+01      92   0.37389E-02   0.65617E-01 0.17893E+02 
c  epsilon      0.37424E+03      79   0.40355E-02   0.42540E+03 0.25606E+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]            -23.888          24.103        0.055051        0.098214
v  Velocity[Y]            -10.299          11.132          0.9543          1.1335
v  Velocity[Z]            -18.353          18.587       0.0026204     -3.8236e-05
v  ǁVelocityǁ          4.7999e-05            25.2          3.3097          1.3722
v  Pressure                -199.8          19.349          -13.49          1.8258
v  k                   9.4842e-07          19.921         0.36004        0.010333
v  epsilon             1.1432e-07          3573.3          18.478         0.41453
v  TurbVisc            1.4128e-09         0.37306         0.14659         0.23233
v  CourantNb                    0          63.801          2.5935         0.38835
v  FourierNb           0.00032731          53.034          2.6831          3.1716
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036277           66.41          5.2766          3.5599


 TIME FOR THE TIME STEP                7:        0.43335E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.524047504E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083852E+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 : -0.50649E+02 0.98449E+01
   Friction velocity        uet   :  0.12598E-04 0.77709E+00
   Friction velocity        uk    :  0.38211E-02 0.23001E+01
   Dimensionless distance   yplus :  0.16512E+01 0.18474E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      29247
   Nb of faces within the viscous sub-layer     :          5
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for          4 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17325E+03     153   0.23659E-01   0.12684E+01 0.59984E+01 
c  Velocity[X]                                      0.56443E+00 
c  Velocity[Y]                                      0.24878E+00 
c  Velocity[Z]                                      0.45522E+00 
c  Pressure     0.49182E+00     860   0.13502E-01   0.27272E+00 0.10599E+02 
c  k            0.55879E+01      96   0.40721E-02   0.70890E-01 0.16338E+02 
c  epsilon      0.47629E+03      80   0.55256E-02   0.65528E+03 0.26098E+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]            -23.524          24.018        0.055983        0.098536
v  Velocity[Y]            -9.9909          10.892         0.95147          1.1357
v  Velocity[Z]            -18.907          18.347       0.0024363     -3.5176e-05
v  ǁVelocityǁ          7.1144e-05          25.615          3.3672          1.3801
v  Pressure               -190.52          20.289          -14.93          1.2202
v  k                   9.5247e-07          29.202         0.40306        0.012147
v  epsilon             1.1434e-07          9237.4           20.86         0.48938
v  TurbVisc            1.7192e-09         0.37322         0.14518         0.23042
v  CourantNb           2.5756e-17          63.917          2.6479         0.39174
v  FourierNb           0.00032298          51.635          2.6714          3.1424
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036242          67.052          5.3193          3.5342


 TIME FOR THE TIME STEP                8:        0.42340E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.459011166E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083851E+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 : -0.44400E+02 0.94250E+01
   Friction velocity        uet   :  0.11883E-04 0.80824E+00
   Friction velocity        uk    :  0.24804E-02 0.29598E+01
   Dimensionless distance   yplus :  0.18629E+01 0.22134E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      28317
   Nb of faces within the viscous sub-layer     :          6
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for          5 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17377E+03     152   0.22766E-01   0.12977E+01 0.59865E+01 
c  Velocity[X]                                      0.57285E+00 
c  Velocity[Y]                                      0.27084E+00 
c  Velocity[Z]                                      0.45400E+00 
c  Pressure     0.43621E+00     811   0.12155E-01   0.24107E+00 0.86691E+01 
c  k            0.61376E+01     100   0.37383E-02   0.76391E-01 0.15073E+02 
c  epsilon      0.62870E+03      80   0.52582E-02   0.67287E+03 0.22547E+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]            -23.082          23.551        0.056807        0.098842
v  Velocity[Y]            -10.728          11.225          0.9515          1.1379
v  Velocity[Z]            -19.402          18.442       0.0022745     -3.4148e-05
v  ǁVelocityǁ          4.6865e-05          25.475          3.4192          1.3886
v  Pressure               -187.59          21.561         -15.924         0.82065
v  k                    1.178e-06          39.216         0.44665        0.014073
v  epsilon             1.1436e-07           14505          23.178         0.56618
v  TurbVisc            2.6043e-09         0.37353         0.14384          0.2286
v  CourantNb                    0          65.914           2.695         0.39532
v  FourierNb           0.00031999          50.238          2.6632          3.1147
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036207          69.223          5.3582            3.51


 TIME FOR THE TIME STEP                9:        0.41168E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.609654537E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083854E+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 : -0.42837E+02 0.95977E+01
   Friction velocity        uet   :  0.12305E-04 0.80184E+00
   Friction velocity        uk    :  0.35746E-02 0.34300E+01
   Dimensionless distance   yplus :  0.15961E+01 0.27222E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      27428
   Nb of faces within the viscous sub-layer     :         12
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         19 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17437E+03     150   0.22874E-01   0.13514E+01 0.60273E+01 
c  Velocity[X]                                      0.59128E+00 
c  Velocity[Y]                                      0.29743E+00 
c  Velocity[Z]                                      0.46268E+00 
c  Pressure     0.40552E+00     773   0.11534E-01   0.22284E+00 0.78857E+01 
c  k            0.67061E+01     104   0.33933E-02   0.86011E-01 0.14326E+02 
c  epsilon      0.75295E+03      81   0.40862E-02   0.56583E+03 0.18811E+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]            -23.059          23.596        0.057479        0.099129
v  Velocity[Y]            -11.208          11.711         0.95368          1.1401
v  Velocity[Z]            -18.859          18.695       0.0021339      -3.112e-05
v  ǁVelocityǁ          4.8491e-05          25.161          3.4645          1.3975
v  Pressure               -191.03          22.613         -16.593         0.52166
v  k                   1.4864e-06          42.371         0.49148        0.016126
v  epsilon             1.1439e-07           18539          25.376         0.64323
v  TurbVisc            6.4317e-09         0.37356         0.14258         0.22685
v  CourantNb                    0          67.916          2.7335         0.39902
v  FourierNb           0.00033138           48.86          2.6586          3.0882
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036172          71.346          5.3921          3.4872


 TIME FOR THE TIME STEP               10:        0.40084E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.129595758E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083852E+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 : -0.41706E+02 0.10150E+02
   Friction velocity        uet   :  0.11735E-04 0.81270E+00
   Friction velocity        uk    :  0.23614E-02 0.35653E+01
   Dimensionless distance   yplus :  0.16056E+01 0.26846E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      26543
   Nb of faces within the viscous sub-layer     :         10
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         34 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17507E+03     148   0.23540E-01   0.14233E+01 0.61030E+01 
c  Velocity[X]                                      0.61561E+00 
c  Velocity[Y]                                      0.32682E+00 
c  Velocity[Z]                                      0.48082E+00 
c  Pressure     0.38978E+00     702   0.11320E-01   0.21205E+00 0.73148E+01 
c  k            0.73290E+01     108   0.35245E-02   0.99132E-01 0.13827E+02 
c  epsilon      0.78235E+03      83   0.36731E-02   0.61268E+03 0.18458E+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]            -23.127          22.825        0.057929        0.099394
v  Velocity[Y]            -11.258          12.275         0.95707          1.1422
v  Velocity[Z]            -18.771           18.55       0.0018776     -2.5572e-05
v  ǁVelocityǁ           7.228e-05          24.964          3.5024          1.4069
v  Pressure               -195.86          23.696         -16.941         0.33854
v  k                   1.6851e-06          36.176          0.5381        0.018328
v  epsilon             1.1442e-07           18388          27.511         0.72175
v  TurbVisc            8.5405e-09         0.37368         0.14138         0.22516
v  CourantNb                    0          69.978          2.7635         0.40277
v  FourierNb           0.00034214          47.508           2.658          3.0628
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036137          73.471          5.4215          3.4655


 TIME FOR THE TIME STEP               11:        0.38161E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.799938813E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083853E+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 : -0.40424E+02 0.10603E+02
   Friction velocity        uet   :  0.44738E-05 0.79649E+00
   Friction velocity        uk    :  0.27855E-02 0.32944E+01
   Dimensionless distance   yplus :  0.13605E+01 0.22810E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      25490
   Nb of faces within the viscous sub-layer     :         10
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         64 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17585E+03     146   0.24126E-01   0.15043E+01 0.61919E+01 
c  Velocity[X]                                      0.64387E+00 
c  Velocity[Y]                                      0.35672E+00 
c  Velocity[Z]                                      0.50376E+00 
c  Pressure     0.38621E+00     666   0.11345E-01   0.20788E+00 0.71089E+01 
c  k            0.80581E+01     112   0.56035E-02   0.11397E+00 0.13353E+02 
c  epsilon      0.80109E+03      85   0.36787E-02   0.57285E+03 0.16714E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -2.4156                             2


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.795          22.502        0.058036        0.099636
v  Velocity[Y]            -11.563          11.849         0.96045          1.1444
v  Velocity[Z]            -19.245          18.199       0.0016332      -2.011e-05
v  ǁVelocityǁ          0.00012742          24.809          3.5331          1.4166
v  Pressure               -197.33           24.58         -17.002         0.25263
v  k                   2.2397e-06          39.264         0.58653        0.020695
v  epsilon             1.1444e-07           17488          29.663         0.80379
v  TurbVisc            1.1356e-08         0.37746         0.14022         0.22351
v  CourantNb                    0          71.586          2.7851         0.40653
v  FourierNb           0.00033928           80.42          2.6612          3.0381
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036103          82.877          5.4463          3.4446


 TIME FOR THE TIME STEP               12:        0.37196E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.610623359E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083852E+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 : -0.38836E+02 0.10992E+02
   Friction velocity        uet   :  0.97144E-05 0.80021E+00
   Friction velocity        uk    :  0.29739E-02 0.34321E+01
   Dimensionless distance   yplus :  0.15248E+01 0.24234E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      24554
   Nb of faces within the viscous sub-layer     :         12
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         91 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17673E+03     144   0.25138E-01   0.15802E+01 0.62640E+01 
c  Velocity[X]                                      0.67002E+00 
c  Velocity[Y]                                      0.38555E+00 
c  Velocity[Z]                                      0.52460E+00 
c  Pressure     0.38793E+00     554   0.11383E-01   0.20635E+00 0.71490E+01 
c  k            0.88891E+01     117   0.39331E-02   0.13095E+00 0.12926E+02 
c  epsilon      0.81693E+03      87   0.40428E-02   0.52040E+03 0.14845E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -47.981                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.462           22.62        0.057924        0.099856
v  Velocity[Y]            -11.454          11.844         0.96274          1.1465
v  Velocity[Z]            -18.657          18.257       0.0013284     -1.3023e-05
v  ǁVelocityǁ          0.00012863          24.787          3.5571          1.4267
v  Pressure               -197.21           25.19          -16.87         0.21235
v  k                   2.5251e-06          42.677         0.63606        0.023232
v  epsilon             1.1447e-07           17290          31.852         0.88982
v  TurbVisc            1.7687e-08         0.40278          0.1391         0.22189
v  CourantNb                    0          72.579          2.7993         0.41026
v  FourierNb           0.00033761          54.237          2.6673          3.0139
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036069          76.198          5.4665          3.4241


 TIME FOR THE TIME STEP               13:        0.34078E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.548277742E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083846E+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 : -0.35999E+02 0.11146E+02
   Friction velocity        uet   :  0.84297E-05 0.74130E+00
   Friction velocity        uk    :  0.30079E-02 0.35633E+01
   Dimensionless distance   yplus :  0.13246E+01 0.25490E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      23617
   Nb of faces within the viscous sub-layer     :         18
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        114 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17771E+03     142   0.26186E-01   0.16433E+01 0.63072E+01 
c  Velocity[X]                                      0.69043E+00 
c  Velocity[Y]                                      0.41163E+00 
c  Velocity[Z]                                      0.54126E+00 
c  Pressure     0.39583E+00     559   0.11409E-01   0.20751E+00 0.72691E+01 
c  k            0.98151E+01     122   0.38652E-02   0.14806E+00 0.12460E+02 
c  epsilon      0.86192E+03      89   0.30460E-02   0.50124E+03 0.13526E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -7.7247e-05                             1
a  epsilon          -6.032                             3


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.901          22.335         0.05776         0.10006
v  Velocity[Y]            -11.453          11.931         0.96343          1.1486
v  Velocity[Z]            -18.834          18.183      0.00092801     -8.3305e-06
v  ǁVelocityǁ          0.00013015          24.881          3.5752           1.437
v  Pressure               -195.43          25.635          -16.55         0.22363
v  k                   2.3247e-06          49.786         0.68567        0.025935
v  epsilon              1.145e-07           21702          34.065         0.97964
v  TurbVisc            2.1343e-08          0.3747         0.13799         0.22028
v  CourantNb                    0          72.965          2.8067         0.41392
v  FourierNb           0.00033661          43.654          2.6749            2.99
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036036           76.68          5.4816          3.4039


 TIME FOR THE TIME STEP               14:        0.34036E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.495472360E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083836E+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 : -0.33312E+02 0.11333E+02
   Friction velocity        uet   :  0.72300E-05 0.69918E+00
   Friction velocity        uk    :  0.25023E-02 0.36966E+01
   Dimensionless distance   yplus :  0.12904E+01 0.26570E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      22644
   Nb of faces within the viscous sub-layer     :         21
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        125 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17879E+03     141   0.27109E-01   0.16904E+01 0.63181E+01 
c  Velocity[X]                                      0.70317E+00 
c  Velocity[Y]                                      0.43425E+00 
c  Velocity[Z]                                      0.55302E+00 
c  Pressure     0.40304E+00     680   0.11375E-01   0.20842E+00 0.74414E+01 
c  k            0.10825E+02     127   0.40198E-02   0.16372E+00 0.11942E+02 
c  epsilon      0.92079E+03      91   0.29493E-02   0.49549E+03 0.12518E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -9.4047e-05                             2
a  epsilon         -5.4357                             4


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.58           22.24         0.05763         0.10024
v  Velocity[Y]            -11.467          11.978         0.96269          1.1507
v  Velocity[Z]            -18.703          18.265      0.00043003     -2.8211e-06
v  ǁVelocityǁ          0.00013209          24.479          3.5883          1.4475
v  Pressure                -191.2          26.219         -16.111         0.25127
v  k                    2.938e-06          45.504         0.73396        0.028788
v  epsilon             1.1453e-07           22624          36.237          1.0718
v  TurbVisc            4.7643e-10         0.37489          0.1369         0.21868
v  CourantNb                    0          72.644          2.8087          0.4175
v  FourierNb             0.000336          42.444          2.6829          2.9662
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00036002          76.489          5.4916          3.3837


 TIME FOR THE TIME STEP               15:        0.37692E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.121140049E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083836E+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 : -0.29872E+02 0.11883E+02
   Friction velocity        uet   :  0.63336E-05 0.69073E+00
   Friction velocity        uk    :  0.28321E-02 0.36021E+01
   Dimensionless distance   yplus :  0.11031E+01 0.27090E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      21698
   Nb of faces within the viscous sub-layer     :         25
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        136 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17996E+03     142   0.28257E-01   0.17282E+01 0.63114E+01 
c  Velocity[X]                                      0.71193E+00 
c  Velocity[Y]                                      0.45348E+00 
c  Velocity[Z]                                      0.56274E+00 
c  Pressure     0.40901E+00     715   0.11283E-01   0.20827E+00 0.76126E+01 
c  k            0.11907E+02     132   0.41913E-02   0.17683E+00 0.11388E+02 
c  epsilon      0.97185E+03      93   0.29705E-02   0.51359E+03 0.11946E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -5.955e-05                             2
a  epsilon         -0.4048                             5


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.974          22.784        0.057439          0.1004
v  Velocity[Y]            -11.679          12.062         0.96134          1.1527
v  Velocity[Z]            -18.292          18.275     -6.2855e-05      2.9775e-06
v  ǁVelocityǁ          0.00012219          24.328          3.5972          1.4583
v  Pressure               -187.87          26.617          -15.57         0.30441
v  k                   3.2051e-06           48.31         0.77958        0.031771
v  epsilon             1.0851e-07           20625          38.295          1.1647
v  TurbVisc            1.6419e-10         0.37533         0.13581         0.21708
v  CourantNb                    0          72.089          2.8066         0.42098
v  FourierNb           0.00033565          41.468          2.6899          2.9426
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035969          76.061          5.4965          3.3636


 TIME FOR THE TIME STEP               16:        0.39007E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.842506081E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083837E+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 : -0.27656E+02 0.12275E+02
   Friction velocity        uet   :  0.62238E-05 0.74351E+00
   Friction velocity        uk    :  0.29768E-02 0.33741E+01
   Dimensionless distance   yplus :  0.14592E+01 0.27137E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      20768
   Nb of faces within the viscous sub-layer     :         31
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18124E+03     146   0.29447E-01   0.17604E+01 0.62954E+01 
c  Velocity[X]                                      0.72000E+00 
c  Velocity[Y]                                      0.47039E+00 
c  Velocity[Z]                                      0.57000E+00 
c  Pressure     0.41665E+00     737   0.11232E-01   0.20870E+00 0.78019E+01 
c  k            0.13059E+02     136   0.43718E-02   0.18623E+00 0.10802E+02 
c  epsilon      0.10331E+04      95   0.30867E-02   0.50913E+03 0.11208E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -4.8098e-05                             1
a  epsilon      -0.0040488                             9


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.894          22.341        0.057169         0.10054
v  Velocity[Y]            -11.802          12.123          0.9606          1.1548
v  Velocity[Z]            -17.841          17.969     -0.00049752      1.0061e-05
v  ǁVelocityǁ          0.00011944              24          3.6021          1.4692
v  Pressure               -183.42          27.058         -14.933         0.39291
v  k                   3.5213e-06          52.941         0.82125        0.034853
v  epsilon             5.3925e-09           17961          40.174          1.2567
v  TurbVisc            1.5587e-08          0.5284         0.13473         0.21547
v  CourantNb                    0          71.198          2.8013         0.42436
v  FourierNb           0.00033556          50.257           2.695           2.919
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035936          75.225          5.4963          3.3433


 TIME FOR THE TIME STEP               17:        0.39807E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.260990280E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083837E+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 : -0.26802E+02 0.12840E+02
   Friction velocity        uet   :  0.70389E-05 0.75308E+00
   Friction velocity        uk    :  0.27421E-02 0.31454E+01
   Dimensionless distance   yplus :  0.15337E+01 0.26926E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      19747
   Nb of faces within the viscous sub-layer     :         35
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        159 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18261E+03     343   0.30798E-01   0.17919E+01 0.62789E+01 
c  Velocity[X]                                      0.72894E+00 
c  Velocity[Y]                                      0.48637E+00 
c  Velocity[Z]                                      0.57660E+00 
c  Pressure     0.42393E+00     739   0.11114E-01   0.20902E+00 0.79302E+01 
c  k            0.14263E+02     177   0.45133E-02   0.19105E+00 0.10195E+02 
c  epsilon      0.10948E+04      98   0.33808E-02   0.53464E+03 0.10896E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -2.0703e-05                             1
a  epsilon         -7.9823                            28


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.947          22.293        0.056931         0.10065
v  Velocity[Y]            -11.501          11.673         0.96131          1.1568
v  Velocity[Z]            -17.327          17.511     -0.00088789       1.615e-05
v  ǁVelocityǁ          0.00010087          24.249          3.6038          1.4802
v  Pressure                  -179          27.373         -14.265         0.48201
v  k                   3.8734e-06          55.434         0.85778        0.037997
v  epsilon              3.796e-08           21339          41.817          1.3457
v  TurbVisc            2.7876e-08          10.505         0.13365         0.21386
v  CourantNb                    0          70.072          2.7933         0.42764
v  FourierNb           0.00033593          108.64           2.697          2.8954
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035904          108.87          5.4904           3.323


 TIME FOR THE TIME STEP               18:        0.47904E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.151095445E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083835E+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+02 0.12513E+02
   Friction velocity        uet   :  0.40707E-05 0.78474E+00
   Friction velocity        uk    :  0.29296E-02 0.35456E+01
   Dimensionless distance   yplus :  0.15636E+01 0.26453E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      18740
   Nb of faces within the viscous sub-layer     :         37
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18408E+03     155   0.31960E-01   0.18210E+01 0.62592E+01 
c  Velocity[X]                                      0.73727E+00 
c  Velocity[Y]                                      0.50100E+00 
c  Velocity[Z]                                      0.58272E+00 
c  Pressure     0.43450E+00     756   0.11012E-01   0.21090E+00 0.80597E+01 
c  k            0.15499E+02     141   0.46123E-02   0.19033E+00 0.95657E+01 
c  epsilon      0.11706E+04      97   0.35720E-02   0.54987E+03 0.10545E+02 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.1791e-05                             1
a  epsilon         -54.254                            17


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.343          22.651        0.056739         0.10074
v  Velocity[Y]            -11.463          11.598         0.96386          1.1589
v  Velocity[Z]            -17.054          17.086      -0.0012352      2.6226e-05
v  ǁVelocityǁ          8.6172e-05          24.592          3.6032          1.4913
v  Pressure                -178.9          28.658         -13.573         0.59048
v  k                   5.2968e-07          54.202          0.8884        0.041157
v  epsilon             3.5416e-08           33665          43.183          1.4299
v  TurbVisc            1.3402e-08          1.2909         0.13256         0.21223
v  CourantNb                    0          69.067          2.7833         0.43083
v  FourierNb           0.00033664          125.77          2.6952          2.8718
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035872          130.06          5.4785          3.3026


 TIME FOR THE TIME STEP               19:        0.40710E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.101315351E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083837E+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 : -0.24731E+02 0.12721E+02
   Friction velocity        uet   :  0.28570E-05 0.77530E+00
   Friction velocity        uk    :  0.24511E-02 0.40115E+01
   Dimensionless distance   yplus :  0.12498E+01 0.26970E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      17627
   Nb of faces within the viscous sub-layer     :         30
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        159 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18564E+03     158   0.33359E-01   0.18477E+01 0.62365E+01 
c  Velocity[X]                                      0.74497E+00 
c  Velocity[Y]                                      0.51437E+00 
c  Velocity[Z]                                      0.58839E+00 
c  Pressure     0.44249E+00     756   0.10750E-01   0.21130E+00 0.81765E+01 
c  k            0.16740E+02     141   0.45897E-02   0.18445E+00 0.89325E+01 
c  epsilon      0.12615E+04      98   0.32998E-02   0.50547E+03 0.97179E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -1.8523e-05                             1
a  epsilon          -204.3                            22


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.436          23.093        0.056618         0.10081
v  Velocity[Y]            -11.549          11.161         0.96806          1.1609
v  Velocity[Z]            -17.027          16.619      -0.0016352      3.1716e-05
v  ǁVelocityǁ          3.1459e-05          24.429          3.6011          1.5026
v  Pressure               -178.26          29.714         -12.859         0.73187
v  k                   4.2749e-06          57.544         0.91286        0.044283
v  epsilon             1.2655e-08           42387          44.265          1.5072
v  TurbVisc            1.4101e-11          1.6176         0.13147          0.2106
v  CourantNb                    0          68.259          2.7722         0.43394
v  FourierNb           0.00033771          39.068           2.689          2.8482
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0003584          71.905          5.4612          3.2822


 TIME FOR THE TIME STEP               20:        0.40692E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.161835114E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.23896E+02 0.12543E+02
   Friction velocity        uet   :  0.23448E-05 0.77126E+00
   Friction velocity        uk    :  0.25602E-02 0.41549E+01
   Dimensionless distance   yplus :  0.13523E+01 0.28265E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      16391
   Nb of faces within the viscous sub-layer     :         26
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        160 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18730E+03     160   0.34289E-01   0.18691E+01 0.62058E+01 
c  Velocity[X]                                      0.75004E+00 
c  Velocity[Y]                                      0.52601E+00 
c  Velocity[Z]                                      0.59306E+00 
c  Pressure     0.45191E+00     740   0.10431E-01   0.21225E+00 0.82144E+01 
c  k            0.17959E+02     140   0.44590E-02   0.17490E+00 0.83269E+01 
c  epsilon      0.13414E+04     100   0.30462E-02   0.43808E+03 0.87972E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -8.5788                            17


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.366          22.324        0.056542         0.10087
v  Velocity[Y]            -11.545          10.765         0.97331          1.1629
v  Velocity[Z]            -17.398          16.464      -0.0019162      4.1784e-05
v  ǁVelocityǁ          3.7711e-05          24.598          3.5987          1.5141
v  Pressure               -176.96          30.312         -12.187         0.86481
v  k                   4.4896e-06          51.707          0.9314        0.047329
v  epsilon             9.8761e-09           38469          45.069          1.5761
v  TurbVisc            3.2558e-08          4.3613         0.13037         0.20895
v  CourantNb                    0          66.927          2.7609         0.43698
v  FourierNb           0.00033907          66.604          2.6786          2.8247
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035808          70.354          5.4396          3.2616


 TIME FOR THE TIME STEP               21:        0.40415E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.257111471E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.23543E+02 0.12328E+02
   Friction velocity        uet   :  0.17360E-05 0.74889E+00
   Friction velocity        uk    :  0.24462E-02 0.39385E+01
   Dimensionless distance   yplus :  0.12483E+01 0.29445E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      15301
   Nb of faces within the viscous sub-layer     :         27
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        161 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18903E+03    2204   0.35156E-01   0.18835E+01 0.61648E+01 
c  Velocity[X]                                      0.75116E+00 
c  Velocity[Y]                                      0.53665E+00 
c  Velocity[Z]                                      0.59573E+00 
c  Pressure     0.45900E+00     739   0.10047E-01   0.21204E+00 0.82274E+01 
c  k            0.19123E+02    1915   0.44883E-02   0.16429E+00 0.77946E+01 
c  epsilon      0.13973E+04    1933   0.96677E-02   0.40258E+03 0.82909E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00010214                             1
a  epsilon         -4.9175                            35


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.296          22.324        0.056368          0.1009
v  Velocity[Y]            -11.023          10.568         0.97855          1.1649
v  Velocity[Z]            -17.627          16.451      -0.0021568      4.9882e-05
v  ǁVelocityǁ          2.3112e-05          24.824           3.597          1.5257
v  Pressure               -175.66          29.763         -11.558          1.0132
v  k                   4.6139e-06          51.299         0.94442        0.050263
v  epsilon             9.4117e-10           31674          45.607          1.6354
v  TurbVisc            7.9493e-08          11.454         0.12927          0.2073
v  CourantNb                    0          66.096          2.7506         0.43997
v  FourierNb           0.00034065          2690.2          2.6652          2.8011
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035776          2693.3          5.4158          3.2411


 TIME FOR THE TIME STEP               22:        0.17359E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.174974456E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083836E+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 : -0.22916E+02 0.12112E+02
   Friction velocity        uet   :  0.81255E-06 0.75698E+00
   Friction velocity        uk    :  0.24071E-02 0.38377E+01
   Dimensionless distance   yplus :  0.12121E+01 0.30280E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      14448
   Nb of faces within the viscous sub-layer     :         32
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        161 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19084E+03    1636   0.37069E-01   0.18935E+01 0.61181E+01 
c  Velocity[X]                                      0.74842E+00 
c  Velocity[Y]                                      0.54659E+00 
c  Velocity[Z]                                      0.59853E+00 
c  Pressure     0.46538E+00     721   0.96854E-02   0.21130E+00 0.82105E+01 
c  k            0.20223E+02     634   0.41566E-02   0.15489E+00 0.73675E+01 
c  epsilon      0.13793E+04     103   0.68853E-02   0.39355E+03 0.81191E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00046991                             2
a  epsilon         -577.33                            50


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.029          22.329        0.056219         0.10092
v  Velocity[Y]            -10.551          10.875         0.98253          1.1669
v  Velocity[Z]            -17.516          16.868      -0.0023339      6.4059e-05
v  ǁVelocityǁ          1.9208e-05          24.101          3.5962          1.5375
v  Pressure               -173.14          29.976         -10.994          1.1495
v  k                   4.8341e-06          52.915         0.95268        0.053072
v  epsilon             6.6786e-09           23837          45.918          1.6856
v  TurbVisc            6.0491e-09          56.164         0.12817         0.20565
v  CourantNb                    0          65.162           2.742         0.44294
v  FourierNb           0.00034236          681.22           2.647          2.7776
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035745          681.49          5.3891          3.2206


 TIME FOR THE TIME STEP               23:        0.10330E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.201686942E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.22371E+02 0.12553E+02
   Friction velocity        uet   :  0.13472E-05 0.74971E+00
   Friction velocity        uk    :  0.15086E-02 0.35013E+01
   Dimensionless distance   yplus :  0.68034E+00 0.30895E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13739
   Nb of faces within the viscous sub-layer     :         31
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        162 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19271E+03     274   0.36922E-01   0.19039E+01 0.60733E+01 
c  Velocity[X]                                      0.74701E+00 
c  Velocity[Y]                                      0.55621E+00 
c  Velocity[Z]                                      0.60064E+00 
c  Pressure     0.47235E+00     719   0.93501E-02   0.21078E+00 0.81706E+01 
c  k            0.21255E+02     147   0.39125E-02   0.14784E+00 0.70543E+01 
c  epsilon      0.13863E+04     104   0.33062E-02   0.36310E+03 0.77597E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -6.2705e-05                             1
a  epsilon       -0.058469                            25


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.073          22.384        0.056156         0.10091
v  Velocity[Y]            -10.575          11.109         0.98421          1.1688
v  Velocity[Z]             -17.36          16.557       -0.002499      7.3995e-05
v  ǁVelocityǁ          2.3482e-05          24.552          3.5965          1.5494
v  Pressure               -168.86          30.774         -10.497          1.2785
v  k                   5.1464e-06          53.058         0.95707        0.055755
v  epsilon             1.3405e-08           23591          46.028          1.7274
v  TurbVisc            1.3416e-10          8.5204         0.12704         0.20397
v  CourantNb                    0          64.985          2.7354         0.44593
v  FourierNb           0.00034411          177.79          2.6264          2.7537
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035714          178.33          5.3618          3.1997


 TIME FOR THE TIME STEP               24:        0.44824E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.891346218E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.21120E+02 0.12765E+02
   Friction velocity        uet   :  0.10782E-05 0.71690E+00
   Friction velocity        uk    :  0.23360E-02 0.34055E+01
   Dimensionless distance   yplus :  0.11068E+01 0.31066E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      13041
   Nb of faces within the viscous sub-layer     :         41
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        163 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19465E+03     168   0.37639E-01   0.19138E+01 0.60292E+01 
c  Velocity[X]                                      0.74640E+00 
c  Velocity[Y]                                      0.56416E+00 
c  Velocity[Z]                                      0.60320E+00 
c  Pressure     0.47877E+00     715   0.90868E-02   0.21001E+00 0.81273E+01 
c  k            0.22214E+02     152   0.37898E-02   0.14329E+00 0.68433E+01 
c  epsilon      0.14075E+04     136   0.42358E-02   0.34228E+03 0.75133E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00011774                             2
a  epsilon         -16.964                            46


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.947           22.38        0.056267         0.10089
v  Velocity[Y]            -10.185          11.319         0.98304          1.1708
v  Velocity[Z]            -16.902          16.526      -0.0026377      8.9648e-05
v  ǁVelocityǁ          2.2387e-05          24.933          3.5979          1.5616
v  Pressure               -163.94          30.489         -10.055          1.4141
v  k                    5.559e-06          53.617         0.95882        0.058328
v  epsilon             5.0252e-10           26336          45.987          1.7623
v  TurbVisc            3.1268e-08           4.375         0.12591         0.20228
v  CourantNb                    0          65.302          2.7306         0.44892
v  FourierNb           0.00034545          204.14          2.6041          2.7298
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035683          207.83          5.3347          3.1787


 TIME FOR THE TIME STEP               25:        0.41277E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.129539648E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083836E+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 : -0.18920E+02 0.13380E+02
   Friction velocity        uet   :  0.20931E-05 0.75153E+00
   Friction velocity        uk    :  0.20019E-02 0.34474E+01
   Dimensionless distance   yplus :  0.12656E+01 0.31010E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      12470
   Nb of faces within the viscous sub-layer     :         39
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        162 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19666E+03    5533   0.39315E-01   0.19227E+01 0.59849E+01 
c  Velocity[X]                                      0.74501E+00 
c  Velocity[Y]                                      0.57194E+00 
c  Velocity[Z]                                      0.60576E+00 
c  Pressure     0.48599E+00     702   0.89189E-02   0.20951E+00 0.80992E+01 
c  k            0.23093E+02    2336   0.36262E-02   0.14021E+00 0.66970E+01 
c  epsilon      0.14183E+04     106   0.28178E-02   0.34580E+03 0.75592E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0016623                             5
a  epsilon         -208.19                            47


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.816          22.492        0.056488         0.10084
v  Velocity[Y]            -10.209          11.552         0.97904          1.1727
v  Velocity[Z]            -16.835          16.661      -0.0027259      0.00010394
v  ǁVelocityǁ          3.7396e-05          25.225          3.6003          1.5739
v  Pressure               -158.65          30.158           -9.65           1.554
v  k                   6.0731e-06          56.367          0.9592        0.060813
v  epsilon             1.2886e-09           28377          45.851          1.7917
v  TurbVisc            2.6888e-08          122.07          0.1248         0.20061
v  CourantNb                    0          65.542          2.7272         0.45193
v  FourierNb           0.00034559          1454.8          2.5818          2.7064
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035652          1455.2          5.3091          3.1583


 TIME FOR THE TIME STEP               26:        0.29062E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.145142470E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083835E+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 : -0.16761E+02 0.13506E+02
   Friction velocity        uet   :  0.36710E-05 0.75882E+00
   Friction velocity        uk    :  0.18419E-02 0.36452E+01
   Dimensionless distance   yplus :  0.93580E+00 0.30760E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11953
   Nb of faces within the viscous sub-layer     :         43
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        161 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.19871E+03    1504   0.38905E-01   0.19311E+01 0.59409E+01 
c  Velocity[X]                                      0.74359E+00 
c  Velocity[Y]                                      0.57909E+00 
c  Velocity[Z]                                      0.60846E+00 
c  Pressure     0.49034E+00     684   0.87921E-02   0.20794E+00 0.79807E+01 
c  k            0.23903E+02     748   0.34113E-02   0.13729E+00 0.65744E+01 
c  epsilon      0.14248E+04     108   0.26732E-02   0.30469E+03 0.71277E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0018178                             4
a  epsilon         -37.361                            62


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.055          22.508        0.056746         0.10078
v  Velocity[Y]            -10.079          11.567         0.97283          1.1747
v  Velocity[Z]            -17.034          16.786      -0.0027616      0.00011991
v  ǁVelocityǁ          4.2069e-05          25.241          3.6034          1.5864
v  Pressure               -155.59          30.256          -9.319          1.6703
v  k                   6.7408e-06          57.799         0.95925        0.063231
v  epsilon             1.8626e-08           29987          45.672           1.817
v  TurbVisc              6.19e-08          48.317         0.12366          0.1989
v  CourantNb                    0          65.792           2.725         0.45497
v  FourierNb           0.00034592          807.93          2.5594          2.6821
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035622          808.69          5.2843          3.1371


 TIME FOR THE TIME STEP               27:        0.10956E+04

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


 INSTANT    0.280000000E+00   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.553596853E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.15708E+02 0.13482E+02
   Friction velocity        uet   :  0.48281E-05 0.75760E+00
   Friction velocity        uk    :  0.22334E-02 0.35265E+01
   Dimensionless distance   yplus :  0.95233E+00 0.30823E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11475
   Nb of faces within the viscous sub-layer     :         40
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        160 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20082E+03     144   0.39018E-01   0.19373E+01 0.58947E+01 
c  Velocity[X]                                      0.74036E+00 
c  Velocity[Y]                                      0.58706E+00 
c  Velocity[Z]                                      0.60985E+00 
c  Pressure     0.49583E+00     684   0.86525E-02   0.20691E+00 0.79194E+01 
c  k            0.24669E+02     137   0.31200E-02   0.13370E+00 0.64465E+01 
c  epsilon      0.14222E+04      96   0.24064E-02   0.31297E+03 0.72627E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0028633                             3
a  epsilon         -19.508                            54


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.22           22.51         0.05698          0.1007
v  Velocity[Y]            -10.077          11.591         0.96553          1.1766
v  Velocity[Z]            -16.725          16.761      -0.0028062      0.00013089
v  ǁVelocityǁ          4.9481e-05          25.157          3.6068          1.5991
v  Pressure               -151.86          30.724         -9.0256          1.7773
v  k                   6.5138e-06          57.632         0.95965        0.065608
v  epsilon             2.3692e-09           31866          45.498          1.8397
v  TurbVisc            5.1524e-09           2.906         0.12252          0.1972
v  CourantNb                    0          66.113          2.7236         0.45804
v  FourierNb           0.00034544          41.933          2.5381           2.658
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035592          69.174          5.2617          3.1161


 TIME FOR THE TIME STEP               28:        0.38322E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.108318381E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.14805E+02 0.13518E+02
   Friction velocity        uet   :  0.54338E-05 0.76000E+00
   Friction velocity        uk    :  0.22336E-02 0.33689E+01
   Dimensionless distance   yplus :  0.10816E+01 0.31601E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      11073
   Nb of faces within the viscous sub-layer     :         37
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        158 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20299E+03     908   0.39443E-01   0.19402E+01 0.58448E+01 
c  Velocity[X]                                      0.73670E+00 
c  Velocity[Y]                                      0.59507E+00 
c  Velocity[Z]                                      0.60847E+00 
c  Pressure     0.49863E+00     684   0.84246E-02   0.20483E+00 0.78631E+01 
c  k            0.25422E+02     399   0.28511E-02   0.12966E+00 0.63122E+01 
c  epsilon      0.14288E+04      98   0.30495E-02   0.29578E+03 0.70854E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023103                             2
a  epsilon          -844.4                            78


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.229          22.359        0.057025          0.1006
v  Velocity[Y]            -10.087          11.695         0.95853          1.1785
v  Velocity[Z]            -16.545          16.867      -0.0027906      0.00014407
v  ǁVelocityǁ           6.086e-05          25.069          3.6101          1.6119
v  Pressure               -148.78          30.922         -8.7298          1.8976
v  k                   4.5471e-06          57.268         0.96061        0.067966
v  epsilon             1.1803e-09           33586          45.354          1.8611
v  TurbVisc            2.5285e-09          27.165          0.1214         0.19549
v  CourantNb                    0          66.356          2.7223         0.46113
v  FourierNb           0.00034432          390.53          2.5187          2.6342
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035562           391.3          5.2409          3.0953


 TIME FOR THE TIME STEP               29:        0.71177E+03

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


 INSTANT    0.300000000E+00   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.203789897E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.13658E+02 0.13354E+02
   Friction velocity        uet   :  0.61667E-05 0.75160E+00
   Friction velocity        uk    :  0.24068E-02 0.34657E+01
   Dimensionless distance   yplus :  0.11559E+01 0.32297E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10698
   Nb of faces within the viscous sub-layer     :         33
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        158 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20523E+03     933   0.39090E-01   0.19448E+01 0.57988E+01 
c  Velocity[X]                                      0.73365E+00 
c  Velocity[Y]                                      0.60234E+00 
c  Velocity[Z]                                      0.60885E+00 
c  Pressure     0.50319E+00     680   0.82834E-02   0.20393E+00 0.77568E+01 
c  k            0.26187E+02     188   0.26625E-02   0.12641E+00 0.61979E+01 
c  epsilon      0.14357E+04      97   0.22125E-02   0.27781E+03 0.68809E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.002479                             2
a  epsilon         -11.352                            40


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.334          22.395        0.056925         0.10049
v  Velocity[Y]            -10.298           11.83         0.95317          1.1804
v  Velocity[Z]            -16.749           16.96      -0.0026683      0.00014935
v  ǁVelocityǁ          7.4457e-05          24.521          3.6129          1.6248
v  Pressure               -145.65          31.313         -8.4658          1.9944
v  k                   5.5753e-06          59.864         0.96204        0.070321
v  epsilon             1.4379e-08           29082          45.242          1.8821
v  TurbVisc            3.9847e-10          45.374          0.1203         0.19381
v  CourantNb                    0          66.314          2.7207         0.46422
v  FourierNb           0.00033898          432.48          2.5004          2.6107
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035532           432.9           5.221          3.0749


 TIME FOR THE TIME STEP               30:        0.71783E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.315774211E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.12809E+02 0.13248E+02
   Friction velocity        uet   :  0.69871E-05 0.74630E+00
   Friction velocity        uk    :  0.20934E-02 0.34926E+01
   Dimensionless distance   yplus :  0.12198E+01 0.32729E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :      10330
   Nb of faces within the viscous sub-layer     :         34
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        157 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20755E+03     146   0.38797E-01   0.19474E+01 0.57509E+01 
c  Velocity[X]                                      0.73005E+00 
c  Velocity[Y]                                      0.60878E+00 
c  Velocity[Z]                                      0.60861E+00 
c  Pressure     0.50568E+00     680   0.81403E-02   0.20240E+00 0.77116E+01 
c  k            0.26981E+02     131   0.25700E-02   0.12421E+00 0.61083E+01 
c  epsilon      0.14447E+04      98   0.23612E-02   0.27989E+03 0.69152E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0022813                             2
a  epsilon           -71.8                            56


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.497          22.323        0.056623         0.10037
v  Velocity[Y]            -10.889          11.671         0.95034          1.1823
v  Velocity[Z]             -16.95          17.042      -0.0025401      0.00015603
v  ǁVelocityǁ          5.7054e-05          24.363          3.6152          1.6379
v  Pressure               -142.15          31.808          -8.214          2.0713
v  k                   6.2086e-06          59.296         0.96371        0.072686
v  epsilon             1.3616e-10           35474          45.146          1.9031
v  TurbVisc            2.4317e-09          4.0914         0.11915         0.19206
v  CourantNb                    0           66.46          2.7182         0.46732
v  FourierNb           0.00033363          67.897          2.4821          2.5862
v  total_pressure       1.012e+05      1.0157e+05      1.0141e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035502          69.555          5.2002          3.0535


 TIME FOR THE TIME STEP               31:        0.64082E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.645177211E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083835E+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 : -0.11718E+02 0.13070E+02
   Friction velocity        uet   :  0.28716E-05 0.73644E+00
   Friction velocity        uk    :  0.18081E-02 0.41764E+01
   Dimensionless distance   yplus :  0.11856E+01 0.33140E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9964
   Nb of faces within the viscous sub-layer     :         22
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        157 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21009E+03    8726   0.55234E-01   0.19507E+01 0.57053E+01 
c  Velocity[X]                                      0.72903E+00 
c  Velocity[Y]                                      0.61471E+00 
c  Velocity[Z]                                      0.60695E+00 
c  Pressure     0.51009E+00     684   0.80049E-02   0.20164E+00 0.76804E+01 
c  k            0.27814E+02    2507   0.24936E-02   0.12254E+00 0.60293E+01 
c  epsilon      0.14567E+04     392   0.34852E-02   0.28485E+03 0.69777E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.001774                             2
a  epsilon        -0.22525                            69


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.463          22.495        0.056261         0.10024
v  Velocity[Y]            -10.896          11.474         0.95038          1.1841
v  Velocity[Z]            -16.999          17.126      -0.0023928      0.00016488
v  ǁVelocityǁ          2.7613e-05          24.432          3.6171          1.6512
v  Pressure               -140.85           32.04         -7.9163          2.1791
v  k                   6.2482e-06          68.922          0.9656        0.075073
v  epsilon             2.0818e-09           53233          45.079          1.9245
v  TurbVisc            8.4239e-09          386.18         0.11811         0.19042
v  CourantNb                    0          66.418          2.7148         0.47043
v  FourierNb           0.00032862            4025          2.4664          2.5639
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035473          4025.3          5.1813          3.0343


 TIME FOR THE TIME STEP               32:        0.45287E+04

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


 INSTANT    0.330000000E+00   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.443654286E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.10831E+02 0.12866E+02
   Friction velocity        uet   :  0.23966E-05 0.72501E+00
   Friction velocity        uk    :  0.19558E-02 0.45471E+01
   Dimensionless distance   yplus :  0.99376E+00 0.33411E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9658
   Nb of faces within the viscous sub-layer     :         28
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        155 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21244E+03     740   0.38455E-01   0.19564E+01 0.56644E+01 
c  Velocity[X]                                      0.72848E+00 
c  Velocity[Y]                                      0.62128E+00 
c  Velocity[Z]                                      0.60666E+00 
c  Pressure     0.51309E+00     683   0.79476E-02   0.20035E+00 0.76430E+01 
c  k            0.28688E+02     165   0.24699E-02   0.12083E+00 0.59465E+01 
c  epsilon      0.14789E+04     100   0.27615E-02   0.25137E+03 0.65459E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0014546                             2
a  epsilon          -64.71                            68


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.448          22.218        0.055883         0.10009
v  Velocity[Y]            -10.201          11.308         0.95281           1.186
v  Velocity[Z]            -16.795          17.155      -0.0022618      0.00017336
v  ǁVelocityǁ          4.2898e-05          24.487           3.619          1.6646
v  Pressure                -140.7          32.213         -7.6127          2.2817
v  k                   6.1996e-06          66.793         0.96768        0.077492
v  epsilon             5.6931e-10           58664          45.053          1.9468
v  TurbVisc            1.8978e-08          26.184         0.11694         0.18862
v  CourantNb                    0          66.536           2.711         0.47354
v  FourierNb           0.00032392          360.12          2.4473          2.5385
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035444          360.35          5.1583          3.0121


 TIME FOR THE TIME STEP               33:        0.62153E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.349783936E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.10681E+02 0.12738E+02
   Friction velocity        uet   :  0.64120E-05 0.71819E+00
   Friction velocity        uk    :  0.21264E-02 0.44764E+01
   Dimensionless distance   yplus :  0.12334E+01 0.33472E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9358
   Nb of faces within the viscous sub-layer     :         28
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        153 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21501E+03    1211   0.39910E-01   0.19598E+01 0.56214E+01 
c  Velocity[X]                                      0.72786E+00 
c  Velocity[Y]                                      0.62658E+00 
c  Velocity[Z]                                      0.60540E+00 
c  Pressure     0.51617E+00     679   0.78455E-02   0.19928E+00 0.75741E+01 
c  k            0.29597E+02     305   0.23262E-02   0.11871E+00 0.58510E+01 
c  epsilon      0.14770E+04     135   0.32408E-02   0.24666E+03 0.64830E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00068605                             1
a  epsilon         -442.99                            76


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.157          22.196         0.05554        0.099922
v  Velocity[Y]            -10.462          11.247          0.9566          1.1879
v  Velocity[Z]            -17.016          17.149      -0.0022452      0.00018207
v  ǁVelocityǁ           7.806e-05          24.549          3.6211          1.6781
v  Pressure               -140.05          32.171         -7.3308          2.3662
v  k                   6.1891e-06          57.506         0.96995         0.07995
v  epsilon             1.0057e-09           51866          45.072          1.9701
v  TurbVisc            1.6814e-08          84.733         0.11583         0.18693
v  CourantNb                    0          66.928          2.7072         0.47668
v  FourierNb           0.00031955          397.16          2.4288          2.5148
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035415          397.35          5.1361          2.9914


 TIME FOR THE TIME STEP               34:        0.80977E+03

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


 INSTANT    0.350000000E+00   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.863893627E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.10595E+02 0.12682E+02
   Friction velocity        uet   :  0.10589E-04 0.71503E+00
   Friction velocity        uk    :  0.17320E-02 0.41535E+01
   Dimensionless distance   yplus :  0.89710E+00 0.33408E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       9088
   Nb of faces within the viscous sub-layer     :         25
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        152 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.21764E+03     646   0.38766E-01   0.19669E+01 0.55847E+01 
c  Velocity[X]                                      0.72892E+00 
c  Velocity[Y]                                      0.63283E+00 
c  Velocity[Z]                                      0.60517E+00 
c  Pressure     0.52069E+00     684   0.77935E-02   0.19892E+00 0.75742E+01 
c  k            0.30535E+02     203   0.21040E-02   0.11666E+00 0.57550E+01 
c  epsilon      0.14682E+04      97   0.23512E-02   0.27154E+03 0.67957E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -21.868                            91


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.118          22.138        0.055298         0.09974
v  Velocity[Y]            -10.227          11.329         0.96045          1.1897
v  Velocity[Z]            -16.879          17.132      -0.0022719       0.0001927
v  ǁVelocityǁ          0.00011451          24.436          3.6234          1.6918
v  Pressure               -138.55          32.601         -7.0199          2.4677
v  k                   3.4053e-07          57.471         0.97233        0.082454
v  epsilon             5.7795e-10           33209          45.124          1.9943
v  TurbVisc            4.7364e-09          52.671         0.11471         0.18519
v  CourantNb                    0          66.978          2.7039         0.47983
v  FourierNb           0.00031546          244.79          2.4095          2.4908
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035386          245.07          5.1134          2.9706


 TIME FOR THE TIME STEP               35:        0.57753E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.103962795E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.10082E+02 0.12563E+02
   Friction velocity        uet   :  0.13199E-04 0.70812E+00
   Friction velocity        uk    :  0.24893E-02 0.41523E+01
   Dimensionless distance   yplus :  0.12335E+01 0.33244E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8788
   Nb of faces within the viscous sub-layer     :         20
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        151 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22035E+03    1551   0.39146E-01   0.19745E+01 0.55499E+01 
c  Velocity[X]                                      0.73147E+00 
c  Velocity[Y]                                      0.63895E+00 
c  Velocity[Z]                                      0.60411E+00 
c  Pressure     0.52393E+00     679   0.77787E-02   0.19817E+00 0.75134E+01 
c  k            0.31494E+02     549   0.20063E-02   0.11512E+00 0.56703E+01 
c  epsilon      0.14704E+04      98   0.19130E-02   0.21446E+03 0.60273E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon           -9.04                           109


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.028          22.397        0.055208        0.099551
v  Velocity[Y]            -10.517          11.236         0.96307          1.1915
v  Velocity[Z]            -16.976          17.079      -0.0023081       0.0002089
v  ǁVelocityǁ          0.00015188          24.482          3.6257          1.7055
v  Pressure               -136.73          33.694         -6.7316          2.5561
v  k                   6.9181e-07          53.388         0.97469        0.085005
v  epsilon             1.7392e-10           34153          45.194          2.0193
v  TurbVisc            6.0213e-12          89.699          0.1136         0.18346
v  CourantNb                    0          67.231          2.7008         0.48299
v  FourierNb           0.00031165          504.27          2.3893          2.4668
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035358          504.46          5.0901          2.9498


 TIME FOR THE TIME STEP               36:        0.96454E+03

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


 INSTANT    0.370000000E+00   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.332773994E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083835E+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 : -0.94456E+01 0.12520E+02
   Friction velocity        uet   :  0.14489E-04 0.70555E+00
   Friction velocity        uk    :  0.20140E-02 0.40020E+01
   Dimensionless distance   yplus :  0.11082E+01 0.33042E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8500
   Nb of faces within the viscous sub-layer     :         13
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        149 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22313E+03    2510   0.41096E-01   0.19863E+01 0.55219E+01 
c  Velocity[X]                                      0.73512E+00 
c  Velocity[Y]                                      0.64544E+00 
c  Velocity[Z]                                      0.60579E+00 
c  Pressure     0.52622E+00     665   0.78088E-02   0.19721E+00 0.74967E+01 
c  k            0.32458E+02     731   0.19913E-02   0.11478E+00 0.56153E+01 
c  epsilon      0.14791E+04     105   0.22900E-02   0.21120E+03 0.59644E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -35.284                           142


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.313          22.463         0.05515        0.099347
v  Velocity[Y]            -10.207          11.146         0.96369          1.1933
v  Velocity[Z]            -16.817          17.133      -0.0024296      0.00021452
v  ǁVelocityǁ          0.00018546          24.515          3.6282          1.7194
v  Pressure               -136.47          33.558         -6.4493          2.6476
v  k                   6.4174e-06          49.648         0.97686        0.087601
v  epsilon             1.4313e-09           32851          45.256          2.0446
v  TurbVisc            3.7649e-10          304.85         0.11255         0.18174
v  CourantNb                    0           67.67           2.698         0.48617
v  FourierNb           0.00030811          4519.3          2.3708          2.4438
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035329          4519.7          5.0688          2.9299


 TIME FOR THE TIME STEP               37:        0.13457E+04

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


 INSTANT    0.380000000E+00   TIME STEP NUMBER              38
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.211076955E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.88273E+01 0.12523E+02
   Friction velocity        uet   :  0.15884E-04 0.70268E+00
   Friction velocity        uk    :  0.32778E-02 0.35853E+01
   Dimensionless distance   yplus :  0.18582E+01 0.33008E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8262
   Nb of faces within the viscous sub-layer     :          9
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        147 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22594E+03     850   0.38636E-01   0.19988E+01 0.54957E+01 
c  Velocity[X]                                      0.74009E+00 
c  Velocity[Y]                                      0.65181E+00 
c  Velocity[Z]                                      0.60692E+00 
c  Pressure     0.52670E+00     646   0.78549E-02   0.19563E+00 0.74894E+01 
c  k            0.33427E+02     706   0.32961E-02   0.11506E+00 0.55762E+01 
c  epsilon      0.16211E+04     578   0.48184E-01   0.25926E+03 0.65976E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -1735.5                           140


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.139          22.459        0.055179         0.09913
v  Velocity[Y]            -10.249          11.193         0.96204          1.1951
v  Velocity[Z]            -17.008           17.28      -0.0025752      0.00021594
v  ǁVelocityǁ          0.00021841          24.849           3.631          1.7334
v  Pressure                -135.8          34.244          -6.164          2.7512
v  k                   6.6079e-06          47.866         0.97889        0.090238
v  epsilon             2.7279e-10           23699           45.31            2.07
v  TurbVisc            9.6299e-09           34.89         0.11135         0.17998
v  CourantNb                    0          67.758          2.6955         0.48936
v  FourierNb           0.00030483          776.27          2.3475          2.4186
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035301          782.74           5.043           2.908


 TIME FOR THE TIME STEP               38:        0.79323E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.148821943E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.81438E+01 0.12459E+02
   Friction velocity        uet   :  0.17247E-04 0.69945E+00
   Friction velocity        uk    :  0.24629E-02 0.36051E+01
   Dimensionless distance   yplus :  0.15569E+01 0.33146E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       8000
   Nb of faces within the viscous sub-layer     :          5
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        146 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.22883E+03    1984   0.39900E-01   0.20147E+01 0.54750E+01 
c  Velocity[X]                                      0.74628E+00 
c  Velocity[Y]                                      0.65887E+00 
c  Velocity[Z]                                      0.60952E+00 
c  Pressure     0.53148E+00     576   0.78377E-02   0.19598E+00 0.74321E+01 
c  k            0.34352E+02     550   0.19234E-02   0.11567E+00 0.55465E+01 
c  epsilon      0.15036E+04      97   0.21261E-02   0.24825E+03 0.64364E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon          -55.63                           122


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.125          22.528        0.055255          0.0989
v  Velocity[Y]            -10.276          11.113         0.95831          1.1969
v  Velocity[Z]            -16.819          17.031      -0.0027739      0.00021932
v  ǁVelocityǁ            0.000223          25.154          3.6345          1.7475
v  Pressure               -134.22          33.981         -5.9336          2.8266
v  k                   6.8557e-06          52.003         0.98081        0.092914
v  epsilon             1.5566e-10           29414          45.345          2.0949
v  TurbVisc            1.3293e-08          192.96         0.11028         0.17825
v  CourantNb                    0          67.457          2.6933         0.49258
v  FourierNb           0.00030179          2433.9          2.3276          2.3953
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035273          2434.3          5.0209          2.8879


 TIME FOR THE TIME STEP               39:        0.10973E+04

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


 INSTANT    0.400000000E+00   TIME STEP NUMBER              40
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.102566277E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083831E+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 : -0.75440E+01 0.12353E+02
   Friction velocity        uet   :  0.18444E-04 0.69828E+00
   Friction velocity        uk    :  0.21140E-02 0.39498E+01
   Dimensionless distance   yplus :  0.11148E+01 0.33638E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7792
   Nb of faces within the viscous sub-layer     :          5
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        144 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23180E+03    2644   0.43232E-01   0.20301E+01 0.54546E+01 
c  Velocity[X]                                      0.75080E+00 
c  Velocity[Y]                                      0.66619E+00 
c  Velocity[Z]                                      0.61313E+00 
c  Pressure     0.53467E+00     571   0.78172E-02   0.19583E+00 0.74492E+01 
c  k            0.35271E+02    1271   0.80204E-02   0.11598E+00 0.55108E+01 
c  epsilon      0.15562E+04     867   0.28601E-01   0.23186E+03 0.61965E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -28.027                           179


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.88          22.769        0.055234        0.098668
v  Velocity[Y]            -11.599          11.066         0.95327          1.1987
v  Velocity[Z]            -17.185          16.994      -0.0028697      0.00022703
v  ǁVelocityǁ          0.00022338          25.056          3.6386          1.7616
v  Pressure               -133.98          35.455         -5.6978          2.9184
v  k                   7.1682e-06           60.75         0.98272        0.095625
v  epsilon             8.7127e-10           37182          45.367          2.1192
v  TurbVisc            9.2214e-09           308.8         0.10919         0.17664
v  CourantNb                    0          67.303           2.692         0.49581
v  FourierNb           0.00029896          1697.8          2.3066          2.3722
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035245          1698.1          4.9986           2.868


 TIME FOR THE TIME STEP               40:        0.15510E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.279243086E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083840E+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 : -0.72752E+01 0.12467E+02
   Friction velocity        uet   :  0.19859E-04 0.70202E+00
   Friction velocity        uk    :  0.25270E-02 0.42691E+01
   Dimensionless distance   yplus :  0.12342E+01 0.34973E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7589
   Nb of faces within the viscous sub-layer     :          7
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        142 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23469E+03     541   0.38856E-01   0.20446E+01 0.54336E+01 
c  Velocity[X]                                      0.75463E+00 
c  Velocity[Y]                                      0.67360E+00 
c  Velocity[Z]                                      0.61637E+00 
c  Pressure     0.53700E+00     575   0.78094E-02   0.19551E+00 0.73948E+01 
c  k            0.36155E+02     160   0.18096E-02   0.11610E+00 0.54719E+01 
c  epsilon      0.15756E+04     114   0.24000E-02   0.25074E+03 0.64221E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -18.115                           122


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.978          22.627        0.055123        0.098419
v  Velocity[Y]            -12.393          10.755         0.94803          1.2005
v  Velocity[Z]            -16.883          17.095      -0.0028654      0.00023812
v  ǁVelocityǁ          0.00022282           25.11          3.6431          1.7759
v  Pressure               -133.58          35.982         -5.4929          2.9977
v  k                   7.5619e-06          64.944         0.98473        0.098371
v  epsilon             1.1984e-09           43180           45.38           2.143
v  TurbVisc            4.8027e-09          60.836         0.10802         0.17479
v  CourantNb                    0          66.937          2.6914         0.49906
v  FourierNb           0.00029634          436.24          2.2851           2.347
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035217          436.61          4.9765          2.8461


 TIME FOR THE TIME STEP               41:        0.49387E+03

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


 INSTANT    0.420000000E+00   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.266409576E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083852E+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 : -0.68558E+01 0.12489E+02
   Friction velocity        uet   :  0.21132E-04 0.70290E+00
   Friction velocity        uk    :  0.31921E-02 0.44140E+01
   Dimensionless distance   yplus :  0.17513E+01 0.36139E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7363
   Nb of faces within the viscous sub-layer     :          6
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        141 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.23766E+03     698   0.38632E-01   0.20608E+01 0.54156E+01 
c  Velocity[X]                                      0.75789E+00 
c  Velocity[Y]                                      0.68195E+00 
c  Velocity[Z]                                      0.62092E+00 
c  Pressure     0.54508E+00     570   0.78669E-02   0.19754E+00 0.73995E+01 
c  k            0.37029E+02     683   0.17212E-02   0.11604E+00 0.54302E+01 
c  epsilon      0.15879E+04     522   0.26254E-02   0.20525E+03 0.58147E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon          -174.4                           125


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.988          22.623        0.054986        0.098173
v  Velocity[Y]            -10.928          10.709         0.94371          1.2023
v  Velocity[Z]            -16.894          17.153      -0.0028181      0.00023547
v  ǁVelocityǁ          0.00022264          24.858           3.648          1.7902
v  Pressure               -132.74          36.181         -5.3045          3.0717
v  k                   8.0633e-06          61.481         0.98672         0.10115
v  epsilon             1.3416e-10           44862           45.37          2.1659
v  TurbVisc             4.401e-09          40.128         0.10689         0.17304
v  CourantNb                    0           66.41          2.6911         0.50234
v  FourierNb           0.00029392          780.87          2.2648          2.3228
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0003519          781.79           4.956          2.8251


 TIME FOR THE TIME STEP               42:        0.69256E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.372134296E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083844E+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 : -0.66947E+01 0.12475E+02
   Friction velocity        uet   :  0.22585E-04 0.70217E+00
   Friction velocity        uk    :  0.29096E-02 0.42947E+01
   Dimensionless distance   yplus :  0.18237E+01 0.37093E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7197
   Nb of faces within the viscous sub-layer     :          6
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24071E+03    5016   0.45270E-01   0.20759E+01 0.53969E+01 
c  Velocity[X]                                      0.76048E+00 
c  Velocity[Y]                                      0.68970E+00 
c  Velocity[Z]                                      0.62571E+00 
c  Pressure     0.54486E+00     554   0.79495E-02   0.19653E+00 0.73815E+01 
c  k            0.37890E+02    1758   0.16509E-02   0.11624E+00 0.53961E+01 
c  epsilon      0.15613E+04     504   0.18398E-02   0.25712E+03 0.65349E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0048294                             1
a  epsilon         -23.086                           145


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.133          22.441        0.054741        0.097911
v  Velocity[Y]            -12.762          10.572         0.94128           1.204
v  Velocity[Z]            -16.824          17.219      -0.0026497       0.0002402
v  ǁVelocityǁ          0.00022261          24.697          3.6532          1.8045
v  Pressure               -132.65          37.598         -5.1422           3.135
v  k                   6.1936e-06            55.5         0.98865         0.10397
v  epsilon             7.3477e-10           39089          45.333           2.188
v  TurbVisc            5.3382e-09          371.54         0.10585         0.17154
v  CourantNb                    0          65.582          2.6911         0.50563
v  FourierNb           0.00029169          1779.2          2.2459          2.3009
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035162          1779.5           4.937          2.8065


 TIME FOR THE TIME STEP               43:        0.24236E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.131018503E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083842E+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 : -0.63834E+01 0.12541E+02
   Friction velocity        uet   :  0.24132E-04 0.70617E+00
   Friction velocity        uk    :  0.28161E-02 0.40804E+01
   Dimensionless distance   yplus :  0.17676E+01 0.38002E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6967
   Nb of faces within the viscous sub-layer     :          5
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24363E+03     775   0.38619E-01   0.20894E+01 0.53767E+01 
c  Velocity[X]                                      0.76268E+00 
c  Velocity[Y]                                      0.69712E+00 
c  Velocity[Z]                                      0.62956E+00 
c  Pressure     0.54944E+00     553   0.79516E-02   0.19722E+00 0.73977E+01 
c  k            0.38745E+02     239   0.16294E-02   0.11686E+00 0.53722E+01 
c  epsilon      0.15467E+04      94   0.18426E-02   0.22781E+03 0.61573E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon         -391.55                           141


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.957          22.409        0.054579        0.097644
v  Velocity[Y]            -12.954           10.46         0.94129          1.2058
v  Velocity[Z]            -16.902          17.198      -0.0024283      0.00023663
v  ǁVelocityǁ          0.00022158          24.651          3.6584          1.8189
v  Pressure               -131.43          37.814         -4.9856          3.1938
v  k                   2.1379e-06          51.453         0.99061         0.10682
v  epsilon             9.7174e-10           35455          45.298          2.2097
v  TurbVisc            1.5842e-09          66.794         0.10469         0.16962
v  CourantNb                    0          65.561           2.691         0.50894
v  FourierNb           0.00028963          398.18          2.2266          2.2754
v  total_pressure       1.012e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035135          398.56          4.9176          2.7843


 TIME FOR THE TIME STEP               44:        0.58251E+03

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


 INSTANT    0.450000000E+00   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.189877552E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083846E+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 : -0.57543E+01 0.12605E+02
   Friction velocity        uet   :  0.25813E-04 0.70967E+00
   Friction velocity        uk    :  0.29559E-02 0.39289E+01
   Dimensionless distance   yplus :  0.17609E+01 0.38739E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6746
   Nb of faces within the viscous sub-layer     :          7
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        139 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24660E+03     725   0.38501E-01   0.21037E+01 0.53584E+01 
c  Velocity[X]                                      0.76408E+00 
c  Velocity[Y]                                      0.70565E+00 
c  Velocity[Z]                                      0.63396E+00 
c  Pressure     0.55128E+00     611   0.80367E-02   0.19689E+00 0.74304E+01 
c  k            0.39597E+02     204   0.16076E-02   0.11736E+00 0.53457E+01 
c  epsilon      0.15547E+04      93   0.18031E-02   0.18976E+03 0.56190E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.011175                             2
a  epsilon         -34.283                           105


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.288          22.412        0.054375        0.097373
v  Velocity[Y]            -12.305          10.513         0.94382          1.2075
v  Velocity[Z]              -16.7          17.472      -0.0021365      0.00022977
v  ǁVelocityǁ          0.00022269          24.911           3.664          1.8333
v  Pressure               -130.12           38.41         -4.8386          3.2432
v  k                   5.1386e-07          52.773         0.99253         0.10971
v  epsilon             2.2989e-10           35436          45.262          2.2311
v  TurbVisc            3.3225e-10          55.135         0.10358         0.16785
v  CourantNb                    0          65.129          2.6907         0.51226
v  FourierNb           0.00028773           368.9          2.2082          2.2512
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035108          369.23          4.8989          2.7634


 TIME FOR THE TIME STEP               45:        0.57472E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.283258163E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.54760E+01 0.12587E+02
   Friction velocity        uet   :  0.26473E-04 0.70834E+00
   Friction velocity        uk    :  0.31502E-02 0.39789E+01
   Dimensionless distance   yplus :  0.18757E+01 0.39468E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6556
   Nb of faces within the viscous sub-layer     :          7
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        137 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.24955E+03    1721   0.40306E-01   0.21166E+01 0.53391E+01 
c  Velocity[X]                                      0.76437E+00 
c  Velocity[Y]                                      0.71376E+00 
c  Velocity[Z]                                      0.63849E+00 
c  Pressure     0.55236E+00     607   0.80012E-02   0.19606E+00 0.74382E+01 
c  k            0.40452E+02     736   0.16062E-02   0.11739E+00 0.53086E+01 
c  epsilon      0.15785E+04     708   0.42556E-02   0.18234E+03 0.55013E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00012078                             1
a  epsilon         -188.77                            81


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.205          22.387        0.054258        0.097093
v  Velocity[Y]            -12.752          10.343         0.94825          1.2093
v  Velocity[Z]            -16.697          17.551      -0.0018556       0.0002236
v  ǁVelocityǁ          0.00021956          24.622            3.67          1.8478
v  Pressure               -129.28          37.782         -4.6962          3.2953
v  k                   2.4143e-06          58.139         0.99454         0.11264
v  epsilon             7.7617e-11           38669          45.243          2.2524
v  TurbVisc            2.7038e-11          219.34         0.10251         0.16622
v  CourantNb                    0          65.539          2.6908          0.5156
v  FourierNb           0.00028598            1322          2.1909          2.2285
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035081          1322.4          4.8816          2.7441


 TIME FOR THE TIME STEP               46:        0.11127E+04

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


 INSTANT    0.470000000E+00   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.946759589E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.53518E+01 0.12588E+02
   Friction velocity        uet   :  0.26480E-04 0.70776E+00
   Friction velocity        uk    :  0.31624E-02 0.41763E+01
   Dimensionless distance   yplus :  0.16950E+01 0.40055E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6345
   Nb of faces within the viscous sub-layer     :          7
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        135 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25305E+03   10000   0.72985E-01   0.21279E+01 0.53184E+01 
c  Velocity[X]                                      0.76403E+00 
c  Velocity[Y]                                      0.72115E+00 
c  Velocity[Z]                                      0.64274E+00 
c  Pressure     0.55271E+00     607   0.79778E-02   0.19493E+00 0.74430E+01 
c  k            0.41313E+02    7094   0.16208E-02   0.11729E+00 0.52685E+01 
c  epsilon      0.16068E+04    3326   0.64469E-02   0.20069E+03 0.57671E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020578                             2
a  epsilon         -381.17                           110


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.22          22.128        0.054274        0.096804
v  Velocity[Y]            -12.918          10.372         0.95357           1.211
v  Velocity[Z]            -16.854          17.535      -0.0015759       0.0002232
v  ǁVelocityǁ          0.00021632          24.756          3.6764          1.8623
v  Pressure               -128.12          38.236         -4.5559          3.3509
v  k                   3.5997e-06          64.704         0.99661         0.11563
v  epsilon             1.1039e-09           43914          45.241          2.2737
v  TurbVisc            3.8131e-10          683.26         0.10148         0.16486
v  CourantNb                    0          65.927          2.6912         0.51894
v  FourierNb           0.00028439          2682.8           2.173          2.2071
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035054            2683          4.8642           2.726


 TIME FOR THE TIME STEP               47:        0.55085E+04

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.122989379E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.62479E+01 0.12671E+02
   Friction velocity        uet   :  0.26480E-04 0.71234E+00
   Friction velocity        uk    :  0.35998E-02 0.44058E+01
   Dimensionless distance   yplus :  0.20070E+01 0.40733E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       6117
   Nb of faces within the viscous sub-layer     :          4
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        131 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25531E+03     437   0.38489E-01   0.21364E+01 0.52950E+01 
c  Velocity[X]                                      0.76341E+00 
c  Velocity[Y]                                      0.72854E+00 
c  Velocity[Z]                                      0.64443E+00 
c  Pressure     0.55615E+00     611   0.79838E-02   0.19516E+00 0.74271E+01 
c  k            0.42182E+02     120   0.14583E-02   0.11732E+00 0.52312E+01 
c  epsilon      0.16261E+04      96   0.15546E-02   0.17113E+03 0.53170E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00029732                             3
a  epsilon         -73.686                            98


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -23.11          22.028         0.05432        0.096505
v  Velocity[Y]             -13.25          10.275         0.95855          1.2127
v  Velocity[Z]            -16.995          17.387      -0.0013137      0.00022341
v  ǁVelocityǁ          0.00021124          24.356           3.683          1.8767
v  Pressure               -127.37          39.139           -4.41          3.4093
v  k                    2.483e-07          67.094         0.99863         0.11866
v  epsilon             8.7507e-10           47269          45.247          2.2952
v  TurbVisc            1.3957e-10          46.069         0.10027         0.16263
v  CourantNb                    0          66.723           2.692         0.52228
v  FourierNb           0.00028292          291.64          2.1533          2.1795
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035027          291.99          4.8453          2.7018


 TIME FOR THE TIME STEP               48:        0.45696E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.388386205E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.45679E+01 0.12686E+02
   Friction velocity        uet   :  0.26308E-04 0.71314E+00
   Friction velocity        uk    :  0.36810E-02 0.44864E+01
   Dimensionless distance   yplus :  0.22218E+01 0.41302E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5889
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        129 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.25813E+03    1117   0.38355E-01   0.21446E+01 0.52721E+01 
c  Velocity[X]                                      0.76271E+00 
c  Velocity[Y]                                      0.73569E+00 
c  Velocity[Z]                                      0.64621E+00 
c  Pressure     0.55586E+00     611   0.79816E-02   0.19410E+00 0.74249E+01 
c  k            0.43061E+02     338   0.14757E-02   0.11808E+00 0.52096E+01 
c  epsilon      0.16488E+04     481   0.35326E-02   0.18980E+03 0.55921E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.030514                             9
a  epsilon         -55.018                           109


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.999          22.091         0.05444        0.096199
v  Velocity[Y]            -11.561          10.433         0.96205          1.2144
v  Velocity[Z]            -16.751          17.274      -0.0011422      0.00022971
v  ǁVelocityǁ          0.00019928          24.622          3.6898          1.8912
v  Pressure               -128.03          38.685         -4.2866          3.4581
v  k                   1.6045e-06          66.448          1.0006         0.12174
v  epsilon             1.7812e-09           48017          45.253          2.3169
v  TurbVisc            1.1862e-11          65.513        0.099186         0.16091
v  CourantNb                    0          67.366          2.6929         0.52561
v  FourierNb           0.00028159          551.46          2.1351          2.1559
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00035001          554.79           4.828          2.6815


 TIME FOR THE TIME STEP               49:        0.79769E+03

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


 INSTANT    0.500000000E+00   TIME STEP NUMBER              50
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.158877063E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.55132E+01 0.12705E+02
   Friction velocity        uet   :  0.25488E-04 0.71455E+00
   Friction velocity        uk    :  0.38183E-02 0.44648E+01
   Dimensionless distance   yplus :  0.23047E+01 0.41886E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5718
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        126 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26090E+03     451   0.38125E-01   0.21534E+01 0.52507E+01 
c  Velocity[X]                                      0.76327E+00 
c  Velocity[Y]                                      0.74252E+00 
c  Velocity[Z]                                      0.64763E+00 
c  Pressure     0.55973E+00     625   0.79632E-02   0.19459E+00 0.73967E+01 
c  k            0.43953E+02     122   0.14466E-02   0.11942E+00 0.52006E+01 
c  epsilon      0.16554E+04      96   0.27984E-02   0.25029E+03 0.64070E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00025916                             2
a  epsilon         -1155.7                            73


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.858          22.479        0.054624        0.095884
v  Velocity[Y]            -11.116          10.338         0.96341          1.2161
v  Velocity[Z]             -16.63          17.312      -0.0010253      0.00023458
v  ǁVelocityǁ          0.00018859          25.165          3.6966          1.9056
v  Pressure               -127.42          38.745         -4.1521          3.5198
v  k                   5.4316e-06          73.712          1.0024         0.12488
v  epsilon             1.2115e-08           53957          45.253          2.3386
v  TurbVisc            8.3713e-10          32.648        0.098089         0.15913
v  CourantNb                    0          67.683          2.6941         0.52895
v  FourierNb           0.00028038          330.79          2.1164          2.1319
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034975          331.47          4.8105          2.6608


 TIME FOR THE TIME STEP               50:        0.46589E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.220253434E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083833E+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 : -0.44798E+01 0.12658E+02
   Friction velocity        uet   :  0.24798E-04 0.71249E+00
   Friction velocity        uk    :  0.39686E-02 0.47025E+01
   Dimensionless distance   yplus :  0.23954E+01 0.42247E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5509
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        125 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26363E+03     138   0.38152E-01   0.21609E+01 0.52283E+01 
c  Velocity[X]                                      0.76348E+00 
c  Velocity[Y]                                      0.74824E+00 
c  Velocity[Z]                                      0.64920E+00 
c  Pressure     0.55983E+00     609   0.79476E-02   0.19379E+00 0.73917E+01 
c  k            0.44858E+02     121   0.14481E-02   0.12120E+00 0.52005E+01 
c  epsilon      0.16479E+04      92   0.19185E-02   0.16469E+03 0.52031E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00028774                             2
a  epsilon         -44.319                            86


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.835          22.565        0.054747        0.095565
v  Velocity[Y]            -11.154          10.156         0.96245          1.2178
v  Velocity[Z]            -16.792          17.223      -0.0010362      0.00023621
v  ǁVelocityǁ          0.00017256           25.52          3.7037          1.9199
v  Pressure               -127.63          38.585         -4.0253          3.5806
v  k                   5.4723e-06          60.048          1.0042         0.12808
v  epsilon             4.3911e-09           54567           45.24          2.3602
v  TurbVisc               1.2e-09          4.6284        0.096994         0.15739
v  CourantNb                    0          67.684          2.6952         0.53228
v  FourierNb            0.0002793          61.393          2.0978           2.108
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034948          70.725          4.7931          2.6403


 TIME FOR THE TIME STEP               51:        0.34642E+03

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


 INSTANT    0.520000000E+00   TIME STEP NUMBER              52
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.908174178E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.40593E+01 0.12537E+02
   Friction velocity        uet   :  0.23591E-04 0.70545E+00
   Friction velocity        uk    :  0.35534E-02 0.42443E+01
   Dimensionless distance   yplus :  0.22036E+01 0.42590E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5296
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        123 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26630E+03     192   0.38290E-01   0.21655E+01 0.52031E+01 
c  Velocity[X]                                      0.76358E+00 
c  Velocity[Y]                                      0.75159E+00 
c  Velocity[Z]                                      0.65028E+00 
c  Pressure     0.56067E+00     613   0.79560E-02   0.19304E+00 0.73206E+01 
c  k            0.45776E+02     119   0.14567E-02   0.12263E+00 0.51923E+01 
c  epsilon      0.16344E+04      91   0.26534E-02   0.22777E+03 0.61278E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0025854                             6
a  epsilon         -0.2729                            93


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.616          22.736        0.054822        0.095244
v  Velocity[Y]            -11.554           10.37         0.95959          1.2195
v  Velocity[Z]            -16.959          17.181      -0.0010996      0.00024152
v  ǁVelocityǁ          0.00015643          25.421          3.7112          1.9343
v  Pressure               -127.29          38.128         -3.9148           3.641
v  k                   1.6915e-06          57.625          1.0061         0.13133
v  epsilon              3.123e-09           40929          45.231          2.3819
v  TurbVisc            1.3136e-09          13.705        0.095917         0.15566
v  CourantNb                    0          67.655          2.6966         0.53561
v  FourierNb           0.00027833          95.073          2.0798          2.0845
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034922          95.484          4.7763          2.6201


 TIME FOR THE TIME STEP               52:        0.36674E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.317089905E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.38929E+01 0.12477E+02
   Friction velocity        uet   :  0.22370E-04 0.70497E+00
   Friction velocity        uk    :  0.27397E-02 0.41578E+01
   Dimensionless distance   yplus :  0.15468E+01 0.42765E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5110
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        122 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26891E+03     594   0.37910E-01   0.21677E+01 0.51759E+01 
c  Velocity[X]                                      0.76197E+00 
c  Velocity[Y]                                      0.75515E+00 
c  Velocity[Z]                                      0.65055E+00 
c  Pressure     0.55977E+00     613   0.78933E-02   0.19187E+00 0.72998E+01 
c  k            0.46706E+02     357   0.14200E-02   0.12377E+00 0.51769E+01 
c  epsilon      0.16341E+04     382   0.25802E-02   0.21921E+03 0.60091E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00032203                             2
a  epsilon         -133.51                            96


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.616          23.034         0.05481         0.09492
v  Velocity[Y]             -11.07          10.138         0.95577          1.2212
v  Velocity[Z]            -17.218          17.119      -0.0012478       0.0002464
v  ǁVelocityǁ          0.00013841          25.324          3.7188          1.9486
v  Pressure               -127.07            38.5         -3.8008          3.7031
v  k                   7.9632e-07          59.198          1.0084         0.13464
v  epsilon              8.049e-10           41402           45.24          2.4038
v  TurbVisc            1.0974e-10          19.673        0.094833         0.15391
v  CourantNb                    0          67.438          2.6983         0.53896
v  FourierNb           0.00027747          498.92           2.062          2.0608
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034896          503.33          4.7603          2.5997


 TIME FOR THE TIME STEP               53:        0.59432E+03

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.185475607E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.39762E+01 0.12458E+02
   Friction velocity        uet   :  0.20940E-04 0.70523E+00
   Friction velocity        uk    :  0.24375E-02 0.42142E+01
   Dimensionless distance   yplus :  0.15594E+01 0.42875E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4913
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        117 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27151E+03    2481   0.40176E-01   0.21669E+01 0.51458E+01 
c  Velocity[X]                                      0.76077E+00 
c  Velocity[Y]                                      0.75626E+00 
c  Velocity[Z]                                      0.64989E+00 
c  Pressure     0.56266E+00     607   0.78209E-02   0.19204E+00 0.72154E+01 
c  k            0.47648E+02    1237   0.13721E-02   0.12463E+00 0.51550E+01 
c  epsilon      0.16376E+04     737   0.16361E-02   0.17917E+03 0.54333E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00035477                             2
a  epsilon         -322.23                            97


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.595           22.67        0.054737          0.0946
v  Velocity[Y]            -11.919          10.072         0.95221          1.2229
v  Velocity[Z]            -17.343          17.215      -0.0014319      0.00025746
v  ǁVelocityǁ          0.00011826          25.195          3.7267          1.9629
v  Pressure               -127.21          38.586          -3.699          3.7624
v  k                   7.3728e-06          63.697          1.0107         0.13801
v  epsilon             1.3889e-09           44482          45.243          2.4257
v  TurbVisc            1.4151e-10          79.527        0.093793         0.15227
v  CourantNb                    0           67.07          2.7003          0.5423
v  FourierNb           0.00027672          472.72          2.0447          2.0382
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034871          472.97           4.745          2.5805


 TIME FOR THE TIME STEP               54:        0.14704E+04

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


 INSTANT    0.550000000E+00   TIME STEP NUMBER              55
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.584463636E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.34774E+01 0.12424E+02
   Friction velocity        uet   :  0.19233E-04 0.70395E+00
   Friction velocity        uk    :  0.28268E-02 0.43714E+01
   Dimensionless distance   yplus :  0.18085E+01 0.42873E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4682
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        113 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27399E+03     625   0.37831E-01   0.21667E+01 0.51171E+01 
c  Velocity[X]                                      0.76043E+00 
c  Velocity[Y]                                      0.75601E+00 
c  Velocity[Z]                                      0.65024E+00 
c  Pressure     0.55927E+00     558   0.77606E-02   0.19009E+00 0.71600E+01 
c  k            0.48609E+02     424   0.13779E-02   0.12558E+00 0.51342E+01 
c  epsilon      0.16614E+04     507   0.37858E-02   0.17462E+03 0.53591E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00036238                             2
a  epsilon         -42.381                            95


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.681          22.442        0.054536        0.094275
v  Velocity[Y]            -13.181          9.8819         0.95008          1.2246
v  Velocity[Z]             -17.04          17.325      -0.0016808      0.00026765
v  ǁVelocityǁ          0.00010048          24.735          3.7344          1.9771
v  Pressure               -127.48          38.218         -3.6297          3.7989
v  k                   1.0402e-05          70.286          1.0132         0.14145
v  epsilon              1.786e-09           49955          45.248          2.4477
v  TurbVisc            4.6251e-09          45.372        0.092722         0.15053
v  CourantNb                    0          66.618          2.7023         0.54563
v  FourierNb           0.00027609          555.64          2.0278          2.0146
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034845          559.17          4.7301          2.5603


 TIME FOR THE TIME STEP               55:        0.62051E+03

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


 INSTANT    0.560000000E+00   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.113561210E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.32831E+01 0.12419E+02
   Friction velocity        uet   :  0.17633E-04 0.70380E+00
   Friction velocity        uk    :  0.41375E-02 0.45919E+01
   Dimensionless distance   yplus :  0.21474E+01 0.42830E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4505
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        112 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27644E+03     417   0.37654E-01   0.21612E+01 0.50831E+01 
c  Velocity[X]                                      0.75836E+00 
c  Velocity[Y]                                      0.75455E+00 
c  Velocity[Z]                                      0.64831E+00 
c  Pressure     0.56271E+00     557   0.76987E-02   0.19031E+00 0.71158E+01 
c  k            0.49593E+02     116   0.13383E-02   0.12684E+00 0.51190E+01 
c  epsilon      0.16908E+04      91   0.17086E-02   0.17033E+03 0.52820E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0003195                             3
a  epsilon         -87.269                            72


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.665          22.353        0.054409        0.093956
v  Velocity[Y]            -11.601          10.277         0.95023          1.2263
v  Velocity[Z]            -16.563          17.396      -0.0019516      0.00026871
v  ǁVelocityǁ          8.3519e-05          24.617          3.7418          1.9912
v  Pressure               -125.94          38.801         -3.5615          3.8349
v  k                   1.5767e-05          72.908          1.0157         0.14495
v  epsilon             5.0544e-09           53578          45.249          2.4698
v  TurbVisc            2.7766e-09          30.488        0.091627         0.14876
v  CourantNb                    0          65.733          2.7041         0.54896
v  FourierNb           0.00027557          216.65          2.0104          1.9906
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034819          217.19          4.7146          2.5395


 TIME FOR THE TIME STEP               56:        0.43315E+03

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


 INSTANT    0.570000000E+00   TIME STEP NUMBER              57
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.127735358E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.30497E+01 0.12514E+02
   Friction velocity        uet   :  0.15710E-04 0.70874E+00
   Friction velocity        uk    :  0.38188E-02 0.46768E+01
   Dimensionless distance   yplus :  0.16722E+01 0.42700E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4289
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        102 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.27884E+03     189   0.36986E-01   0.21585E+01 0.50529E+01 
c  Velocity[X]                                      0.75795E+00 
c  Velocity[Y]                                      0.75284E+00 
c  Velocity[Z]                                      0.64768E+00 
c  Pressure     0.55702E+00     576   0.75861E-02   0.18760E+00 0.70371E+01 
c  k            0.50598E+02     116   0.13383E-02   0.12824E+00 0.51061E+01 
c  epsilon      0.16964E+04     105   0.15945E-02   0.17390E+03 0.53329E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00046101                             3
a  epsilon         -45.216                           116


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.808          22.368        0.054219        0.093625
v  Velocity[Y]            -12.392          9.9114         0.95303          1.2279
v  Velocity[Z]            -16.792          17.618      -0.0022296       0.0002725
v  ǁVelocityǁ           7.547e-05          24.583          3.7494          2.0052
v  Pressure               -125.25          38.817         -3.4833          3.8807
v  k                   2.8653e-06          68.999          1.0181         0.14851
v  epsilon             9.1319e-10           52089          45.248           2.492
v  TurbVisc            2.0402e-08          11.447        0.090531         0.14697
v  CourantNb                    0          65.668          2.7056         0.55225
v  FourierNb           0.00027517          109.74          1.9935          1.9664
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034794          113.09          4.6991          2.5187


 TIME FOR THE TIME STEP               57:        0.35701E+03

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


 INSTANT    0.580000000E+00   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.120062829E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083831E+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 : -0.31270E+01 0.12533E+02
   Friction velocity        uet   :  0.13995E-04 0.70897E+00
   Friction velocity        uk    :  0.26435E-02 0.45497E+01
   Dimensionless distance   yplus :  0.15439E+01 0.42460E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4068
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        100 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28120E+03     497   0.37091E-01   0.21507E+01 0.50175E+01 
c  Velocity[X]                                      0.75740E+00 
c  Velocity[Y]                                      0.74851E+00 
c  Velocity[Z]                                      0.64481E+00 
c  Pressure     0.55258E+00     522   0.74437E-02   0.18517E+00 0.69738E+01 
c  k            0.51622E+02     142   0.13282E-02   0.12957E+00 0.50909E+01 
c  epsilon      0.16751E+04      90   0.26725E-02   0.21237E+03 0.58963E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k              -0.02664                             2
a  epsilon         -167.91                           134


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.932          22.594        0.054067         0.09329
v  Velocity[Y]            -13.365           10.08         0.95811          1.2296
v  Velocity[Z]            -17.161          17.713      -0.0024573      0.00027352
v  ǁVelocityǁ          7.9625e-05          24.503          3.7571          2.0191
v  Pressure               -124.95          39.328         -3.4289           3.908
v  k                   5.3906e-06          68.533          1.0206         0.15215
v  epsilon             1.5225e-09           50209          45.252          2.5143
v  TurbVisc            3.4508e-11          64.693        0.089485         0.14527
v  CourantNb                    0          65.575          2.7071         0.55555
v  FourierNb           0.00027488          385.58          1.9773          1.9434
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034769          385.93          4.6844          2.4989


 TIME FOR THE TIME STEP               58:        0.45646E+03

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


 INSTANT    0.590000000E+00   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.156483159E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083831E+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 : -0.31559E+01 0.12540E+02
   Friction velocity        uet   :  0.12595E-04 0.70829E+00
   Friction velocity        uk    :  0.33655E-02 0.45343E+01
   Dimensionless distance   yplus :  0.25522E+01 0.42217E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3898
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         98 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28351E+03     478   0.36760E-01   0.21441E+01 0.49843E+01 
c  Velocity[X]                                      0.75712E+00 
c  Velocity[Y]                                      0.74496E+00 
c  Velocity[Z]                                      0.64206E+00 
c  Pressure     0.55236E+00     540   0.73823E-02   0.18443E+00 0.69318E+01 
c  k            0.52660E+02     152   0.13013E-02   0.13051E+00 0.50679E+01 
c  epsilon      0.16651E+04      91   0.15756E-02   0.17870E+03 0.54063E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0023453                             3
a  epsilon         -24.599                           124


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.024          22.253         0.05392        0.092943
v  Velocity[Y]            -11.397          10.309         0.96462          1.2312
v  Velocity[Z]            -16.611          17.691      -0.0027283      0.00027743
v  ǁVelocityǁ          9.2224e-05          24.998           3.765           2.033
v  Pressure               -125.38          39.754         -3.3577          3.9479
v  k                   1.2593e-05          67.179           1.023         0.15585
v  epsilon             1.5406e-09           58007          45.264          2.5368
v  TurbVisc             4.186e-09          38.087         0.08841         0.14353
v  CourantNb                    0          65.846          2.7089         0.55882
v  FourierNb           0.00027472          295.16          1.9605          1.9198
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034744          295.46          4.6694          2.4786


 TIME FOR THE TIME STEP               59:        0.45612E+03

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


 INSTANT    0.600000000E+00   TIME STEP NUMBER              60
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.823122600E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083830E+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 : -0.31792E+01 0.12539E+02
   Friction velocity        uet   :  0.11821E-04 0.70672E+00
   Friction velocity        uk    :  0.40520E-02 0.44893E+01
   Dimensionless distance   yplus :  0.23840E+01 0.41906E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3698
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         96 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28577E+03     673   0.36487E-01   0.21348E+01 0.49484E+01 
c  Velocity[X]                                      0.75599E+00 
c  Velocity[Y]                                      0.73982E+00 
c  Velocity[Z]                                      0.63898E+00 
c  Pressure     0.54907E+00     520   0.73093E-02   0.18282E+00 0.68649E+01 
c  k            0.53711E+02     267   0.12675E-02   0.13161E+00 0.50474E+01 
c  epsilon      0.16303E+04      93   0.16508E-02   0.19831E+03 0.57101E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00021707                             3
a  epsilon         -33.558                           160


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.888          22.249        0.053842        0.092592
v  Velocity[Y]            -12.028          10.059         0.97132          1.2329
v  Velocity[Z]            -16.521           17.63      -0.0030167      0.00027657
v  ǁVelocityǁ          0.00011404          24.524           3.773          2.0467
v  Pressure               -124.86          40.257         -3.2873          3.9901
v  k                   2.3362e-05          59.746          1.0254         0.15961
v  epsilon             3.4541e-10           40414          45.277          2.5593
v  TurbVisc            4.6822e-09          41.461        0.087353         0.14182
v  CourantNb                    0          66.492          2.7109         0.56209
v  FourierNb           0.00027468          382.68          1.9438          1.8965
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034719          383.34          4.6547          2.4586


 TIME FOR THE TIME STEP               60:        0.54085E+03

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


 INSTANT    0.610000000E+00   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.206977402E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.32278E+01 0.12640E+02
   Friction velocity        uet   :  0.11388E-04 0.71102E+00
   Friction velocity        uk    :  0.35048E-02 0.40729E+01
   Dimensionless distance   yplus :  0.21563E+01 0.41686E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3518
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         95 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.28801E+03    2025   0.36737E-01   0.21262E+01 0.49141E+01 
c  Velocity[X]                                      0.75505E+00 
c  Velocity[Y]                                      0.73469E+00 
c  Velocity[Z]                                      0.63643E+00 
c  Pressure     0.54896E+00     518   0.73033E-02   0.18215E+00 0.67927E+01 
c  k            0.54775E+02    1480   0.14543E-02   0.13300E+00 0.50320E+01 
c  epsilon      0.16151E+04    1647   0.12015E-01   0.22333E+03 0.60780E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00026222                             2
a  epsilon         -1569.5                           137


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.951            22.3        0.053815        0.092239
v  Velocity[Y]            -12.451          10.068           0.977          1.2345
v  Velocity[Z]            -16.699          17.523      -0.0032989       0.0002786
v  ǁVelocityǁ          0.00013868          24.922           3.781          2.0602
v  Pressure               -125.35          40.823          -3.201          4.0422
v  k                   1.1864e-05          58.409          1.0278         0.16345
v  epsilon             5.3726e-10           30227          45.289          2.5819
v  TurbVisc             4.869e-09          166.85        0.086322         0.14016
v  CourantNb                    0          67.059          2.7133         0.56531
v  FourierNb           0.00027479          1764.8          1.9277          1.8739
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034694            1768           4.641          2.4392


 TIME FOR THE TIME STEP               61:        0.14566E+04

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


 INSTANT    0.620000000E+00   TIME STEP NUMBER              62
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.258756145E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083830E+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 : -0.32632E+01 0.12559E+02
   Friction velocity        uet   :  0.11650E-04 0.70495E+00
   Friction velocity        uk    :  0.30604E-02 0.36594E+01
   Dimensionless distance   yplus :  0.20193E+01 0.41416E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3321
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         86 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29021E+03    1315   0.38482E-01   0.21152E+01 0.48777E+01 
c  Velocity[X]                                      0.75229E+00 
c  Velocity[Y]                                      0.72877E+00 
c  Velocity[Z]                                      0.63410E+00 
c  Pressure     0.54382E+00     502   0.72181E-02   0.17994E+00 0.67302E+01 
c  k            0.55852E+02     595   0.12333E-02   0.13474E+00 0.50229E+01 
c  epsilon      0.15764E+04     276   0.16900E-02   0.17138E+03 0.53267E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.048874                             7
a  epsilon         -29.631                           188


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.829           22.57        0.053776        0.091879
v  Velocity[Y]            -10.833          10.477          0.9807          1.2361
v  Velocity[Z]            -16.745          17.382      -0.0035265      0.00028503
v  ǁVelocityǁ          0.00016626          24.942          3.7888          2.0737
v  Pressure               -125.78           41.24          -3.121          4.0891
v  k                    6.064e-06          57.275          1.0301         0.16735
v  epsilon             1.2924e-09           24891          45.293          2.6046
v  TurbVisc            3.3584e-10          104.68        0.085275          0.1385
v  CourantNb                    0           67.42          2.7156         0.56851
v  FourierNb           0.00027504          450.86          1.9103          1.8511
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034669          451.23           4.626          2.4196


 TIME FOR THE TIME STEP               62:        0.84844E+03

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


 INSTANT    0.630000000E+00   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.749135820E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.32943E+01 0.12521E+02
   Friction velocity        uet   :  0.12533E-04 0.70217E+00
   Friction velocity        uk    :  0.33409E-02 0.37447E+01
   Dimensionless distance   yplus :  0.18394E+01 0.40980E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3180
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         79 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29232E+03     368   0.35496E-01   0.21057E+01 0.48436E+01 
c  Velocity[X]                                      0.75248E+00 
c  Velocity[Y]                                      0.72223E+00 
c  Velocity[Z]                                      0.63094E+00 
c  Pressure     0.54173E+00     518   0.71832E-02   0.17869E+00 0.66670E+01 
c  k            0.56942E+02     165   0.12404E-02   0.13701E+00 0.50229E+01 
c  epsilon      0.15770E+04     277   0.21905E-02   0.15308E+03 0.50306E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00035912                             1
a  epsilon         -42.572                           174


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.824           22.37        0.053783        0.091525
v  Velocity[Y]            -11.151          10.168         0.98203          1.2378
v  Velocity[Z]            -16.795           17.39      -0.0037775      0.00028825
v  ǁVelocityǁ          0.00019729          25.126          3.7965           2.087
v  Pressure               -125.69          41.861         -3.0292          4.1467
v  k                   2.5831e-05          57.362          1.0323         0.17132
v  epsilon             9.2958e-10           27961           45.29          2.6272
v  TurbVisc             1.149e-09          44.047        0.084245         0.13676
v  CourantNb                    0          67.706          2.7179         0.57167
v  FourierNb           0.00027546          351.59          1.8941           1.828
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034644          351.89           4.612          2.3997


 TIME FOR THE TIME STEP               63:        0.44087E+03

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


 INSTANT    0.640000000E+00   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.480335991E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083834E+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 : -0.32397E+01 0.12485E+02
   Friction velocity        uet   :  0.14039E-04 0.69975E+00
   Friction velocity        uk    :  0.33346E-02 0.38434E+01
   Dimensionless distance   yplus :  0.20708E+01 0.40131E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3026
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         79 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29443E+03     667   0.35281E-01   0.20945E+01 0.48082E+01 
c  Velocity[X]                                      0.75057E+00 
c  Velocity[Y]                                      0.71508E+00 
c  Velocity[Z]                                      0.62886E+00 
c  Pressure     0.53766E+00     518   0.70784E-02   0.17673E+00 0.65899E+01 
c  k            0.58041E+02     266   0.12503E-02   0.13936E+00 0.50238E+01 
c  epsilon      0.15833E+04      91   0.28004E-02   0.14628E+03 0.49142E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0010545                             2
a  epsilon        -0.31803                           156


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.774           22.61        0.053776        0.091172
v  Velocity[Y]            -10.498          10.121         0.98122          1.2394
v  Velocity[Z]            -16.796          17.319      -0.0039406      0.00029858
v  ǁVelocityǁ          0.00023028          25.186          3.8041          2.1001
v  Pressure               -126.04          42.578         -2.9268          4.2137
v  k                   2.6672e-05          60.573          1.0346         0.17535
v  epsilon              1.307e-09           25196           45.29          2.6498
v  TurbVisc            1.6409e-08           61.29        0.083241         0.13512
v  CourantNb                    0          67.734            2.72         0.57479
v  FourierNb           0.00027604           346.3          1.8783          1.8059
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0003462          346.71          4.5982          2.3807


 TIME FOR THE TIME STEP               64:        0.53758E+03

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


 INSTANT    0.650000000E+00   TIME STEP NUMBER              65
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.117634649E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083836E+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 : -0.31646E+01 0.12518E+02
   Friction velocity        uet   :  0.16062E-04 0.68880E+00
   Friction velocity        uk    :  0.40456E-02 0.37463E+01
   Dimensionless distance   yplus :  0.19980E+01 0.39058E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2874
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         76 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29648E+03     966   0.35607E-01   0.20838E+01 0.47739E+01 
c  Velocity[X]                                      0.74925E+00 
c  Velocity[Y]                                      0.70842E+00 
c  Velocity[Z]                                      0.62609E+00 
c  Pressure     0.53576E+00     482   0.69664E-02   0.17562E+00 0.64913E+01 
c  k            0.59148E+02     348   0.12355E-02   0.14143E+00 0.50186E+01 
c  epsilon      0.15925E+04      91   0.16800E-02   0.18446E+03 0.55148E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k      
a  epsilon          -28.36                           229


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.771          22.761        0.053678        0.090818
v  Velocity[Y]            -10.677          10.215           0.979           1.241
v  Velocity[Z]            -16.646          17.146      -0.0041001      0.00030527
v  ǁVelocityǁ          0.00026575          24.918          3.8116          2.1131
v  Pressure               -124.39          43.274         -2.8708          4.2455
v  k                   9.0505e-06          60.514          1.0371         0.17945
v  epsilon              1.531e-09           24582          45.293          2.6725
v  TurbVisc            3.8454e-09          49.941        0.082281         0.13353
v  CourantNb                    0          67.562          2.7221         0.57787
v  FourierNb            0.0002768          404.88          1.8633          1.7846
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034595          405.22          4.5854          2.3625


 TIME FOR THE TIME STEP               65:        0.64862E+03

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


 INSTANT    0.660000000E+00   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.108333652E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083847E+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 : -0.30697E+01 0.12437E+02
   Friction velocity        uet   :  0.18548E-04 0.70248E+00
   Friction velocity        uk    :  0.36905E-02 0.36953E+01
   Dimensionless distance   yplus :  0.19917E+01 0.37578E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2731
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         73 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.29851E+03     453   0.35163E-01   0.20722E+01 0.47391E+01 
c  Velocity[X]                                      0.74758E+00 
c  Velocity[Y]                                      0.70117E+00 
c  Velocity[Z]                                      0.62344E+00 
c  Pressure     0.53438E+00     504   0.69010E-02   0.17479E+00 0.64512E+01 
c  k            0.60260E+02     120   0.12139E-02   0.14286E+00 0.50016E+01 
c  epsilon      0.15956E+04      92   0.16308E-02   0.16043E+03 0.51431E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -8.454e-05                             1
a  epsilon        -0.12506                           163


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.623          22.577        0.053558        0.090468
v  Velocity[Y]            -10.802          9.8541         0.97651          1.2426
v  Velocity[Z]            -16.596          17.435      -0.0041374      0.00030286
v  ǁVelocityǁ          0.00030083          25.069          3.8189           2.126
v  Pressure                -124.2          43.839         -2.7966          4.2929
v  k                   6.8526e-06          62.284          1.0397         0.18362
v  epsilon             1.2947e-09           32066          45.295           2.695
v  TurbVisc            1.0419e-09          40.613        0.081309         0.13191
v  CourantNb                    0          67.036          2.7242         0.58092
v  FourierNb           0.00027776          244.17          1.8485           1.763
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034571          244.56          4.5727           2.344


 TIME FOR THE TIME STEP               66:        0.43224E+03

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


 INSTANT    0.670000000E+00   TIME STEP NUMBER              67
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.657686405E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083853E+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 : -0.29640E+01 0.12378E+02
   Friction velocity        uet   :  0.21226E-04 0.68370E+00
   Friction velocity        uk    :  0.32102E-02 0.38199E+01
   Dimensionless distance   yplus :  0.19396E+01 0.35976E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2587
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         67 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30048E+03     400   0.34807E-01   0.20582E+01 0.47022E+01 
c  Velocity[X]                                      0.74444E+00 
c  Velocity[Y]                                      0.69340E+00 
c  Velocity[Z]                                      0.62039E+00 
c  Pressure     0.53371E+00     513   0.68388E-02   0.17428E+00 0.63734E+01 
c  k            0.61376E+02     121   0.11951E-02   0.14462E+00 0.49896E+01 
c  epsilon      0.16043E+04      92   0.15538E-02   0.16125E+03 0.51515E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00086649                             2
a  epsilon         -31.629                           179


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.846          22.593        0.053373        0.090121
v  Velocity[Y]            -11.184          10.083         0.97499          1.2443
v  Velocity[Z]            -16.684          17.372      -0.0041942      0.00030191
v  ǁVelocityǁ          0.00033411          24.822          3.8259          2.1386
v  Pressure               -124.24          44.457          -2.715          4.3459
v  k                    2.227e-07           64.97          1.0424         0.18785
v  epsilon             1.3874e-09           35427          45.298          2.7176
v  TurbVisc            1.9681e-09          46.662        0.080374         0.13034
v  CourantNb                    0          66.541          2.7262         0.58393
v  FourierNb           0.00027893          296.69          1.8345          1.7422
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034547          297.69          4.5607          2.3261


 TIME FOR THE TIME STEP               67:        0.41809E+03

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


 INSTANT    0.680000000E+00   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.949710732E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083846E+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 : -0.28383E+01 0.12309E+02
   Friction velocity        uet   :  0.23910E-04 0.70225E+00
   Friction velocity        uk    :  0.39648E-02 0.37997E+01
   Dimensionless distance   yplus :  0.23955E+01 0.35253E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2472
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         60 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30243E+03     360   0.34554E-01   0.20445E+01 0.46660E+01 
c  Velocity[X]                                      0.74157E+00 
c  Velocity[Y]                                      0.68523E+00 
c  Velocity[Z]                                      0.61769E+00 
c  Pressure     0.53197E+00     485   0.68363E-02   0.17345E+00 0.62947E+01 
c  k            0.62494E+02     111   0.11933E-02   0.14672E+00 0.49829E+01 
c  epsilon      0.15957E+04      92   0.15438E-02   0.16312E+03 0.51908E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0003948                             1
a  epsilon        -0.43204                           191


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.739          22.405          0.0531        0.089764
v  Velocity[Y]            -11.139          9.9965         0.97526          1.2459
v  Velocity[Z]             -16.66          17.523      -0.0042313      0.00030354
v  ǁVelocityǁ          0.00036672          25.072          3.8326          2.1511
v  Pressure               -123.73           45.32         -2.6538          4.3855
v  k                   9.6348e-07           66.82          1.0452         0.19214
v  epsilon             1.6614e-09           31541          45.293          2.7399
v  TurbVisc            9.6559e-13          44.551        0.079426         0.12874
v  CourantNb                    0          66.386           2.728         0.58689
v  FourierNb           0.00028034          379.41          1.8204           1.721
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034523          380.02          4.5484          2.3079


 TIME FOR THE TIME STEP               68:        0.39154E+03

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


 INSTANT    0.690000000E+00   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.199410015E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083835E+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 : -0.27069E+01 0.12243E+02
   Friction velocity        uet   :  0.26623E-04 0.68548E+00
   Friction velocity        uk    :  0.46289E-02 0.36643E+01
   Dimensionless distance   yplus :  0.22614E+01 0.35427E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2339
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30435E+03     349   0.34346E-01   0.20284E+01 0.46277E+01 
c  Velocity[X]                                      0.73797E+00 
c  Velocity[Y]                                      0.67674E+00 
c  Velocity[Z]                                      0.61373E+00 
c  Pressure     0.52906E+00     487   0.67732E-02   0.17217E+00 0.62127E+01 
c  k            0.63615E+02     112   0.12007E-02   0.14863E+00 0.49723E+01 
c  epsilon      0.15802E+04      91   0.19642E-02   0.15388E+03 0.50549E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0029703                             5
a  epsilon         -988.85                           208


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.966          22.335        0.052866        0.089414
v  Velocity[Y]            -10.635            9.97         0.97788          1.2475
v  Velocity[Z]            -16.572          17.695      -0.0042637      0.00029473
v  ǁVelocityǁ          0.00037725          24.514          3.8391          2.1634
v  Pressure                -124.2           45.83         -2.5766          4.4287
v  k                   1.3965e-05          63.131           1.048         0.19651
v  epsilon             4.0578e-10           23090          45.281          2.7621
v  TurbVisc             7.453e-10          37.765        0.078564         0.12728
v  CourantNb                    0          66.037          2.7294         0.58982
v  FourierNb             0.000282          351.82          1.8079          1.7018
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034499          352.34          4.5373          2.2916


 TIME FOR THE TIME STEP               69:        0.38770E+03

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


 INSTANT    0.700000000E+00   TIME STEP NUMBER              70
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.182553416E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083845E+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 : -0.27075E+01 0.12187E+02
   Friction velocity        uet   :  0.29226E-04 0.69800E+00
   Friction velocity        uk    :  0.41369E-02 0.36814E+01
   Dimensionless distance   yplus :  0.21686E+01 0.35483E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2238
   Nb of faces within the viscous sub-layer     :          3
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         53 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30626E+03    1901   0.36399E-01   0.20139E+01 0.45917E+01 
c  Velocity[X]                                      0.73506E+00 
c  Velocity[Y]                                      0.66776E+00 
c  Velocity[Z]                                      0.61110E+00 
c  Pressure     0.52768E+00     480   0.67816E-02   0.17150E+00 0.61456E+01 
c  k            0.64740E+02     672   0.11929E-02   0.15035E+00 0.49577E+01 
c  epsilon      0.15689E+04     108   0.17505E-02   0.15160E+03 0.50222E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00046169                             1
a  epsilon         -316.26                           147


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.931          22.316        0.052618        0.089046
v  Velocity[Y]            -11.853          10.119         0.98262          1.2491
v  Velocity[Z]            -16.359          17.715      -0.0042281      0.00028751
v  ǁVelocityǁ          0.00038332          25.289          3.8454          2.1755
v  Pressure               -124.42          46.483         -2.5163          4.4605
v  k                   5.8716e-06          60.598          1.0508         0.20094
v  epsilon             9.6572e-10           22286          45.279          2.7845
v  TurbVisc            1.3907e-10          154.49        0.077764         0.12593
v  CourantNb                    0          65.895          2.7307          0.5927
v  FourierNb           0.00028366          1225.1          1.7962          1.6839
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034475          1225.6          4.5269          2.2766


 TIME FOR THE TIME STEP               70:        0.10409E+04

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


 INSTANT    0.710000000E+00   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.185204504E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083839E+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 : -0.25218E+01 0.12185E+02
   Friction velocity        uet   :  0.31642E-04 0.68213E+00
   Friction velocity        uk    :  0.35815E-02 0.36829E+01
   Dimensionless distance   yplus :  0.20602E+01 0.35296E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2124
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         50 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.30809E+03    1090   0.34649E-01   0.19963E+01 0.45525E+01 
c  Velocity[X]                                      0.73093E+00 
c  Velocity[Y]                                      0.65822E+00 
c  Velocity[Z]                                      0.60715E+00 
c  Pressure     0.52471E+00     503   0.67024E-02   0.17027E+00 0.60793E+01 
c  k            0.65867E+02     296   0.11847E-02   0.15150E+00 0.49332E+01 
c  epsilon      0.15558E+04      92   0.15725E-02   0.13709E+03 0.47781E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00028007                             2
a  epsilon         -37.168                           168


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.984          22.182         0.05236         0.08868
v  Velocity[Y]            -12.285          10.072         0.98876          1.2507
v  Velocity[Z]            -16.775          17.775      -0.0042814      0.00027688
v  ǁVelocityǁ          0.00038873          24.576          3.8517          2.1873
v  Pressure               -124.01          47.117         -2.4539           4.491
v  k                   3.5831e-06          56.885          1.0537         0.20544
v  epsilon             2.1342e-10           23101          45.292          2.8072
v  TurbVisc            5.8572e-10          68.939        0.076868         0.12443
v  CourantNb                    0          66.071          2.7319         0.59554
v  FourierNb           0.00028437          449.74          1.7827           1.664
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034451          450.07          4.5146          2.2595


 TIME FOR THE TIME STEP               71:        0.69130E+03

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


 INSTANT    0.720000000E+00   TIME STEP NUMBER              72
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.596870586E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083832E+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 : -0.24573E+01 0.12274E+02
   Friction velocity        uet   :  0.33715E-04 0.68773E+00
   Friction velocity        uk    :  0.46372E-02 0.36245E+01
   Dimensionless distance   yplus :  0.26108E+01 0.34895E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2039
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31001E+03    3061   0.42111E-01   0.19777E+01 0.45128E+01 
c  Velocity[X]                                      0.72562E+00 
c  Velocity[Y]                                      0.64908E+00 
c  Velocity[Z]                                      0.60305E+00 
c  Pressure     0.52042E+00     484   0.66064E-02   0.16861E+00 0.60057E+01 
c  k            0.66998E+02     988   0.11715E-02   0.15259E+00 0.49073E+01 
c  epsilon      0.15371E+04     348   0.15937E-02   0.14810E+03 0.49738E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00020973                             2
a  epsilon        -0.39995                           159


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.949          22.278        0.052148        0.088305
v  Velocity[Y]            -12.468          10.169         0.99517          1.2523
v  Velocity[Z]            -17.072          17.712      -0.0043722      0.00027266
v  ǁVelocityǁ          0.00039483          24.946           3.858           2.199
v  Pressure                -124.5          47.764         -2.3874          4.5322
v  k                   3.0874e-06          53.427          1.0567         0.21001
v  epsilon             9.3134e-10           20888          45.307          2.8298
v  TurbVisc            4.1689e-10          277.85         0.07616         0.12345
v  CourantNb                    0            66.4          2.7333         0.59831
v  FourierNb           0.00028449          911.58          1.7712           1.649
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034427          911.88          4.5044          2.2473


 TIME FOR THE TIME STEP               72:        0.15488E+04

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


 INSTANT    0.730000000E+00   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.171319767E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083843E+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 : -0.23786E+01 0.12401E+02
   Friction velocity        uet   :  0.35592E-04 0.68239E+00
   Friction velocity        uk    :  0.47408E-02 0.36050E+01
   Dimensionless distance   yplus :  0.23721E+01 0.34330E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1939
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         42 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31169E+03    1562   0.33496E-01   0.19595E+01 0.44738E+01 
c  Velocity[X]                                      0.72002E+00 
c  Velocity[Y]                                      0.63968E+00 
c  Velocity[Z]                                      0.59977E+00 
c  Pressure     0.51689E+00     517   0.64996E-02   0.16732E+00 0.59294E+01 
c  k            0.68138E+02     611   0.11598E-02   0.15381E+00 0.48830E+01 
c  epsilon      0.15392E+04     311   0.19780E-02   0.14191E+03 0.48591E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00015073                             3
a  epsilon         -28.669                           153


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.076           22.08        0.052056        0.087924
v  Velocity[Y]            -12.501          10.146          1.0007          1.2538
v  Velocity[Z]            -16.765          17.755       -0.004533      0.00026943
v  ǁVelocityǁ          0.00040115          24.527           3.864          2.2105
v  Pressure                -124.6          48.612         -2.3195           4.564
v  k                   6.7856e-06          51.845          1.0597         0.21466
v  epsilon             6.6289e-10           21164          45.339          2.8529
v  TurbVisc            1.2712e-11          73.234        0.075295         0.12178
v  CourantNb                    0          66.723          2.7349         0.60105
v  FourierNb           0.00028458          636.63          1.7583          1.6289
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034404          637.55          4.4932            2.23


 TIME FOR THE TIME STEP               73:        0.94868E+03

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


 INSTANT    0.740000000E+00   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.140360390E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083856E+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 : -0.22844E+01 0.12481E+02
   Friction velocity        uet   :  0.37128E-04 0.68034E+00
   Friction velocity        uk    :  0.57020E-02 0.36201E+01
   Dimensionless distance   yplus :  0.25554E+01 0.33790E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1862
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         43 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31345E+03    1027   0.33704E-01   0.19396E+01 0.44334E+01 
c  Velocity[X]                                      0.71414E+00 
c  Velocity[Y]                                      0.63029E+00 
c  Velocity[Z]                                      0.59515E+00 
c  Pressure     0.51142E+00     502   0.63855E-02   0.16540E+00 0.58769E+01 
c  k            0.69283E+02     238   0.11501E-02   0.15545E+00 0.48651E+01 
c  epsilon      0.15443E+04      94   0.16366E-02   0.15296E+03 0.50368E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00018641                             3
a  epsilon          -43.55                           167


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.918          22.258        0.052013         0.08754
v  Velocity[Y]            -12.457          10.241          1.0045          1.2554
v  Velocity[Z]            -16.947          17.573      -0.0047621      0.00025998
v  ǁVelocityǁ          0.00038926          24.897          3.8699          2.2218
v  Pressure               -122.56          49.659         -2.2242           4.617
v  k                    1.887e-05          49.184          1.0628         0.21937
v  epsilon             4.1406e-10           24013          45.367          2.8761
v  TurbVisc            2.3105e-09          97.238        0.074583         0.12058
v  CourantNb                    0          67.218          2.7363         0.60373
v  FourierNb           0.00028483          956.31           1.747          1.6132
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0003438          956.74          4.4833          2.2169


 TIME FOR THE TIME STEP               74:        0.66014E+03

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


 INSTANT    0.750000000E+00   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.494651005E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083843E+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 : -0.21770E+01 0.12594E+02
   Friction velocity        uet   :  0.38428E-04 0.68044E+00
   Friction velocity        uk    :  0.55333E-02 0.36969E+01
   Dimensionless distance   yplus :  0.23986E+01 0.33435E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1786
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         45 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31519E+03    1986   0.34965E-01   0.19210E+01 0.43948E+01 
c  Velocity[X]                                      0.70894E+00 
c  Velocity[Y]                                      0.62062E+00 
c  Velocity[Z]                                      0.59140E+00 
c  Pressure     0.51170E+00     485   0.63149E-02   0.16533E+00 0.57785E+01 
c  k            0.70435E+02     718   0.11489E-02   0.15721E+00 0.48488E+01 
c  epsilon      0.15478E+04     104   0.16541E-02   0.15038E+03 0.49924E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00040838                             2
a  epsilon         -33.881                           162


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.929           22.36        0.052013        0.087146
v  Velocity[Y]            -10.764          10.353           1.006           1.257
v  Velocity[Z]            -17.175          17.556      -0.0050213      0.00025725
v  ǁVelocityǁ          0.00037777            25.1          3.8757          2.2329
v  Pressure               -121.79          50.596         -2.1526          4.6568
v  k                   1.5727e-05          47.712          1.0658         0.22416
v  epsilon             1.3408e-09           24862          45.377          2.8991
v  TurbVisc            1.4928e-09           155.2        0.073882         0.11944
v  CourantNb                    0          67.357          2.7377         0.60635
v  FourierNb           0.00028525          878.63          1.7355          1.5978
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034357          879.01          4.4732          2.2041


 TIME FOR THE TIME STEP               75:        0.10798E+04

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


 INSTANT    0.760000000E+00   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.208088443E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083846E+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 : -0.21614E+01 0.12565E+02
   Friction velocity        uet   :  0.39399E-04 0.67885E+00
   Friction velocity        uk    :  0.47745E-02 0.35896E+01
   Dimensionless distance   yplus :  0.26435E+01 0.33406E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1717
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         59 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31685E+03     362   0.33003E-01   0.19020E+01 0.43561E+01 
c  Velocity[X]                                      0.70305E+00 
c  Velocity[Y]                                      0.61163E+00 
c  Velocity[Z]                                      0.58727E+00 
c  Pressure     0.50788E+00     553   0.62412E-02   0.16403E+00 0.57225E+01 
c  k            0.71597E+02     132   0.11501E-02   0.15892E+00 0.48310E+01 
c  epsilon      0.15572E+04      91   0.15700E-02   0.15255E+03 0.50254E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00063883                             3
a  epsilon          -53.93                           122


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -22.78          22.627        0.052033        0.086753
v  Velocity[Y]            -10.509           10.03          1.0053          1.2586
v  Velocity[Z]            -16.599           17.26      -0.0053203      0.00024875
v  ǁVelocityǁ          0.00036992          25.097          3.8815          2.2437
v  Pressure               -121.57          51.563         -2.0666          4.7126
v  k                   1.9359e-06          48.203          1.0688         0.22901
v  epsilon             9.8261e-10           27825          45.385          2.9222
v  TurbVisc            4.2704e-09          48.983        0.073145         0.11821
v  CourantNb                    0          67.345          2.7391         0.60892
v  FourierNb           0.00028585          436.08          1.7238          1.5814
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034334          436.56          4.4629          2.1903


 TIME FOR THE TIME STEP               76:        0.41412E+03

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


 INSTANT    0.770000000E+00   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.287123012E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083856E+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 : -0.21562E+01 0.12541E+02
   Friction velocity        uet   :  0.39975E-04 0.67494E+00
   Friction velocity        uk    :  0.39010E-02 0.35875E+01
   Dimensionless distance   yplus :  0.26336E+01 0.33565E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1635
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for         79 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.31851E+03     729   0.32747E-01   0.18824E+01 0.43172E+01 
c  Velocity[X]                                      0.69718E+00 
c  Velocity[Y]                                      0.60293E+00 
c  Velocity[Z]                                      0.58226E+00 
c  Pressure     0.50307E+00     540   0.61720E-02   0.16238E+00 0.56373E+01 
c  k            0.72770E+02     118   0.11474E-02   0.16039E+00 0.48092E+01 
c  epsilon      0.15667E+04      91   0.15598E-02   0.14234E+03 0.48498E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00064865                             3
a  epsilon         -185.98                           135


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.737          22.745        0.052063         0.08637
v  Velocity[Y]            -10.706          9.9654           1.003          1.2601
v  Velocity[Z]            -16.675          17.476       -0.005651      0.00023817
v  ǁVelocityǁ          0.00036489          24.913           3.887          2.2544
v  Pressure               -121.74          52.504         -1.9869          4.7561
v  k                   7.8355e-06          51.427           1.072         0.23394
v  epsilon             3.5374e-10           26954          45.397          2.9455
v  TurbVisc            1.4061e-10          61.994        0.072474          0.1171
v  CourantNb                    0          67.239          2.7405         0.61144
v  FourierNb           0.00028662          375.79           1.713          1.5666
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034311          376.34          4.4535           2.178


 TIME FOR THE TIME STEP               77:        0.54186E+03

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


 INSTANT    0.780000000E+00   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.775540202E-16
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 : -0.21461E+01 0.12458E+02
   Friction velocity        uet   :  0.40400E-04 0.67217E+00
   Friction velocity        uk    :  0.35030E-02 0.35594E+01
   Dimensionless distance   yplus :  0.23649E+01 0.33875E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1560
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        110 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32013E+03    1191   0.32109E-01   0.18626E+01 0.42783E+01 
c  Velocity[X]                                      0.69097E+00 
c  Velocity[Y]                                      0.59428E+00 
c  Velocity[Z]                                      0.57731E+00 
c  Pressure     0.49947E+00     542   0.61243E-02   0.16117E+00 0.55454E+01 
c  k            0.73955E+02     418   0.11393E-02   0.16191E+00 0.47876E+01 
c  epsilon      0.15807E+04      92   0.15800E-02   0.16431E+03 0.51996E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0082691                             7
a  epsilon        -0.25589                           124


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.568           22.68        0.052059        0.085979
v  Velocity[Y]            -10.708          10.285          1.0002          1.2617
v  Velocity[Z]            -16.992          17.277      -0.0059394      0.00022918
v  ǁVelocityǁ          0.00035937          24.693          3.8924          2.2649
v  Pressure               -122.18          53.249         -1.9103           4.804
v  k                   7.7677e-06          52.834          1.0754         0.23894
v  epsilon             1.1862e-09           24139          45.416          2.9689
v  TurbVisc            2.2486e-09           174.8         0.07186         0.11611
v  CourantNb                    0           67.21          2.7418         0.61392
v  FourierNb           0.00028757          886.96           1.703          1.5531
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034288          887.46          4.4448           2.167


 TIME FOR THE TIME STEP               78:        0.75860E+03

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


 INSTANT    0.790000000E+00   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.975907056E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083859E+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 : -0.21342E+01 0.12371E+02
   Friction velocity        uet   :  0.40472E-04 0.67177E+00
   Friction velocity        uk    :  0.42564E-02 0.35390E+01
   Dimensionless distance   yplus :  0.22766E+01 0.34194E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1481
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        156 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32172E+03     755   0.32307E-01   0.18434E+01 0.42405E+01 
c  Velocity[X]                                      0.68513E+00 
c  Velocity[Y]                                      0.58622E+00 
c  Velocity[Z]                                      0.57201E+00 
c  Pressure     0.49768E+00     541   0.60987E-02   0.16049E+00 0.54766E+01 
c  k            0.75150E+02     238   0.11298E-02   0.16346E+00 0.47659E+01 
c  epsilon      0.15940E+04      94   0.15486E-02   0.14550E+03 0.48857E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00039846                             2
a  epsilon         -26.478                           123


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.009          22.657        0.051927        0.085586
v  Velocity[Y]            -11.746          10.058         0.99782          1.2633
v  Velocity[Z]            -17.276          17.228      -0.0062806      0.00021559
v  ǁVelocityǁ          0.00034709          24.607          3.8977          2.2752
v  Pressure               -123.22          54.155         -1.8531           4.836
v  k                   6.4252e-06          51.198          1.0789         0.24401
v  epsilon              6.514e-09           27413          45.439          2.9922
v  TurbVisc            2.3784e-09          55.625        0.071221         0.11504
v  CourantNb                    0          66.703          2.7431         0.61636
v  FourierNb           0.00028871          395.24           1.693          1.5389
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034265          395.95          4.4361          2.1553


 TIME FOR THE TIME STEP               79:        0.58337E+03

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


 INSTANT    0.800000000E+00   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.200694854E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083858E+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 : -0.21176E+01 0.12266E+02
   Friction velocity        uet   :  0.40350E-04 0.67583E+00
   Friction velocity        uk    :  0.27497E-02 0.35791E+01
   Dimensionless distance   yplus :  0.14139E+01 0.34422E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1398
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        211 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32327E+03     133   0.31846E-01   0.18251E+01 0.42042E+01 
c  Velocity[X]                                      0.68038E+00 
c  Velocity[Y]                                      0.57804E+00 
c  Velocity[Z]                                      0.56670E+00 
c  Pressure     0.49348E+00     522   0.60602E-02   0.15907E+00 0.54095E+01 
c  k            0.76358E+02     109   0.11282E-02   0.16544E+00 0.47500E+01 
c  epsilon      0.16053E+04      91   0.14854E-02   0.14222E+03 0.48231E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00056359                             2
a  epsilon        -0.28832                           105


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.978          22.525         0.05175        0.085198
v  Velocity[Y]            -10.878          9.9128         0.99695          1.2648
v  Velocity[Z]            -17.433          17.488         -0.0066       0.0002061
v  ǁVelocityǁ          0.00034006          25.016          3.9026          2.2853
v  Pressure               -124.11          54.807         -1.8035           4.862
v  k                   1.3769e-06          51.706          1.0825         0.24915
v  epsilon             1.1353e-09           35068          45.465          3.0156
v  TurbVisc            1.5495e-09          10.314        0.070612         0.11405
v  CourantNb                    0          66.544          2.7443         0.61875
v  FourierNb           0.00029005          70.203          1.6836          1.5256
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034242          70.681          4.4278          2.1443


 TIME FOR THE TIME STEP               80:        0.32596E+03

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


 INSTANT    0.810000000E+00   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.266112811E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083859E+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 : -0.20956E+01 0.12239E+02
   Friction velocity        uet   :  0.39817E-04 0.67105E+00
   Friction velocity        uk    :  0.42366E-02 0.38641E+01
   Dimensionless distance   yplus :  0.17898E+01 0.34450E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1310
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        272 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32478E+03     424   0.31423E-01   0.18096E+01 0.41714E+01 
c  Velocity[X]                                      0.67764E+00 
c  Velocity[Y]                                      0.57021E+00 
c  Velocity[Z]                                      0.56180E+00 
c  Pressure     0.48934E+00     558   0.59824E-02   0.15776E+00 0.53569E+01 
c  k            0.77578E+02     112   0.11423E-02   0.16763E+00 0.47366E+01 
c  epsilon      0.16117E+04     112   0.23684E-02   0.15623E+03 0.50510E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k           -0.00060933                             3
a  epsilon         -32.356                            94


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.016          22.467        0.051464        0.084809
v  Velocity[Y]            -12.287          10.152         0.99812          1.2664
v  Velocity[Z]            -17.276          17.565      -0.0069381        0.000192
v  ǁVelocityǁ          0.00033896          25.021          3.9075          2.2952
v  Pressure               -123.91          55.312         -1.7395           4.896
v  k                   2.0648e-07          59.525          1.0861         0.25437
v  epsilon             2.9122e-09           45057          45.482           3.039
v  TurbVisc            8.4488e-11          57.699        0.070061         0.11313
v  CourantNb                    0          65.956          2.7451         0.62109
v  FourierNb           0.00029158           577.7          1.6752          1.5133
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034219          578.39          4.4203          2.1344


 TIME FOR THE TIME STEP               81:        0.44886E+03

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


 INSTANT    0.820000000E+00   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685        -0.165867851E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083860E+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 : -0.22361E+01 0.12199E+02
   Friction velocity        uet   :  0.38668E-04 0.66940E+00
   Friction velocity        uk    :  0.43849E-02 0.42258E+01
   Dimensionless distance   yplus :  0.23680E+01 0.34419E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1228
   Nb of faces within the viscous sub-layer     :          1
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        329 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32626E+03     372   0.31246E-01   0.17921E+01 0.41366E+01 
c  Velocity[X]                                      0.67493E+00 
c  Velocity[Y]                                      0.56184E+00 
c  Velocity[Z]                                      0.55538E+00 
c  Pressure     0.48528E+00     522   0.58954E-02   0.15653E+00 0.53068E+01 
c  k            0.78811E+02     112   0.11498E-02   0.16946E+00 0.47175E+01 
c  epsilon      0.16165E+04      91   0.16221E-02   0.17973E+03 0.54130E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.011291                             5
a  epsilon        -0.97489                           101


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.015          22.481         0.05111        0.084421
v  Velocity[Y]            -10.991          10.891          1.0013          1.2679
v  Velocity[Z]            -17.194          17.546      -0.0072135      0.00019285
v  ǁVelocityǁ          0.00034345          24.899          3.9123           2.305
v  Pressure               -124.46          55.977         -1.7078          4.9033
v  k                   1.3811e-06          70.763          1.0897         0.25966
v  epsilon             3.3127e-10           57613          45.496          3.0623
v  TurbVisc            6.3247e-12          21.703        0.069498         0.11223
v  CourantNb                    0          65.778          2.7459         0.62339
v  FourierNb           0.00029331          134.09          1.6664           1.501
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034196          134.32          4.4123          2.1244


 TIME FOR THE TIME STEP               82:        0.41404E+03

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


 INSTANT    0.830000000E+00   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2       15836        -0.152083845E+03
Smooth wall               5      141685         0.475939273E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083858E+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 : -0.49570E+01 0.12200E+02
   Friction velocity        uet   :  0.36866E-04 0.67602E+00
   Friction velocity        uk    :  0.48554E-02 0.46075E+01
   Dimensionless distance   yplus :  0.26221E+01 0.34313E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1151
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


Incoming flow detained for        392 outlet faces on       9303

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.32773E+03    9398   0.31659E-01   0.17759E+01 0.41035E+01 
c  Velocity[X]                                      0.67309E+00 
c  Velocity[Y]                                      0.55408E+00 
c  Velocity[Z]                                      0.54874E+00 
c  Pressure     0.48338E+00     487   0.57995E-02   0.15598E+00 0.52277E+01 
c  k            0.80057E+02    3974   0.11487E-02   0.17087E+00 0.46921E+01 
c  epsilon      0.16210E+04    1072   0.17091E-02   0.14302E+03 0.48284E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k            -0.0054517                             5
a  epsilon         -33.931                            86


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -23.055          22.257        0.050644        0.084031
v  Velocity[Y]            -11.429           9.943           1.006          1.2695
v  Velocity[Z]             -17.16          17.664       -0.007533      0.00017815
v  ǁVelocityǁ          0.00035311          24.788           3.917          2.3145
v  Pressure               -123.95          56.398          -1.669          4.9173
v  k                   1.2937e-05          67.431          1.0934         0.26502
v  epsilon             3.9455e-11           60463          45.513          3.0857
v  TurbVisc            4.9266e-10          251.24        0.069027         0.11141
v  CourantNb                    0          65.894          2.7465         0.62565
v  FourierNb           0.00029526          3219.8          1.6596          1.4905
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034173          3220.3          4.4061          2.1161


 TIME FOR THE TIME STEP               83:        0.45308E+04

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


 INSTANT    0.840000000E+00   TIME STEP NUMBER              84
 ============================================================= 



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

  max_time_step                              84 (current: 84)

 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        -0.143589453E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        9303         0.152083858E+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 : -0.34406E+01 0.12286E+02
   Friction velocity        uet   :  0.34628E-04 0.67592E+00
   Friction velocity        uk    :  0.49445E-02 0.44977E+01
   Dimensionless distance   yplus :  0.30353E+01 0.34024E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1085
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :     141685
------------------------------------------------------------


@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            
@ @@ WARNING: MESH TOO REFINED AT THE WALL                   
@    ========                                                
@    The mesh seems to be too refined at the wall to use     
@      a high-Reynolds turbulence model.                     
@                                                            
@    The last time step at which too small values for the    
@      dimensionless distance to the wall (yplus) have been  
@      observed is the time step         82
@                                                            
@    The minimum value for yplus must be greater than the    
@      limit value YPLULI =    0.23810E+01
@                                                            
@    Have a look at the distribution of yplus at the wall    
@      (with EnSight or ParaView for example) to conclude on 
@      the way the results quality might be affected.        
@                                                            
@    This warning is only printed at the first two           
@      occurences of the problem and at the last time step   
@      of the calculation. The vanishing of the message does 
@      not necessarily mean the vanishing of the problem.    
@                                                            
@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@@
@                                                            

Incoming flow detained for        446 outlet faces on       9303


 Write final restart files
   checkpoint at iteration         84, Physical time    0.84000E+00


   ** 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:    0.88088E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.33400E+03   10000   0.19527E+00   0.17611E+01 0.40725E+01 
c  Velocity[X]                                      0.67155E+00 
c  Velocity[Y]                                      0.54626E+00 
c  Velocity[Z]                                      0.54325E+00 
c  Pressure     0.47762E+00     469   0.56921E-02   0.15419E+00 0.51862E+01 
c  k            0.81313E+02   10000   0.11505E-02   0.17213E+00 0.46644E+01 
c  epsilon      0.16059E+04    8372   0.41747E-02   0.16889E+03 0.52562E+01 
-----------------------------------------------------------------------------
  
  

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

   field       initial min     initial max  clips to min  clips to max
-  -------  --------------  --------------  ------------  ------------
a  k             -0.018259                             6
a  epsilon         -354.17                            95


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

   field                  minimum         maximum        set mean    spatial mean
-  --------------  --------------  --------------  --------------  --------------
v  Velocity[X]            -22.933          22.173         0.05023        0.083655
v  Velocity[Y]            -11.682          10.457          1.0114           1.271
v  Velocity[Z]            -17.065          17.686      -0.0078107      0.00017111
v  ǁVelocityǁ          0.00036717          24.792          3.9217          2.3239
v  Pressure               -123.19          57.337         -1.6413          4.9189
v  k                   5.8368e-06          54.566          1.0971         0.27045
v  epsilon             3.0828e-09           45596           45.53          3.1092
v  TurbVisc            1.0783e-09            1850         0.06882         0.11183
v  CourantNb                    0          66.209          2.7473         0.62787
v  FourierNb           0.00029742          7237.1          1.6531          1.4886
v  total_pressure      1.0121e+05      1.0157e+05      1.0142e+05       1.014e+05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00034151          7237.7          4.4005          2.1164


 TIME FOR THE TIME STEP               84:        0.67967E+04

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.44230E-02
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          73020.273 s
  System CPU time:         2256.592 s
  Total CPU time:        301045.157 s

  Elapsed time:           77210.172 s
  CPU / elapsed time          0.975

Memory use summary:

  Total memory used:                               8.864 GiB
                             local minimum:        2.180 GiB  (rank 3)
                             local maximum:        2.241 GiB  (rank 2)
  Theoretical instrumented dynamic memory:         5.350 GiB
                             local minimum:        1.332 GiB  (rank 0)
                             local maximum:        1.342 GiB  (rank 1)
