command: 
 /Programs/Code_Saturne-4.0.2/build-catalyst/libexec/code_saturne/cs_solver --param Valve Mesh=1M RSM.xml --mpi

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

                                  (R)
                      Code_Saturne

                      Version 4.0.2


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

  revision 4.0.2
  build Tue 18 Aug 2015 06:24:59 PM GMT-3
  MPI version 3.0 (Open MPI 1.8.4)


  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:                Wed 19 Aug 2015 08:50:44 AM GMT-3
  System:              Linux 2.6.32-431.el6.x86_64
  Machine:             AntechPC
  Processor:           model name	: Intel(R) Core(TM) i7-2670QM CPU @ 2.20GHz
  Memory:              16041 MB
  User:                antech (Andrew)
  Directory:           /home/antech/work/valve/RESU/20150819-0850_2
  MPI ranks:           8 (appnum attribute: 0)
  OpenMP threads:      1
  Processors/node:     8
  I/O read method:     collective MPI-IO (explicit offsets)
  I/O write method:    collective MPI-IO (explicit offsets)
  I/O rank step:        1

  External libraries for partitioning:
    SCOTCH 5.1.12

 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   =             11 (Nb variables                )
       NSCAL  =              0 (Nb scalars                  )
       NSCAUS =              0 (Nb user scalars             )
       NSCAPP =              0 (Nb specific physics scalars )
       NPROCE =              6 (Nb cell properties          )


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


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

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

       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.10000E+04 (Reference density           )
       VISCL0 =    0.20000E-03 (Ref. molecular dyn. visc.   )
       CP0    =    0.43000E+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  =             31 (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)     )

   - SSG Rij-epsilon     (ITURB = 31)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IRIJNU =              0 (Matrix stabilization        )
       IRIJRB =              0 (Reconstruct at boundaries   )
       IGRARI =              1 (Account for gravity         )
       ICLSYR =              1 (Symmetry implicitation      )
       ICLPTR =              0 (Wall implicitation          )

 --- 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))

   - SSG Rij-epsilon     (ITURB = 31)
       CSSGS1 =    0.17000E+01 (Cs1 coeff.                  )
       CSSGS2 =   -0.10500E+01 (Cs2 coeff.                  )
       CSSGR1 =    0.90000E+00 (Cr1 coeff.                  )
       CSSGR2 =    0.80000E+00 (Cr2 coeff.                  )
       CSSGR3 =    0.65000E+00 (Cr3 coeff.                  )
       CSSGR4 =    0.62500E+00 (Cr4 coeff.                  )
       CSSGR5 =    0.20000E+00 (Cr5 coeff.                  )
       CSRIJ  =    0.22000E+00 (Rij Cs diffusion coeff.     )
       CRIJ3  =    0.55000E+00 (Gravity term coeff.         )
       Ce1    =    0.14400E+01 (Ceps1 coeff.                )
       CSSGE2 =    0.18300E+01 (Ceps2 coeff.                )
       SIGMAE =    0.12200E+01 (sigma_eps coeff.            )
       CMU    =    0.90000E-01 (Cmu constant                )


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              2 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+01 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-08 (Minimum time step           )
       DTMAX  =    0.10000E-01 (Maximum time step           )
       DTREF  =    0.10000E-04 (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
 r11                   1  0.1000E+01
 r22                   1  0.1000E+01
 r33                   1  0.1000E+01
 r12                   1  0.1000E+01
 r13                   1  0.1000E+01
 r23                   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
 r11                   1      1      1      1      0 0.00E+00 0.10E+01
 r22                   1      1      1      1      0 0.00E+00 0.10E+01
 r33                   1      1      1      1      0 0.00E+00 0.10E+01
 r12                   1      1      1      1      0 0.00E+00 0.10E+01
 r13                   1      1      1      1      0 0.00E+00 0.10E+01
 r23                   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-03  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-03  0.0000E+00
 r11                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 r22                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 r33                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 r12                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 r13                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 r23                 100      1  0.1000E-04  0.1000E-03  0.0000E+00
 epsilon             100      1  0.1000E-04  0.1000E-03  0.0000E+00
-----------------------------------------------------------

-------------------------------------------
 Variable         IRCFLU IMLIGR      CLIMGR
-------------------------------------------
 Velocity              1     -1  0.1500E+01
 Pressure              1     -1  0.1500E+01
 r11                   1     -1  0.1500E+01
 r22                   1     -1  0.1500E+01
 r33                   1     -1  0.1500E+01
 r12                   1     -1  0.1500E+01
 r13                   1     -1  0.1500E+01
 r23                   1     -1  0.1500E+01
 epsilon               1     -1  0.1500E+01
-----------------------------------

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


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


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


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


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

------------------------------------
 Variable              EPSILO IDIRCL
------------------------------------
 Velocity          0.1000E-04      1
 Pressure          0.1000E-04      1
 r11               0.1000E-04      1
 r22               0.1000E-04      1
 r33               0.1000E-04      1
 r12               0.1000E-04      1
 r13               0.1000E-04      1
 r23               0.1000E-04      1
 epsilon           0.1000E-04      1
------------------------------------

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


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


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

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


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

       INPDT0 =              0 (1: 0 time step calcuation   )
       NTMABS =          10000 (Final time step required    )

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


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


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

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

 --- Post-processed variables


Velocity
Pressure
r11
r22
r33
r12
r13
r23
epsilon
TurbVisc
CourantNb
FourierNb
total_pressure
Local Time Step
         --           --

 --- 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 r11                           -1
         7 r22                           -1
         8 r33                           -1
         9 r12                           -1
        10 r13                           -1
        11 r23                           -1
        12 epsilon                       -1
        14 LamVisc                       -1
        15 TurbVisc                      -1
        16 CourantNb                     -1
        17 FourierNb                     -1
        18 total_pressure                -1
        19 Local Time Step               -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 r11                            0
         7 r22                            0
         8 r33                            0
         9 r12                            0
        10 r13                            0
        11 r23                            0
        12 epsilon                        0
        15 TurbVisc                    -999
        16 CourantNb                   -999
        17 FourierNb                   -999
        18 total_pressure              -999
        19 Local Time Step             -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

   1: name: Catalyst
      directory: postprocessing
      format: Catalyst
      options: 
      time dependency: fixed mesh
      output: every 1 time steps



Code_Saturne: cs_partition.c:2943: Warning
Partitioning with LibSCOTCH requested, but PT-SCOTCH is not available,
so serial SCOTCH will be used.
 Reading file:        mesh_input
 Finished reading:    mesh_input
 No "partition_input/domain_number_8" file available;

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

 Partitioning 1177965 cells to 4 domains
   (SCOTCH_graphPart).

  Total number of faces on parallel boundaries: 5290
  wall-clock time: 4.777127 s

  Number of cells per domain (histogramm):
    [     285658 ;     287917 [ =          1
    [     287917 ;     290177 [ =          1
    [     290177 ;     292437 [ =          0
    [     292437 ;     294697 [ =          0
    [     294697 ;     296957 [ =          1
    [     296957 ;     299216 [ =          0
    [     299216 ;     301476 [ =          0
    [     301476 ;     303736 [ =          0
    [     303736 ;     305996 [ =          0
    [     305996 ;     308256 ] =          1

 Writing file:        partition_output/domain_number_4
 Finished writing:    partition_output/domain_number_4

 Partitioning 1177965 cells to 8 domains
   (SCOTCH_graphPart).

  Total number of faces on parallel boundaries: 15372
  wall-clock time: 7.852163 s

  Number of cells per domain (histogramm):
    [     140076 ;     141519 [ =          2
    [     141519 ;     142963 [ =          1
    [     142963 ;     144406 [ =          1
    [     144406 ;     145850 [ =          0
    [     145850 ;     147293 [ =          0
    [     147293 ;     148737 [ =          1
    [     148737 ;     150180 [ =          0
    [     150180 ;     151624 [ =          0
    [     151624 ;     153067 [ =          0
    [     153067 ;     154511 ] =          3

 Writing file:        partition_output/domain_number_8
 Finished writing:    partition_output/domain_number_8

 Partitioning finished (13.6 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 =             140076
    maximum value =             154511

      1 : [     140076 ;     142963 [ =          3
      2 : [     142963 ;     145850 [ =          1
      3 : [     145850 ;     148737 [ =          1
      4 : [     148737 ;     151624 [ =          0
      5 : [     151624 ;     154511 ] =          3

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

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

    minimum value =             143842
    maximum value =             158741

      1 : [     143842 ;     146821 [ =          3
      2 : [     146821 ;     149801 [ =          1
      3 : [     149801 ;     152781 [ =          1
      4 : [     152781 ;     155761 [ =          0
      5 : [     155761 ;     158741 ] =          3

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

 Histogram of the number of ghost cells per rank:

    minimum value =               2820
    maximum value =               4276

      1 : [       2820 ;       3111 [ =          1
      2 : [       3111 ;       3402 [ =          0
      3 : [       3402 ;       3693 [ =          3
      4 : [       3693 ;       3984 [ =          2
      5 : [       3984 ;       4276 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =             278811
    maximum value =             307815

      1 : [     278811 ;     284611 [ =          3
      2 : [     284611 ;     290412 [ =          1
      3 : [     290412 ;     296213 [ =          1
      4 : [     296213 ;     302014 [ =          0
      5 : [     302014 ;     307815 ] =          3

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

 Histogram of the number of boundary faces per rank:

    minimum value =               6433
    maximum value =               8474

      1 : [       6433 ;       6841 [ =          5
      2 : [       6841 ;       7249 [ =          0
      3 : [       7249 ;       7657 [ =          1
      4 : [       7657 ;       8065 [ =          1
      5 : [       8065 ;       8474 ] =          1

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

 Histogram of the number of interior faces per cell:

    minimum value =                  2
    maximum value =                  4

      1 : [          2 ;          3 [ =        833
      2 : [          3 ;          4 ] =    1177132

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  2
    maximum value =                  5

      1 : [          2 ;          3 [ =          1
      2 : [          3 ;          4 [ =          4
      3 : [          4 ;          5 ] =          3

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

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

 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 =             143437
    maximum value =             158365

      1 : [     143437 ;     146422 [ =          3
      2 : [     146422 ;     149408 [ =          1
      3 : [     149408 ;     152393 [ =          1
      4 : [     152393 ;     155379 [ =          0
      5 : [     155379 ;     158365 ] =          3

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =              75783
    maximum value =              84107

      1 : [      75783 ;      77447 [ =          3
      2 : [      77447 ;      79112 [ =          1
      3 : [      79112 ;      80777 [ =          1
      4 : [      80777 ;      82442 [ =          0
      5 : [      82442 ;      84107 ] =          3

 Mesh coordinates:               minimum    and maximum
                       X : -1.2000000e-01  1.2000000e-01
                       Y : -6.9990911e-02  6.0000000e-02
                       Z : -7.0000000e-02  7.0000000e-02
 Mesh
     Number of cells:          1177965
     Number of interior faces: 2327348
     Number of boundary faces: 57164
     Number of vertices:       213908

 Groups:
    "Group_Of_All_Faces"
       boundary faces:        57164
    "Group_Of_All_Volumes"
       cells:               1177965
    "Inlet"
       boundary faces:         2782
    "Outlet"
       boundary faces:         2770

 --- Information on the volumes
       Minimum control volume      =  2.7744748e-10
       Maximum control volume      =  1.2741690e-08
       Total volume for the domain =  2.4661851e-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: 10 -->   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 (0.8 s)
                                                             
       ALMAX  =    0.13538E+00 (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
  r11               0.4000E-03  0.4000E-03
  r22               0.4000E-03  0.4000E-03
  r33               0.4000E-03  0.4000E-03
  r12               0.0000E+00  0.0000E+00
  r13               0.0000E+00  0.0000E+00
  r23               0.0000E+00  0.0000E+00
  epsilon           0.9771E-05  0.9771E-05
 ---------------------------------

                dt  0.1000E-04  0.1000E-04
 ---------------------------------



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

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



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



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


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




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


 INSTANT    0.100000000E-04   TIME STEP NUMBER               1
 ============================================================= 


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1000E+04  0.1000E+04
  molecular_viscos  0.2000E-03  0.2000E-03
  turbulent_viscos  0.3316E+01  0.3316E+01
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2        2782
Smooth wall               5       51612
Rough wall                6           0
Symmetry                  4           0
Free outlet               3        2770
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 =    0.12000E+00  -0.22227E-03  -0.42054E-03



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782         0.000000000E+00
Smooth wall               5       51612         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         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    :  0.12644E-01 0.13416E-01
   Dimensionless distance   yplus :  0.12439E+02 0.95421E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10747E-01       1   0.23789E-05   0.29685E+07 0.90909E+05 
c  Velocity[X]                                      0.19215E+07 
c  Velocity[Y]                                      0.78720E+06 
c  Velocity[Z]                                      0.25982E+06 
c  Pressure     0.71222E+00     662   0.72621E+00   0.94649E+00 0.90909E+05 
c  r11          0.18703E+00      10   0.33016E-01   0.29541E-01 0.72500E+05 
c  r22          0.18683E+00      10   0.33005E-01   0.29458E-01 0.72465E+05 
c  r33          0.18683E+00      10   0.33005E-01   0.29458E-01 0.72465E+05 
c  r12          0.22001E-04       9   0.28236E-01   0.42820E-09 0.90909E+05 
c  r13          0.22298E-04       9   0.27913E-01   0.44089E-09 0.90909E+05 
c  r23          0.25199E-07       9   0.32158E-01   0.58498E-15 0.90909E+05 
c  epsilon      0.27107E+01      11   0.34454E-01   0.98649E+01 0.90903E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -0.00020588                           651
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -58.066          64.592          3.8448          3.7856
v  Velocity[Y]             -17.106          87.237         0.11165        0.038985
v  Velocity[Z]             -56.624          60.356      -0.0049103      0.00037236
v  ǁVelocityǁ           0.00037566          90.234          4.9095          4.7699
v  Pressure             1.0324e+05      1.8971e+08      9.5897e+07      9.6762e+07
v  r11                  0.00011869         0.02291      0.00043788      0.00043247
v  r22                  0.00011702        0.022889      0.00043782      0.00043242
v  r33                  0.00011702        0.022889      0.00043782      0.00043242
v  r12                 -3.0667e-06      3.1573e-06      1.8314e-11      3.1408e-12
v  r13                 -3.3289e-06      3.2936e-06     -1.7619e-12     -4.9928e-12
v  r23                  -1.643e-08      1.6223e-08     -4.1899e-14     -1.2648e-14
v  epsilon              1.5668e-09         0.41913      0.00089605      0.00076309
v  TurbVisc                  3.316           3.316           3.316           3.316
v  CourantNb                     0               0               0               0
v  FourierNb              0.073348          0.7231         0.23112         0.21189
v  total_pressure       2.0456e+05      1.8981e+08      9.5998e+07      9.6864e+07
v  Local Time Step         1.1e-05         1.1e-05         1.1e-05         1.1e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.073348          0.7231         0.23112         0.21189


 TIME FOR THE TIME STEP                1:        0.51637E+02

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


 INSTANT    0.200000000E-04   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.330956153E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392527827E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.84998E-03 0.45544E+02
   Friction velocity        uet   :  0.84113E-04 0.42057E+01
   Friction velocity        uk    :  0.13268E-01 0.78807E-01
   Dimensionless distance   yplus :  0.18496E+02 0.26962E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13677E+04       6   0.30821E-01   0.64291E+04 0.45805E+04 
c  Velocity[X]                                      0.22117E+04 
c  Velocity[Y]                                      0.24151E+04 
c  Velocity[Z]                                      0.18024E+04 
c  Pressure     0.81442E+00     318   0.37869E-01   0.11366E+01 0.13972E+06 
c  r11          0.21175E+00       7   0.48150E-03   0.57343E-02 0.23060E+05 
c  r22          0.20895E+00       7   0.44572E-03   0.49921E-02 0.21895E+05 
c  r33          0.20894E+00       7   0.44535E-03   0.49889E-02 0.21890E+05 
c  r12          0.13710E-02      14   0.24658E-02   0.38262E-05 0.81949E+05 
c  r13          0.13524E-02      12   0.21348E-02   0.37406E-05 0.81850E+05 
c  r23          0.36767E-03      15   0.60461E-02   0.27773E-06 0.83270E+05 
c  epsilon      0.29833E+01       7   0.55008E-03   0.22647E+01 0.27693E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -0.00012774                           304
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -53.975          60.702          3.8698          3.8102
v  Velocity[Y]             -16.654          75.867         0.11295         0.04015
v  Velocity[Z]             -52.882          54.965      -0.0050045      0.00025994
v  ǁVelocityǁ            0.0014945          83.698          4.9414          4.8015
v  Pressure             -2.115e+06      1.7123e+06      7.9658e+05      8.0836e+05
v  r11                  0.00031308        0.031722      0.00045525      0.00044745
v  r22                  0.00031126        0.030641      0.00045437      0.00044673
v  r33                  0.00034126         0.03076      0.00045437      0.00044672
v  r12                 -0.00028276      0.00040254        9.01e-08      6.3659e-08
v  r13                 -0.00034629      0.00036179      1.0011e-09     -5.9159e-10
v  r23                 -0.00014812      0.00016016       4.107e-09      2.4513e-09
v  epsilon              2.5558e-09         0.59461       0.0012375       0.0010581
v  TurbVisc               0.001364           20679          3.1148          3.1968
v  CourantNb            8.7072e-06               1        0.092948        0.085869
v  FourierNb            0.00014656               1         0.23053         0.21197
v  total_pressure      -2.0137e+06      1.8136e+06       8.979e+05      9.0969e+05
v  Local Time Step      1.8169e-08        1.21e-05      1.2089e-05      1.2087e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00033315            1.85         0.32348         0.29784


 TIME FOR THE TIME STEP                2:        0.45547E+02

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


 INSTANT    0.300000000E-04   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.478030993E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392532914E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.77635E-03 0.46862E+02
   Friction velocity        uet   :  0.74712E-04 0.42799E+01
   Friction velocity        uk    :  0.13250E-01 0.93252E-01
   Dimensionless distance   yplus :  0.18524E+02 0.31923E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14104E+04       5   0.23460E-01   0.34524E+04 0.32541E+04 
c  Velocity[X]                                      0.11171E+04 
c  Velocity[Y]                                      0.13475E+04 
c  Velocity[Z]                                      0.98786E+03 
c  Pressure     0.47659E+00     282   0.16404E-01   0.51097E+00 0.12417E+06 
c  r11          0.24293E+00       7   0.55448E-03   0.56688E-02 0.17226E+05 
c  r22          0.23751E+00       7   0.51690E-03   0.49401E-02 0.16555E+05 
c  r33          0.23748E+00       7   0.51637E-03   0.49350E-02 0.16549E+05 
c  r12          0.30410E-02      13   0.15422E-02   0.71680E-05 0.44218E+05 
c  r13          0.30000E-02      11   0.14370E-02   0.69835E-05 0.44150E+05 
c  r23          0.87419E-03      14   0.25437E-02   0.71735E-06 0.48039E+05 
c  epsilon      0.36937E+01       6   0.57474E-03   0.22526E+01 0.19552E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -2.5822e-05                           228
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -50.35          62.152           3.872          3.8123
v  Velocity[Y]             -15.805          68.597         0.11241        0.040266
v  Velocity[Z]             -51.084          59.217      -0.0051283      0.00010066
v  ǁVelocityǁ           0.00058233          81.322          4.9456          4.8063
v  Pressure            -3.7904e+06      7.9306e+05      3.6286e+05      3.7152e+05
v  r11                   0.0002965        0.039824      0.00047471      0.00046431
v  r22                  0.00029861        0.037984      0.00047289      0.00046281
v  r33                  0.00031172        0.038264      0.00047288      0.00046279
v  r12                 -0.00070546       0.0009354      2.3054e-07      1.6877e-07
v  r13                 -0.00083243       0.0008402       2.518e-09     -1.2536e-09
v  r23                 -0.00044198      0.00045039      1.1221e-08       7.238e-09
v  epsilon              2.1035e-10         0.74887       0.0016184       0.0013889
v  TurbVisc              0.0013944           12677          3.2185          3.3285
v  CourantNb            2.8816e-05               1         0.10218        0.094396
v  FourierNb            0.00018066               1         0.25415         0.23437
v  total_pressure      -3.6891e+06      8.9439e+05      4.6418e+05      4.7285e+05
v  Local Time Step      1.9986e-08       1.331e-05      1.3281e-05      1.3274e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00055305          1.5992         0.35633         0.32877


 TIME FOR THE TIME STEP                3:        0.47234E+02

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


 INSTANT    0.400000000E-04   TIME STEP NUMBER               4
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.956753046E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392544249E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.83736E-03 0.44716E+02
   Friction velocity        uet   :  0.80585E-04 0.41751E+01
   Friction velocity        uk    :  0.13236E-01 0.10592E+00
   Dimensionless distance   yplus :  0.18533E+02 0.36269E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.41074E+04       5   0.70038E-02   0.23362E+04 0.25207E+04 
c  Velocity[X]                                      0.70201E+03 
c  Velocity[Y]                                      0.10461E+04 
c  Velocity[Z]                                      0.58811E+03 
c  Pressure     0.29973E+00     133   0.58252E-02   0.26665E+00 0.10011E+06 
c  r11          0.86845E+00       6   0.19135E-03   0.55462E-02 0.13264E+05 
c  r22          0.86630E+00       6   0.17434E-03   0.48278E-02 0.12845E+05 
c  r33          0.86628E+00       6   0.17409E-03   0.48216E-02 0.12840E+05 
c  r12          0.48257E-02      13   0.14081E-02   0.95179E-05 0.28464E+05 
c  r13          0.47424E-02      11   0.13315E-02   0.91539E-05 0.28324E+05 
c  r23          0.15036E-02      14   0.21345E-02   0.12313E-05 0.32311E+05 
c  epsilon      0.43111E+01       6   0.60679E-03   0.23216E+01 0.14898E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -2.0763e-05                           178
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -53.341           58.09          3.8729          3.8131
v  Velocity[Y]             -15.321          64.614         0.11149        0.040258
v  Velocity[Z]             -51.128          54.434      -0.0051313        5.27e-05
v  ǁVelocityǁ           0.00097829          76.547          4.9487          4.8102
v  Pressure            -4.0075e+06      8.6354e+05      3.6577e+05      3.7474e+05
v  r11                  0.00029038        0.046987      0.00049634      0.00048315
v  r22                  0.00023692        0.044592      0.00049346      0.00048076
v  r33                  0.00030007        0.045069      0.00049342      0.00048072
v  r12                  -0.0012254       0.0015832       4.247e-07      3.1873e-07
v  r13                  -0.0014775       0.0014146      4.0408e-09     -2.2561e-09
v  r23                 -0.00084514      0.00081156      2.0543e-08      1.3668e-08
v  epsilon              2.7729e-10          1.0267       0.0020449       0.0017611
v  TurbVisc              0.0014205      1.5402e+05          3.8624          4.2816
v  CourantNb             6.327e-07               1         0.11222          0.1037
v  FourierNb             0.0001795               1          0.2804         0.25965
v  total_pressure      -3.9061e+06      9.6487e+05       4.671e+05      4.7606e+05
v  Local Time Step      2.8717e-09      1.4641e-05       1.458e-05      1.4565e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00042763           1.719         0.39262         0.36334


 TIME FOR THE TIME STEP                4:        0.43898E+02

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


 INSTANT    0.500000000E-04   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.912911423E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392540256E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14378E-02 0.41996E+02
   Friction velocity        uet   :  0.13805E-03 0.39189E+01
   Friction velocity        uk    :  0.13232E-01 0.11699E+00
   Dimensionless distance   yplus :  0.18535E+02 0.40077E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.63109E+04       4   0.36638E-02   0.18148E+04 0.20936E+04 
c  Velocity[X]                                      0.47213E+03 
c  Velocity[Y]                                      0.93094E+03 
c  Velocity[Z]                                      0.41170E+03 
c  Pressure     0.22227E+00      93   0.30347E-02   0.17931E+00 0.33091E+06 
c  r11          0.10106E+01       6   0.19179E-03   0.53675E-02 0.10455E+05 
c  r22          0.10068E+01       6   0.17519E-03   0.46969E-02 0.10209E+05 
c  r33          0.10063E+01       6   0.17499E-03   0.46901E-02 0.10205E+05 
c  r12          0.66503E-02      13   0.12905E-02   0.10292E-04 0.19480E+05 
c  r13          0.63704E-02      11   0.12486E-02   0.97134E-05 0.19281E+05 
c  r23          0.22621E-02      14   0.19378E-02   0.17039E-05 0.23106E+05 
c  epsilon      0.48487E+01       6   0.63511E-03   0.24371E+01 0.11888E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -1.5544e-05                           141
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -51.796          58.094          3.8736          3.8138
v  Velocity[Y]             -15.257          64.048         0.11029        0.040149
v  Velocity[Z]             -50.603          52.704      -0.0051116      3.8073e-05
v  ǁVelocityǁ            0.0020996          76.591          4.9519          4.8143
v  Pressure            -4.0358e+06      9.5739e+05      3.6657e+05      3.7554e+05
v  r11                  0.00026015        0.052999      0.00052019      0.00050406
v  r22                  0.00019607        0.050368      0.00051615      0.00050069
v  r33                  0.00024458        0.050962      0.00051609      0.00050063
v  r12                  -0.0018629       0.0022806      6.7511e-07      5.1651e-07
v  r13                  -0.0022712       0.0020692        5.33e-09     -3.7631e-09
v  r23                  -0.0013146       0.0011967      3.1312e-08      2.1025e-08
v  epsilon              9.5921e-11          1.4373       0.0025216       0.0021792
v  TurbVisc               0.001441      1.1691e+05          4.2787          4.8518
v  CourantNb            7.0123e-07               1         0.12322          0.1139
v  FourierNb             0.0002146               1         0.30708         0.28441
v  total_pressure      -3.9345e+06      1.0587e+06      4.6789e+05      4.7687e+05
v  Local Time Step      2.9029e-09      1.6105e-05      1.6003e-05      1.5976e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00046673          1.8853         0.43031         0.39831


 TIME FOR THE TIME STEP                5:        0.43573E+02

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


 INSTANT    0.600000000E-04   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.200854383E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392539153E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.73080E-03 0.40233E+02
   Friction velocity        uet   :  0.69896E-04 0.37815E+01
   Friction velocity        uk    :  0.13231E-01 0.12664E+00
   Dimensionless distance   yplus :  0.18535E+02 0.43415E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26222E+05       3   0.82000E-03   0.15212E+04 0.20327E+04 
c  Velocity[X]                                      0.38112E+03 
c  Velocity[Y]                                      0.80804E+03 
c  Velocity[Z]                                      0.33200E+03 
c  Pressure     0.18975E+00     127   0.30219E-02   0.14496E+00 0.40766E+07 
c  r11          0.20799E+01       5   0.10344E-03   0.51559E-02 0.84034E+04 
c  r22          0.20836E+01       5   0.94586E-04   0.45691E-02 0.82862E+04 
c  r33          0.20869E+01       5   0.94262E-04   0.45625E-02 0.82837E+04 
c  r12          0.82541E-02      13   0.11662E-02   0.95320E-05 0.13662E+05 
c  r13          0.84716E-02      11   0.10450E-02   0.87437E-05 0.13401E+05 
c  r23          0.48574E-02      14   0.11106E-02   0.20170E-05 0.16991E+05 
c  epsilon      0.53157E+01       6   0.65517E-03   0.25806E+01 0.97737E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -6.2338e-06                            99
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -52.098          56.907          3.8742          3.8144
v  Velocity[Y]             -15.271          63.955         0.10884        0.039934
v  Velocity[Z]             -50.324          51.379      -0.0050909      2.6304e-05
v  ǁVelocityǁ            0.0029486          77.417          4.9551          4.8185
v  Pressure            -3.9732e+06      1.8307e+06      3.4939e+05      3.5802e+05
v  r11                  0.00016719        0.057774      0.00054631      0.00052711
v  r22                  0.00019005        0.055189      0.00054108      0.00052272
v  r33                  0.00016474        0.055837      0.00054098      0.00052263
v  r12                  -0.0026183       0.0029797      9.8245e-07      7.6372e-07
v  r13                  -0.0031026       0.0027815      6.2708e-09     -5.8227e-09
v  r23                  -0.0017955        0.001553      4.2613e-08      2.8461e-08
v  epsilon              5.6045e-12          1.9147       0.0030524       0.0026473
v  TurbVisc              0.0014635      3.3779e+05          5.7747           6.885
v  CourantNb            7.7861e-07               1         0.13528         0.12508
v  FourierNb            0.00022041          1.1154         0.33523         0.31004
v  total_pressure      -3.8719e+06       1.932e+06      4.5072e+05      4.5935e+05
v  Local Time Step           1e-09      1.7716e-05      1.7565e-05      1.7522e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00065881          1.9124         0.47051         0.43512


 TIME FOR THE TIME STEP                6:        0.43643E+02

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


 INSTANT    0.700000000E-04   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.172599465E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392550732E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.37765E-03 0.39523E+02
   Friction velocity        uet   :  0.36120E-04 0.37141E+01
   Friction velocity        uk    :  0.13231E-01 0.13504E+00
   Dimensionless distance   yplus :  0.18534E+02 0.46333E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42857E+05       4   0.46693E-03   0.34596E+04 0.12780E+05 
c  Velocity[X]                                      0.84965E+03 
c  Velocity[Y]                                      0.17635E+04 
c  Velocity[Z]                                      0.84639E+03 
c  Pressure     0.19331E+00     133   0.15208E-01   0.14499E+00 0.78209E+08 
c  r11          0.47447E+01       5   0.48045E-04   0.49385E-02 0.68738E+04 
c  r22          0.47408E+01       5   0.44566E-04   0.44580E-02 0.68503E+04 
c  r33          0.47408E+01       5   0.44482E-04   0.44518E-02 0.68487E+04 
c  r12          0.11299E-01      13   0.85776E-03   0.78415E-05 0.97089E+04 
c  r13          0.96907E-02      11   0.91024E-03   0.68787E-05 0.93737E+04 
c  r23          0.59856E-02      14   0.10014E-02   0.21182E-05 0.12697E+05 
c  epsilon      0.60512E+01       6   0.62845E-03   0.27394E+01 0.81973E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -8.6032e-06                            82
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -51.469          55.056          3.8748           3.815
v  Velocity[Y]             -36.735          110.68         0.10734        0.039659
v  Velocity[Z]             -66.463          50.785      -0.0051055      1.4937e-05
v  ǁVelocityǁ            0.0026077          131.71           4.959          4.8237
v  Pressure            -4.5141e+07       2.072e+07       3.357e+05      3.4409e+05
v  r11                  0.00012974        0.061374      0.00057471      0.00055238
v  r22                  0.00018362           0.059      0.00056833      0.00054698
v  r33                  0.00012773        0.059704      0.00056818      0.00054686
v  r12                  -0.0034246       0.0038761      1.3459e-06      1.0607e-06
v  r13                   -0.003886        0.003598      6.7347e-09     -8.4334e-09
v  r23                  -0.0022309       0.0018301      5.3783e-08       3.524e-08
v  epsilon              3.5178e-14          2.4465        0.003641       0.0031696
v  TurbVisc              0.0014885      5.7811e+06          16.445          20.303
v  CourantNb            8.8342e-07               1         0.14846         0.13736
v  FourierNb            0.00027101          13.598         0.36537         0.33705
v  total_pressure      -4.5039e+07      2.0821e+07      4.3702e+05      4.4542e+05
v  Local Time Step           1e-09      1.9487e-05      1.9281e-05       1.922e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00065671          13.598         0.51384         0.47441


 TIME FOR THE TIME STEP                7:        0.45459E+02

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


 INSTANT    0.800000000E-04   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.654308577E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392550299E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.53225E-03 0.38919E+02
   Friction velocity        uet   :  0.50908E-04 0.36486E+01
   Friction velocity        uk    :  0.13232E-01 0.14235E+00
   Dimensionless distance   yplus :  0.18533E+02 0.48876E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71633E+05       3   0.26871E-03   0.67564E+06 0.19423E+06 
c  Velocity[X]                                      0.12464E+06 
c  Velocity[Y]                                      0.39134E+06 
c  Velocity[Z]                                      0.15966E+06 
c  Pressure     0.42904E+00     152   0.25550E+00   0.31567E+00 0.82713E+09 
c  r11          0.92672E+01       5   0.24951E-04   0.47382E-02 0.57147E+04 
c  r22          0.92668E+01       5   0.23519E-04   0.43680E-02 0.57529E+04 
c  r33          0.92686E+01       5   0.23467E-04   0.43621E-02 0.57518E+04 
c  r12          0.17913E-01      13   0.50510E-03   0.60413E-05 0.70557E+04 
c  r13          0.16643E-01      11   0.48354E-03   0.49539E-05 0.66397E+04 
c  r23          0.10207E-01      13   0.67541E-03   0.20256E-05 0.96068E+04 
c  epsilon      0.74851E+01       6   0.53843E-03   0.29059E+01 0.69720E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -6.6784e-06                            80
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -921.47          609.94          3.8733          3.8134
v  Velocity[Y]             -2572.5           477.3         0.10374        0.038594
v  Velocity[Z]             -328.41          1583.6      -0.0030455       0.0013051
v  ǁVelocityǁ            0.0040636          3100.4          4.9788          4.8462
v  Pressure            -1.9598e+08      9.8159e+08      3.2994e+05      3.3789e+05
v  r11                   0.0001494        0.063974      0.00060543      0.00057994
v  r22                   0.0001713         0.06192      0.00059801      0.00057361
v  r33                  0.00010875        0.062666      0.00059782      0.00057345
v  r12                  -0.0042446        0.004765       1.764e-06      1.4077e-06
v  r13                  -0.0045399       0.0044738      6.2587e-09     -1.1774e-08
v  r23                  -0.0025719       0.0020963      6.4068e-08      4.0499e-08
v  epsilon              3.8696e-14          3.0591       0.0042915       0.0037503
v  TurbVisc              0.0015127      9.2097e+08          873.23          780.21
v  CourantNb            5.3013e-07               1         0.16286         0.15082
v  FourierNb            0.00029785          2680.2         0.40274         0.37029
v  total_pressure      -1.9588e+08      9.8169e+08      4.3127e+05      4.3921e+05
v  Local Time Step           1e-09      2.1436e-05      2.1169e-05      2.1092e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0007231          2680.2         0.56561         0.52111


 TIME FOR THE TIME STEP                8:        0.45761E+02

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


 INSTANT    0.900000000E-04   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.760157810E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392546383E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.82527E-03 0.17602E+03
   Friction velocity        uet   :  0.78937E-04 0.15967E+02
   Friction velocity        uk    :  0.12978E-01 0.14869E+00
   Dimensionless distance   yplus :  0.18531E+02 0.51084E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10823E+06       3   0.84773E-02   0.67227E+08 0.90181E+06 
c  Velocity[X]                                      0.18410E+08 
c  Velocity[Y]                                      0.34148E+08 
c  Velocity[Z]                                      0.14670E+08 
c  Pressure     0.62274E+01     165   0.38043E+00   0.10315E+01 0.10434E+10 
c  r11          0.12616E+02       6   0.18116E-04   0.45701E-02 0.48253E+04 
c  r22          0.12613E+02       6   0.17802E-04   0.42977E-02 0.48993E+04 
c  r33          0.12613E+02       6   0.17458E-04   0.42919E-02 0.48955E+04 
c  r12          0.52199E-01      14   0.25056E-03   0.48696E-05 0.67078E+04 
c  r13          0.50723E-01      14   0.22540E-03   0.36728E-05 0.54308E+04 
c  r23          0.19847E-01      16   0.81144E-03   0.19100E-05 0.11766E+05 
c  epsilon      0.86936E+01      12   0.48037E-03   0.30759E+01 0.59912E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -6.9422e-06                            71
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -6943.1           11524          3.8922           3.833
v  Velocity[Y]             -6047.6            7004         0.09374        0.022942
v  Velocity[Z]             -4855.8          6334.7       -0.022458       -0.010897
v  ǁVelocityǁ            0.0043802           13014           5.148          5.0232
v  Pressure            -1.7072e+10      1.7009e+09      3.1508e+05      3.2772e+05
v  r11                  3.8532e-06          0.0658      0.00063856      0.00060992
v  r22                  4.0246e-06        0.064157      0.00063024      0.00060276
v  r33                  1.4897e-05        0.064883      0.00062999      0.00060255
v  r12                  -0.0050424       0.0055994      2.2271e-06      1.7959e-06
v  r13                  -0.0053147       0.0053355      5.9489e-09     -1.4029e-08
v  r23                  -0.0027819       0.0022399      7.6585e-08      4.8357e-08
v  epsilon              4.2565e-14          3.7224       0.0050081       0.0043944
v  TurbVisc              0.0015246      8.3724e+08          824.33          755.44
v  CourantNb            4.2706e-07               1         0.17865         0.16564
v  FourierNb            0.00031566          2436.6         0.43763         0.40136
v  total_pressure      -1.7072e+10       1.701e+09      4.1641e+05      4.2904e+05
v  Local Time Step           1e-09      2.3579e-05      2.3244e-05      2.3154e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00082035          2436.6         0.61629           0.567


 TIME FOR THE TIME STEP                9:        0.44688E+02

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


 INSTANT    0.100000000E-03   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.380379235E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392545799E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.10170E-02 0.19820E+04
   Friction velocity        uet   :  0.97276E-04 0.13247E+03
   Friction velocity        uk    :  0.93591E-02 0.15417E+00
   Dimensionless distance   yplus :  0.18532E+02 0.52991E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.16897E+06       6   0.45215E-01   0.15549E+10 0.13790E+07 
c  Velocity[X]                                      0.52207E+09 
c  Velocity[Y]                                      0.61009E+09 
c  Velocity[Z]                                      0.42270E+09 
c  Pressure     0.36308E+02     167   0.26045E+00   0.99786E+00 0.11225E+10 
c  r11          0.16289E+02      13   0.16072E-04   0.44423E-02 0.45273E+04 
c  r22          0.16286E+02      12   0.16820E-04   0.42464E-02 0.44584E+04 
c  r33          0.16284E+02      12   0.15885E-04   0.42396E-02 0.43729E+04 
c  r12          0.54142E-01      27   0.69853E-03   0.63923E-05 0.26623E+05 
c  r13          0.54637E-01      30   0.61440E-03   0.41901E-05 0.24830E+05 
c  r23          0.27778E-01      33   0.14158E-02   0.30872E-05 0.41567E+05 
c  epsilon      0.10171E+02      19   0.42089E-03   0.32491E+01 0.52216E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon              -7.065e-06                            74
a  Local Time Step


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -15479           16541          3.8412          3.7646
v  Velocity[Y]              -16258           16239         0.18006         0.14693
v  Velocity[Z]              -26512           18618        0.029106        0.017483
v  ǁVelocityǁ            0.0014466           35216          6.0073          6.0563
v  Pressure            -4.5908e+10      8.5945e+10      5.1073e+05       5.016e+05
v  r11                  6.5236e-08        0.067158      0.00067408      0.00064234
v  r22                  2.9276e-06        0.065878      0.00066511      0.00063456
v  r33                  5.6474e-07        0.066526      0.00066478      0.00063426
v  r12                  -0.0057863       0.0063368      2.7652e-06      2.2606e-06
v  r13                  -0.0060646       0.0061134      3.0319e-10     -2.1187e-08
v  r23                  -0.0028484       0.0022416      1.0211e-07      7.1712e-08
v  epsilon              4.6822e-14          4.4068       0.0057957       0.0051075
v  TurbVisc             0.00049835      7.6113e+08          825.75          799.47
v  CourantNb            4.2588e-07               1         0.19634         0.18237
v  FourierNb            0.00022265          2215.1          0.4756         0.43549
v  total_pressure      -4.5908e+10      8.5945e+10      6.1206e+05      6.0293e+05
v  Local Time Step           1e-09      2.5937e-05      2.5515e-05      2.5415e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00061126          2215.1         0.67194         0.61785


 TIME FOR THE TIME STEP               10:        0.46137E+02

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


 INSTANT    0.110000000E-03   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.158275612E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392397082E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24261E-02 0.28055E+05
   Friction velocity        uet   :  0.25004E-03 0.21073E+04
   Friction velocity        uk    :  0.10425E-01 0.26388E+00
   Dimensionless distance   yplus :  0.18538E+02 0.54628E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.71784E+06       6   0.21092E+00   0.48093E+11 0.76182E+07 
c  Velocity[X]                                      0.16492E+11 
c  Velocity[Y]                                      0.14069E+11 
c  Velocity[Z]                                      0.17531E+11 
c  Pressure     0.13655E+03     174   0.17799E+00   0.97835E+00 0.93228E+09 
c  r11          0.19432E+02      19   0.15074E-04   0.43719E-02 0.56873E+04 
c  r22          0.19427E+02      25   0.16747E-04   0.42242E-02 0.59730E+04 
c  r33          0.19419E+02      21   0.15812E-04   0.42125E-02 0.60824E+04 
c  r12          0.75962E-01      49   0.10448E-02   0.15770E-04 0.66042E+05 
c  r13          0.76487E-01      50   0.11534E-02   0.11946E-04 0.81097E+05 
c  r23          0.83185E-01      55   0.15186E-02   0.10394E-04 0.17276E+06 
c  epsilon      0.11201E+02      27   0.39031E-03   0.34371E+01 0.46002E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -7.0823e-06                            80
a  Local Time Step      3.1398e-10                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -30506           26100          3.9384          3.8496
v  Velocity[Y]              -33287           40451         -0.0105       -0.051957
v  Velocity[Z]              -30239           26399         0.10534        0.017562
v  ǁVelocityǁ            0.0019194           45052           8.996          9.6615
v  Pressure            -1.6058e+11      7.9766e+11      2.1299e+06      2.8465e+06
v  r11                   7.176e-08        0.068411       0.0007121      0.00067738
v  r22                  2.9191e-07        0.067159       0.0007025      0.00066891
v  r33                   4.115e-07        0.067743      0.00070224      0.00066873
v  r12                  -0.0064488       0.0069739      3.3924e-06      2.8066e-06
v  r13                  -0.0066783       0.0067966      1.8056e-07      1.4869e-07
v  r23                  -0.0029112       0.0026653     -6.0145e-08     -1.1001e-07
v  epsilon              5.1504e-14          5.5359       0.0066601       0.0058966
v  TurbVisc             0.00061478      6.9194e+08          832.49          856.39
v  CourantNb            2.3554e-07               1           0.219         0.20422
v  FourierNb            2.5637e-05          2013.7         0.51574         0.47177
v  total_pressure      -1.6058e+11      7.9766e+11      2.2312e+06      2.9478e+06
v  Local Time Step           1e-09      2.8531e-05      2.7963e-05      2.7863e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00070432          2013.7         0.73474         0.67599


 TIME FOR THE TIME STEP               11:        0.49354E+02

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


 INSTANT    0.120000000E-03   TIME STEP NUMBER              12
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.742315256E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391744274E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.22675E-02 0.29271E+05
   Friction velocity        uet   :  0.22661E-03 0.18035E+04
   Friction velocity        uk    :  0.10321E-01 0.31010E+00
   Dimensionless distance   yplus :  0.17640E+02 0.66479E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92322E+07       6   0.13283E+00   0.15800E+12 0.82353E+07 
c  Velocity[X]                                      0.56261E+11 
c  Velocity[Y]                                      0.54434E+11 
c  Velocity[Z]                                      0.47309E+11 
c  Pressure     0.26829E+03     170   0.12994E+00   0.10200E+01 0.13067E+10 
c  r11          0.21701E+02      21   0.15425E-04   0.44007E-02 0.75327E+04 
c  r22          0.21709E+02      22   0.14379E-04   0.42918E-02 0.79495E+04 
c  r33          0.21711E+02      23   0.15620E-04   0.43210E-02 0.10362E+05 
c  r12          0.11691E+00      47   0.13251E-02   0.45686E-04 0.13446E+06 
c  r13          0.11988E+00      39   0.90602E-03   0.50066E-04 0.18476E+06 
c  r23          0.16134E+00      40   0.10245E-02   0.54627E-04 0.38944E+06 
c  epsilon      0.12494E+02      40   0.36127E-03   0.36730E+01 0.43085E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11            
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -7.5575e-06                            85
a  Local Time Step      3.4538e-10                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -34117           46272          4.2799          4.3115
v  Velocity[Y]              -49177           33872       0.0044488       -0.068512
v  Velocity[Z]              -24590           47978        0.059977          0.2212
v  ǁVelocityǁ             0.026956           68641          13.048          14.687
v  Pressure            -1.1787e+12      4.0688e+11       1.416e+05     -6.3758e+05
v  r11                  8.5063e-07        0.069573      0.00075276      0.00071511
v  r22                   3.211e-07        0.068036      0.00074309      0.00070659
v  r33                  1.0974e-07        0.068629      0.00074254      0.00070602
v  r12                   -0.006977       0.0074928      4.5801e-06       3.878e-06
v  r13                  -0.0077072       0.0074898     -1.5066e-07      -1.398e-07
v  r23                  -0.0030109       0.0030978     -6.2986e-08     -8.4636e-08
v  epsilon              5.6654e-14          6.7557       0.0076102       0.0067713
v  TurbVisc             0.00011102      6.2903e+08          1203.2            1180
v  CourantNb            4.5968e-08               1         0.27265         0.25696
v  FourierNb            7.2478e-06          1830.6         0.55476         0.50721
v  total_pressure      -1.1787e+12      4.0688e+11      2.4292e+05     -5.3625e+05
v  Local Time Step           1e-09      3.1384e-05      3.0385e-05      3.0305e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier       0.0010345          1830.6         0.82741         0.76417


 TIME FOR THE TIME STEP               12:        0.50465E+02

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


 INSTANT    0.130000000E-03   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.134708898E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391392230E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27552E-02 0.18396E+05
   Friction velocity        uet   :  0.27244E-03 0.14452E+04
   Friction velocity        uk    :  0.10512E-01 0.35316E+00
   Dimensionless distance   yplus :  0.19563E+02 0.77755E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10362E+08       7   0.13829E+00   0.26565E+12 0.10270E+08 
c  Velocity[X]                                      0.97952E+11 
c  Velocity[Y]                                      0.88602E+11 
c  Velocity[Z]                                      0.79097E+11 
c  Pressure     0.39201E+03     172   0.10788E+00   0.10217E+01 0.12113E+10 
c  r11          0.23171E+02      23   0.28505E-04   0.47883E-02 0.95078E+04 
c  r22          0.23307E+02      23   0.10264E-02   0.22130E+00 0.12159E+06 
c  r33          0.23311E+02      22   0.10224E-02   0.17760E-01 0.35975E+05 
c  r12          0.32052E+00      39   0.47581E-02   0.22390E-03 0.20249E+06 
c  r13          0.27920E+00      42   0.66432E-02   0.15305E-03 0.24660E+06 
c  r23          0.15128E+01      36   0.91195E-02   0.37246E-03 0.63027E+06 
c  epsilon      0.13236E+02      29   0.79294E-03   0.42064E+01 0.46200E+04 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                 -9.9629e-05                             1
a  r22            
a  r33            
a  r12            
a  r13            
a  r23            
a  epsilon             -7.2891e-06                            81
a  Local Time Step      1.3179e-10                             6


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -52647           19998           3.807          3.5402
v  Velocity[Y]              -28916           32587        0.037014       -0.013373
v  Velocity[Z]              -30301           28483       -0.038463       -0.034326
v  ǁVelocityǁ             0.028072           53479          19.981          22.418
v  Pressure            -1.7511e+12      3.7851e+11     -9.4162e+05      -3.193e+06
v  r11                  4.5406e-08        0.070559      0.00079603      0.00075583
v  r22                  4.5373e-08         0.47772      0.00078689      0.00074784
v  r33                  5.0166e-07        0.092996      0.00078595      0.00074684
v  r12                  -0.0074825       0.0094417      5.7195e-06      4.9192e-06
v  r13                  -0.0074592       0.0078795      1.1232e-06      9.4421e-07
v  r23                   -0.010474       0.0075726       8.222e-08      8.1366e-08
v  epsilon               6.232e-14          8.0023       0.0086474       0.0077404
v  TurbVisc              0.0001178      5.7185e+08          1091.3          1082.1
v  CourantNb            2.5352e-07               1         0.33445         0.31757
v  FourierNb             1.343e-06          1664.2         0.58789         0.53757
v  total_pressure      -1.7511e+12      3.7851e+11      -8.403e+05     -3.0917e+06
v  Local Time Step           1e-09      3.4523e-05        3.28e-05       3.277e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00027739          1664.2         0.92234         0.85514


 TIME FOR THE TIME STEP               13:        0.49753E+02

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


 INSTANT    0.140000000E-03   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.419472969E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.396407477E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.11754E-01 0.41605E+05
   Friction velocity        uet   :  0.11797E-02 0.32169E+04
   Friction velocity        uk    :  0.10150E-01 0.33872E+00
   Dimensionless distance   yplus :  0.19586E+02 0.81398E+03
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15435E+08       7   0.10648E+00   0.28949E+12 0.87771E+07 
c  Velocity[X]                                      0.94264E+11 
c  Velocity[Y]                                      0.86516E+11 
c  Velocity[Z]                                      0.10871E+12 
c  Pressure     0.39552E+03     185   0.10985E+00   0.10062E+01 0.16530E+10 
c  r11          0.24534E+02      22   0.53210E-03   0.55315E-02 0.12572E+05 
c  r22          0.24670E+02      20   0.21253E-02   0.29689E-01 0.46985E+05 
c  r33          0.24644E+02      21   0.42635E-02   0.28614E-01 0.61676E+05 
c  r12          0.94877E+00      36   0.32631E-01   0.91828E-02 0.47884E+06 
c  r13          0.84873E+00      33   0.44093E-01   0.86887E-03 0.18781E+06 
c  r23          0.16212E+01      33   0.64938E-01   0.88662E-03 0.67378E+06 
c  epsilon      0.80114E+02      27   0.61724E-01   0.35012E+03 0.17416E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0019302                            13
a  r22                 -0.00099665                             6
a  r33                 -0.00065053                             8
a  r12                  -0.0008571                            17
a  r13                  -0.0013272                            16
a  r23                 -0.00036966                            15
a  epsilon              -7.743e-05                            68
a  Local Time Step      4.1791e-10                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -74396           69594          4.4191          4.1665
v  Velocity[Y]              -28304           97822          0.4764           0.437
v  Velocity[Z]              -62746           51040        -0.11817        -0.21236
v  ǁVelocityǁ             0.046196      1.2944e+05          25.536          28.806
v  Pressure              -1.27e+12      4.9764e+11     -5.3951e+05       4.644e+05
v  r11                  8.2064e-08        0.072079      0.00084303      0.00080056
v  r22                  3.6025e-07         0.59691        0.000834      0.00079284
v  r33                  1.3579e-08         0.16692      0.00083304      0.00079168
v  r12                   -0.017788         0.10333      1.4916e-06      1.3535e-06
v  r13                   -0.013278        0.015347      4.8064e-06       4.015e-06
v  r23                    -0.01228        0.013015      2.6831e-07      1.6865e-07
v  epsilon              6.8552e-14          19.838       0.0098015       0.0088311
v  TurbVisc             0.00014486      5.1986e+08            1010          1013.3
v  CourantNb            6.3734e-08               1         0.44261         0.42621
v  FourierNb            1.4582e-06          1512.9          0.6041         0.55426
v  total_pressure        -1.27e+12      4.9764e+11     -4.3819e+05      5.6572e+05
v  Local Time Step           1e-09      3.7975e-05      3.4403e-05      3.4521e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00019716          1512.9          1.0467         0.98047


 TIME FOR THE TIME STEP               14:        0.51930E+02

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


 INSTANT    0.150000000E-03   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.895044782E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.389672752E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.30874E-01 0.75395E+05
   Friction velocity        uet   :  0.30887E-02 0.53680E+04
   Friction velocity        uk    :  0.91447E-02 0.74284E+00
   Dimensionless distance   yplus :  0.19455E+02 0.13111E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.17763E+08       8   0.12387E+00   0.49784E+12 0.84260E+07 
c  Velocity[X]                                      0.17151E+12 
c  Velocity[Y]                                      0.15091E+12 
c  Velocity[Z]                                      0.17542E+12 
c  Pressure     0.49064E+03     195   0.16678E+00   0.10083E+01 0.11527E+10 
c  r11          0.24275E+02      31   0.35509E-03   0.11278E-01 0.25780E+05 
c  r22          0.24240E+02      30   0.35805E-03   0.25703E-01 0.34298E+05 
c  r33          0.24982E+02      30   0.54397E-03   0.17258E+00 0.13259E+06 
c  r12          0.24075E+01      34   0.24801E-02   0.62400E-02 0.25177E+06 
c  r13          0.29086E+01      33   0.23377E-02   0.27614E-02 0.20812E+06 
c  r23          0.21778E+01      36   0.26556E-02   0.53595E-02 0.70329E+06 
c  epsilon      0.61670E+02      39   0.42987E-03   0.21001E+02 0.29652E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0021229                            12
a  r22                 -0.00092466                            10
a  r33                  -0.0011259                            12
a  r12                 -0.00044346                            23
a  r13                 -0.00040994                            15
a  r23                 -0.00045043                            30
a  epsilon             -0.00096221                            64
a  Local Time Step       4.597e-10                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -72088      1.0507e+05          4.1762          4.4278
v  Velocity[Y]              -73180           64329         0.16752         0.47241
v  Velocity[Z]              -70256      1.0488e+05          0.5279         0.49031
v  ǁVelocityǁ             0.066263      1.4111e+05          38.076          43.509
v  Pressure            -1.5823e+12      1.5823e+12      -6.315e+06     -5.4602e+06
v  r11                  1.3811e-07         0.09474      0.00089426      0.00084992
v  r22                  9.0204e-10         0.44611      0.00088718      0.00084391
v  r33                  5.0479e-08         0.32521      0.00088659      0.00084303
v  r12                   -0.023438            0.18     -2.3852e-06     -2.0924e-06
v  r13                   -0.015906         0.04416      1.0767e-05      9.2822e-06
v  r23                   -0.089689        0.014463      1.2627e-07      6.9689e-08
v  epsilon              7.5407e-14          21.182         0.01112         0.01008
v  TurbVisc             3.9597e-05       4.726e+08          563.19          563.76
v  CourantNb            2.9565e-07               1         0.50384         0.48995
v  FourierNb            1.6418e-06          1375.4         0.61873         0.56994
v  total_pressure      -1.5823e+12      1.5823e+12     -6.2136e+06     -5.3589e+06
v  Local Time Step           1e-09      4.1772e-05      3.6138e-05      3.6442e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00017468          1375.4          1.1226          1.0599


 TIME FOR THE TIME STEP               15:        0.51453E+02

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


 INSTANT    0.160000000E-03   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.119751701E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.398806052E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12384E-01 0.59976E+05
   Friction velocity        uet   :  0.12604E-02 0.41613E+04
   Friction velocity        uk    :  0.90584E-02 0.61912E+00
   Dimensionless distance   yplus :  0.20174E+02 0.19496E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.34386E+08       7   0.16898E+00   0.12549E+13 0.19261E+08 
c  Velocity[X]                                      0.42586E+12 
c  Velocity[Y]                                      0.40017E+12 
c  Velocity[Z]                                      0.42890E+12 
c  Pressure     0.79921E+03     182   0.75687E-01   0.10136E+01 0.12542E+10 
c  r11          0.23548E+02      29   0.45988E-03   0.11742E-01 0.26507E+05 
c  r22          0.23714E+02      27   0.52604E-03   0.42124E-01 0.42759E+05 
c  r33          0.25678E+02      26   0.79283E-03   0.81262E-01 0.13546E+06 
c  r12          0.16874E+01      39   0.69886E-02   0.36139E-02 0.23607E+06 
c  r13          0.13493E+01      41   0.15402E-01   0.67505E-02 0.52209E+06 
c  r23          0.24556E+01      36   0.35431E-02   0.19105E-01 0.16052E+07 
c  epsilon      0.59803E+02      26   0.84137E-03   0.94734E+02 0.74899E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                 -0.00011138                             6
a  r22                 -0.00059451                             8
a  r33                 -0.00073107                             8
a  r12                 -0.00057651                            26
a  r13                 -0.00038631                            29
a  r23                 -0.00048358                            20
a  epsilon              -0.0011326                           102
a  Local Time Step      8.5433e-11                            13


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -70196           43722          3.7667           3.545
v  Velocity[Y]              -48275           38462        -0.30966        -0.36749
v  Velocity[Z]              -76037           38502        -0.49286        -0.72636
v  ǁVelocityǁ             0.070626           95692          47.502          54.099
v  Pressure            -9.5584e+11      2.9826e+12      2.1473e+06       7.102e+05
v  r11                   1.054e-08         0.10711       0.0009511      0.00090566
v  r22                  8.0605e-08         0.24581      0.00094736      0.00090256
v  r33                  5.5142e-08         0.47032      0.00094728      0.00090218
v  r12                   -0.028705         0.16226     -5.7222e-06       -5.18e-06
v  r13                   -0.018106        0.060174      1.6458e-05      1.4537e-05
v  r23                   -0.056884        0.051481      1.6153e-07      1.7304e-07
v  epsilon              8.2947e-14          14.653        0.012625        0.011521
v  TurbVisc             8.4411e-05      4.2964e+08          445.82          434.35
v  CourantNb            6.4907e-07               1         0.57537         0.56678
v  FourierNb            5.0712e-07          1250.3         0.60677          0.5616
v  total_pressure      -9.5584e+11      2.9826e+12      2.2486e+06      8.1153e+05
v  Local Time Step           1e-09       4.595e-05      3.6272e-05      3.6783e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00016908          1250.3          1.1821          1.1284


 TIME FOR THE TIME STEP               16:        0.49887E+02

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


 INSTANT    0.170000000E-03   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.728154321E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.389100036E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.35245E-01 0.71726E+05
   Friction velocity        uet   :  0.29550E-02 0.44162E+04
   Friction velocity        uk    :  0.95076E-02 0.77910E+00
   Dimensionless distance   yplus :  0.19995E+02 0.17145E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for        105 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.42558E+08       7   0.16551E+00   0.58264E+12 0.12156E+08 
c  Velocity[X]                                      0.18987E+12 
c  Velocity[Y]                                      0.17908E+12 
c  Velocity[Z]                                      0.21369E+12 
c  Pressure     0.48644E+03     180   0.74250E-01   0.93592E+00 0.18056E+10 
c  r11          0.13788E+04       8   0.12410E+00   0.71241E-01 0.20682E+06 
c  r22          0.43704E+04       8   0.10881E+00   0.75144E-01 0.12416E+06 
c  r33          0.57914E+04       7   0.11151E+00   0.84072E+04 0.17205E+09 
c  r12          0.24877E+04       7   0.11616E+00   0.67269E+00 0.21605E+08 
c  r13          0.34472E+04       7   0.12364E+00   0.39320E+02 0.13183E+09 
c  r23          0.52768E+04       7   0.10718E+00   0.36480E+02 0.20408E+09 
c  epsilon      0.29233E+04      11   0.96308E-01   0.30134E+04 0.53791E+07 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0020417                            66
a  r22                  -0.0023616                            43
a  r33                  -0.0039655                            71
a  r12                 -0.00072377                            82
a  r13                 -0.00088542                           108
a  r23                  -0.0005252                            83
a  epsilon              -0.0069282                           336
a  Local Time Step      9.3977e-11                            13


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -29538           32554          3.9032          3.8534
v  Velocity[Y]              -37014           29968        -0.26296        -0.31315
v  Velocity[Z]              -39947           33509        0.022483       -0.079949
v  ǁVelocityǁ             0.038193           46721          52.803            59.4
v  Pressure            -4.0764e+11      8.4532e+11     -1.2496e+07     -1.6749e+07
v  r11                  6.0919e-09         0.33862       0.0010151      0.00096924
v  r22                  4.8428e-09         0.29567       0.0010161       0.0009705
v  r33                  6.9565e-09          7.2513       0.0010232      0.00097599
v  r12                    -0.03872         0.15814     -1.3945e-05     -1.2381e-05
v  r13                    -0.22443         0.48712      2.3689e-05      2.1326e-05
v  r23                    -0.47004        0.068245     -6.5652e-07     -4.1486e-07
v  epsilon              9.1242e-14          19.121        0.014351         0.01319
v  TurbVisc             7.5617e-05      3.9058e+08          393.64          378.28
v  CourantNb            9.8857e-07               1         0.65054         0.64744
v  FourierNb            5.7196e-07          1136.7         0.58535         0.54481
v  total_pressure      -4.0764e+11      8.4532e+11     -1.2395e+07     -1.6648e+07
v  Local Time Step           1e-09      5.0545e-05      3.6064e-05      3.6801e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00016377          1136.7          1.2359          1.1922


 TIME FOR THE TIME STEP               17:        0.46428E+02

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


 INSTANT    0.180000000E-03   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.234087100E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.395697249E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.21388E-01 0.36456E+05
   Friction velocity        uet   :  0.20496E-02 0.26655E+04
   Friction velocity        uk    :  0.91301E-02 0.10475E+01
   Dimensionless distance   yplus :  0.20909E+02 0.29064E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for        293 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.26836E+08       6   0.10968E+00   0.21593E+12 0.78607E+07 
c  Velocity[X]                                      0.63946E+11 
c  Velocity[Y]                                      0.73727E+11 
c  Velocity[Z]                                      0.78257E+11 
c  Pressure     0.34203E+03     165   0.63380E-01   0.81606E+00 0.11835E+10 
c  r11          0.21662E+03      10   0.77489E-02   0.27792E+01 0.14470E+07 
c  r22          0.64979E+03      11   0.60501E-02   0.58672E+01 0.33297E+06 
c  r33          0.35845E+04       9   0.15535E-02   0.71329E+03 0.39094E+08 
c  r12          0.39141E+03      12   0.33354E-02   0.12718E+01 0.27614E+07 
c  r13          0.74880E+03      12   0.10792E-02   0.10619E+02 0.18576E+08 
c  r23          0.99523E+03      11   0.50764E-02   0.17153E+01 0.17732E+08 
c  epsilon      0.83733E+05       9   0.38251E-02   0.70045E+07 0.14734E+09 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0019538                           136
a  r22                  -0.0018676                            90
a  r33                    -0.02167                           106
a  r12                 -0.00083827                           156
a  r13                  -0.0027522                           187
a  r23                  -0.0013354                           148
a  epsilon              -0.0048102                           241
a  Local Time Step      3.2441e-10                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -17954           40841          4.1011          3.9788
v  Velocity[Y]              -19391           22799        -0.29079        -0.37215
v  Velocity[Z]              -41822           42497        0.088355        -0.15914
v  ǁVelocityǁ             0.075295           60601           57.97          64.579
v  Pressure             -5.064e+11      3.2198e+11     -1.3951e+07     -1.7855e+07
v  r11                  6.7011e-09          0.4798       0.0010871       0.0010418
v  r22                  1.3513e-07          2.4961       0.0010993       0.0010538
v  r33                  4.9059e-08          9.4585       0.0011049       0.0010575
v  r12                    -0.12122         0.96424     -2.2045e-05     -1.9468e-05
v  r13                    -0.98659         0.58349       2.819e-05      2.6134e-05
v  r23                    -0.56303          0.7202     -1.6126e-07      1.6182e-07
v  epsilon              1.0037e-13          223.94        0.016652        0.015407
v  TurbVisc             9.3009e-05      3.5507e+08          356.42          341.18
v  CourantNb            9.6701e-07               1         0.69202         0.69224
v  FourierNb            6.1096e-07          1033.3         0.56861         0.53169
v  total_pressure       -5.064e+11      3.2198e+11      -1.385e+07     -1.7754e+07
v  Local Time Step           1e-09      5.5599e-05      3.6056e-05      3.7004e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      9.6112e-05          1033.3          1.2606          1.2239


 TIME FOR THE TIME STEP               18:        0.45416E+02

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


 INSTANT    0.190000000E-03   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.216535367E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.389641596E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.53218E-01 0.18011E+05
   Friction velocity        uet   :  0.51419E-02 0.13385E+04
   Friction velocity        uk    :  0.90617E-02 0.11955E+01
   Dimensionless distance   yplus :  0.20900E+02 0.33171E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for        595 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.20943E+08       6   0.69686E-01   0.11284E+12 0.56729E+07 
c  Velocity[X]                                      0.35173E+11 
c  Velocity[Y]                                      0.32909E+11 
c  Velocity[Z]                                      0.44758E+11 
c  Pressure     0.27421E+03     172   0.57494E-01   0.72476E+00 0.11910E+10 
c  r11          0.92073E+02      14   0.15667E-01   0.18393E+02 0.32780E+07 
c  r22          0.85930E+02      14   0.10319E-01   0.63729E+01 0.75247E+06 
c  r33          0.31470E+04       9   0.36232E-03   0.45649E+02 0.29428E+07 
c  r12          0.60191E+02      14   0.18590E-01   0.36732E+00 0.22935E+07 
c  r13          0.32641E+03      13   0.12787E-01   0.30599E+02 0.14801E+08 
c  r23          0.28977E+03      12   0.49634E-02   0.88687E+01 0.42238E+07 
c  epsilon      0.80085E+05      10   0.39639E-03   0.34633E+06 0.82892E+07 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0036835                            89
a  r22                  -0.0015387                            76
a  r33                    -0.11796                           101
a  r12                  -0.0018513                           210
a  r13                   -0.016715                           159
a  r23                  -0.0028828                           155
a  epsilon               -0.010854                           129
a  Local Time Step      3.5724e-10                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -34631           33561          4.2365           4.062
v  Velocity[Y]              -53904           19718        -0.63293        -0.77852
v  Velocity[Z]              -32172           23105         0.11337        -0.19735
v  ǁVelocityǁ             0.078778           71694          63.466           69.87
v  Pressure            -6.1332e+11      2.5713e+11     -1.5019e+07     -1.8626e+07
v  r11                  7.3712e-09          1.6062       0.0011688       0.0011252
v  r22                  5.8008e-08          1.8313       0.0011885        0.001144
v  r33                  5.8752e-08          9.3772        0.001198       0.0011514
v  r12                    -0.23262          0.5325     -3.1471e-05     -2.8079e-05
v  r13                     -2.3848         0.44689       3.138e-05       2.998e-05
v  r23                    -0.58797           1.716      1.6578e-06      1.6172e-06
v  epsilon               1.104e-13          252.07         0.01952        0.018216
v  TurbVisc             7.3375e-05       3.228e+08          317.68          296.99
v  CourantNb            1.2719e-06               1         0.74212         0.74684
v  FourierNb             5.304e-07           939.4         0.54372         0.50923
v  total_pressure      -6.1332e+11      2.5713e+11     -1.4918e+07     -1.8525e+07
v  Local Time Step           1e-09      6.1159e-05      3.5508e-05      3.6569e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00011011           939.4          1.2858          1.2561


 TIME FOR THE TIME STEP               19:        0.46771E+02

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


 INSTANT    0.200000000E-03   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.893870624E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.396353638E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.40148E-02 0.42889E+05
   Friction velocity        uet   :  0.36364E-03 0.25270E+04
   Friction velocity        uk    :  0.94295E-02 0.11897E+01
   Dimensionless distance   yplus :  0.23611E+02 0.33009E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for        758 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.18213E+08       6   0.67986E-01   0.90935E+11 0.44105E+07 
c  Velocity[X]                                      0.26969E+11 
c  Velocity[Y]                                      0.30592E+11 
c  Velocity[Z]                                      0.33375E+11 
c  Pressure     0.22755E+03     160   0.55530E-01   0.67365E+00 0.13326E+10 
c  r11          0.60302E+02      14   0.34069E-01   0.11223E+02 0.22717E+07 
c  r22          0.56533E+02      13   0.87595E-01   0.14576E+02 0.13822E+07 
c  r33          0.28165E+04      10   0.22141E-02   0.75474E+02 0.29726E+07 
c  r12          0.44841E+02      14   0.54280E-01   0.17675E+01 0.36811E+07 
c  r13          0.18732E+03      14   0.21870E-01   0.77979E+01 0.14860E+08 
c  r23          0.21496E+03      11   0.61351E-02   0.78834E+01 0.22833E+08 
c  epsilon      0.75484E+05      12   0.33398E-02   0.10085E+07 0.28543E+07 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0033722                            87
a  r22                   -0.010376                            57
a  r33                    -0.29451                            80
a  r12                  -0.0018875                           172
a  r13                    -0.04532                           128
a  r23                  -0.0015974                           137
a  epsilon              -0.0081774                           109
a  Local Time Step      3.9282e-10                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -41834           47191          4.1071          3.8889
v  Velocity[Y]              -29238           28306        -0.51667         -0.5525
v  Velocity[Z]              -45270           29784       -0.072244        -0.35267
v  ǁVelocityǁ             0.042242           54547          68.289           74.63
v  Pressure            -2.1867e+11       3.709e+11     -1.6698e+07     -1.9417e+07
v  r11                  1.7918e-08         0.70226       0.0012582       0.0012182
v  r22                  8.6571e-10          1.7614       0.0012884       0.0012466
v  r33                   2.357e-08          9.2158       0.0013048       0.0012598
v  r12                    -0.61243         0.21743     -4.3042e-05     -3.8758e-05
v  r13                     -1.8626         0.37012      3.4833e-05      3.3915e-05
v  r23                    -0.74798          1.2474      1.1711e-06      1.2775e-06
v  epsilon              1.2144e-13          615.96        0.023216        0.021741
v  TurbVisc             4.0125e-05      2.9345e+08          294.51          275.69
v  CourantNb            1.5632e-06               1          0.7728         0.77885
v  FourierNb            6.3749e-07             854         0.51317         0.48061
v  total_pressure      -2.1867e+11       3.709e+11     -1.6597e+07     -1.9315e+07
v  Local Time Step           1e-09      6.7275e-05      3.4368e-05      3.5525e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010941             854           1.286          1.2595


 TIME FOR THE TIME STEP               20:        0.46403E+02

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


 INSTANT    0.210000000E-03   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.199327440E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392375074E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.54071E-01 0.18575E+05
   Friction velocity        uet   :  0.53556E-02 0.10273E+04
   Friction velocity        uk    :  0.97249E-02 0.11771E+01
   Dimensionless distance   yplus :  0.22578E+02 0.32661E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for        955 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.15774E+08       6   0.54162E-01   0.90550E+11 0.54174E+07 
c  Velocity[X]                                      0.29543E+11 
c  Velocity[Y]                                      0.28362E+11 
c  Velocity[Z]                                      0.32645E+11 
c  Pressure     0.25782E+03     178   0.52872E-01   0.74436E+00 0.98183E+09 
c  r11          0.28455E+02      29   0.29102E-02   0.26097E+01 0.91166E+06 
c  r22          0.64249E+02      18   0.11577E-01   0.91020E+01 0.96523E+06 
c  r33          0.25178E+04       9   0.34371E-03   0.21182E+02 0.24640E+07 
c  r12          0.13611E+02      29   0.10737E-02   0.18061E+00 0.11221E+07 
c  r13          0.82362E+02      14   0.28411E-02   0.44044E+01 0.75831E+07 
c  r23          0.13111E+03      12   0.14573E-02   0.59074E+01 0.49471E+07 
c  epsilon      0.70466E+05      10   0.48594E-03   0.21179E+06 0.11740E+07 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0030861                            73
a  r22                  -0.0028453                            28
a  r33                    -0.25475                            54
a  r12                  -0.0019136                            89
a  r13                   -0.057989                           110
a  r23                  -0.0014415                            83
a  epsilon               -0.021711                            63
a  Local Time Step      3.1734e-10                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -13767           12435          4.0316          3.7486
v  Velocity[Y]              -35091           28740        -0.53892        -0.70908
v  Velocity[Z]              -13857           39937       -0.059608        -0.28099
v  ǁVelocityǁ              0.04951           44184          74.096          80.346
v  Pressure            -2.6038e+11      4.0989e+11     -1.7897e+07     -2.0543e+07
v  r11                   2.492e-08          1.1179       0.0013573        0.001322
v  r22                  8.9614e-08          3.1283       0.0014003       0.0013626
v  r33                  1.8832e-08          9.0324       0.0014183       0.0013775
v  r12                    -0.46152         0.20537     -5.8009e-05     -5.2495e-05
v  r13                     -1.3195         0.36219      3.5447e-05      3.5398e-05
v  r23                     -0.7081         0.18432      4.1034e-07      7.9969e-07
v  epsilon              1.3359e-13          1118.8        0.027175        0.025727
v  TurbVisc             6.0546e-05      2.6677e+08          266.43          251.99
v  CourantNb            1.1241e-06               1         0.79212         0.79899
v  FourierNb            2.8732e-07          776.36         0.48248         0.45086
v  total_pressure      -2.6038e+11      4.0989e+11     -1.7796e+07     -2.0442e+07
v  Local Time Step           1e-09      7.4002e-05      3.3411e-05      3.4569e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00011108          776.36          1.2746          1.2498


 TIME FOR THE TIME STEP               21:        0.46608E+02

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


 INSTANT    0.220000000E-03   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.162285241E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391534691E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.10674E+00 0.14342E+05
   Friction velocity        uet   :  0.10127E-01 0.82378E+03
   Friction velocity        uk    :  0.91258E-02 0.11652E+01
   Dimensionless distance   yplus :  0.23145E+02 0.32331E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1138 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.14742E+08       6   0.51951E-01   0.72527E+11 0.38126E+07 
c  Velocity[X]                                      0.21098E+11 
c  Velocity[Y]                                      0.26149E+11 
c  Velocity[Z]                                      0.25280E+11 
c  Pressure     0.22508E+03     206   0.58182E-01   0.73044E+00 0.14303E+10 
c  r11          0.29292E+02      24   0.55776E-03   0.92399E+00 0.37428E+06 
c  r22          0.51676E+02      19   0.18015E-02   0.40061E+01 0.67614E+06 
c  r33          0.22499E+04       9   0.30831E-04   0.14800E+02 0.21798E+07 
c  r12          0.71090E+01      21   0.19357E-02   0.40445E+00 0.13624E+07 
c  r13          0.54735E+02      12   0.56394E-03   0.33893E+01 0.71928E+07 
c  r23          0.12003E+03      12   0.48994E-03   0.99010E+00 0.24928E+07 
c  epsilon      0.65990E+05      10   0.72705E-04   0.37075E+06 0.53304E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0070481                           111
a  r22                     -0.0059                            56
a  r33                    -0.22974                            80
a  r12                  -0.0022268                            93
a  r13                   -0.057728                           130
a  r23                  -0.0033467                           116
a  epsilon               -0.063903                           199
a  Local Time Step      8.0911e-10                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -38603           18651          4.0868          3.8167
v  Velocity[Y]              -41155           17917        -0.83074         -1.0546
v  Velocity[Z]              -34675           42919       -0.090885        -0.37072
v  ǁVelocityǁ              0.11039           54232          78.889          85.193
v  Pressure            -3.4403e+11      1.5364e+11     -1.2214e+07     -1.4031e+07
v  r11                   5.436e-08           1.651       0.0014665       0.0014369
v  r22                  4.5304e-08          2.6947       0.0015234       0.0014909
v  r33                  1.6303e-07          8.8331       0.0015435       0.0015081
v  r12                    -0.25193         0.21698     -7.7412e-05     -7.0629e-05
v  r13                    -0.92759         0.35045      3.3751e-05      3.4944e-05
v  r23                    -0.89612         0.23423      1.4949e-06      1.8886e-06
v  epsilon              1.4695e-13            2795        0.032755         0.03118
v  TurbVisc             7.2877e-05      2.4252e+08          240.08          224.81
v  CourantNb            1.0771e-06               1         0.81862         0.82587
v  FourierNb            4.9984e-07          705.77         0.44996         0.41948
v  total_pressure      -3.4403e+11      1.5364e+11     -1.2113e+07      -1.393e+07
v  Local Time Step           1e-09      8.1403e-05      3.2011e-05      3.3169e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      8.8865e-05          705.77          1.2686          1.2454


 TIME FOR THE TIME STEP               22:        0.47521E+02

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


 INSTANT    0.230000000E-03   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.129795710E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.390874630E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.14454E+00 0.28276E+05
   Friction velocity        uet   :  0.14829E-01 0.20397E+04
   Friction velocity        uk    :  0.94301E-02 0.11522E+01
   Dimensionless distance   yplus :  0.23363E+02 0.31971E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1350 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13157E+08       6   0.66244E-01   0.84793E+11 0.58558E+07 
c  Velocity[X]                                      0.22112E+11 
c  Velocity[Y]                                      0.31271E+11 
c  Velocity[Z]                                      0.31410E+11 
c  Pressure     0.24808E+03     186   0.53034E-01   0.77561E+00 0.11558E+10 
c  r11          0.34719E+02      27   0.15086E-02   0.12476E+01 0.33451E+06 
c  r22          0.51787E+02      25   0.72007E-01   0.23507E+01 0.54908E+06 
c  r33          0.20069E+04      16   0.18576E-02   0.13873E+02 0.20058E+07 
c  r12          0.96147E+01      29   0.17889E+00   0.34255E+00 0.11577E+07 
c  r13          0.37156E+02      20   0.34912E-01   0.13705E+01 0.39933E+07 
c  r23          0.11116E+03      17   0.95944E-02   0.31545E+00 0.21088E+07 
c  epsilon      0.61880E+05      15   0.88262E-04   0.13679E+07 0.27205E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0012344                            86
a  r22                   -0.012082                            74
a  r33                    -0.20294                            80
a  r12                  -0.0029653                           135
a  r13                     -0.0532                           162
a  r23                  -0.0046711                            99
a  epsilon                -0.11894                           145
a  Local Time Step      1.0577e-10                             9


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -15775           21767          4.0526          3.6922
v  Velocity[Y]              -14676           26165        -0.48246        -0.60494
v  Velocity[Z]              -12653           20577        -0.23827        -0.31052
v  ǁVelocityǁ               0.1352           29085          84.373          90.745
v  Pressure            -2.0824e+11      8.0567e+11     -1.3098e+07     -1.4676e+07
v  r11                  5.9796e-08          2.2052       0.0015769       0.0015523
v  r22                  6.0302e-10           3.819       0.0016499       0.0016222
v  r33                  7.6065e-08          8.6168       0.0016726       0.0016425
v  r12                    -0.29294         0.21055     -9.3264e-05      -8.575e-05
v  r13                     -1.2655         0.42924       2.994e-05      3.2396e-05
v  r23                     -1.0424          0.2886      4.6468e-06      4.9226e-06
v  epsilon              1.6164e-13          6351.1        0.040824        0.038809
v  TurbVisc             4.4334e-05      2.2047e+08          228.95          220.51
v  CourantNb            9.0343e-07               1          0.8408         0.84827
v  FourierNb            4.8621e-07           641.6         0.42081         0.39143
v  total_pressure      -2.0824e+11      8.0567e+11     -1.2997e+07     -1.4575e+07
v  Local Time Step           1e-09      8.9543e-05      3.0824e-05      3.1921e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      9.1936e-05           641.6          1.2616          1.2397


 TIME FOR THE TIME STEP               23:        0.47941E+02

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


 INSTANT    0.240000000E-03   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.182323275E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.394889589E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.92720E-01 0.12186E+05
   Friction velocity        uet   :  0.89993E-02 0.86035E+03
   Friction velocity        uk    :  0.10020E-01 0.11679E+01
   Dimensionless distance   yplus :  0.23829E+02 0.32553E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1391 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.13413E+08       6   0.53045E-01   0.51522E+11 0.33634E+07 
c  Velocity[X]                                      0.14703E+11 
c  Velocity[Y]                                      0.18599E+11 
c  Velocity[Z]                                      0.18219E+11 
c  Pressure     0.20009E+03     163   0.59825E-01   0.72584E+00 0.19423E+10 
c  r11          0.54417E+03      10   0.32227E+00   0.33991E+01 0.41144E+06 
c  r22          0.69713E+03      10   0.31063E+00   0.10462E+03 0.26940E+07 
c  r33          0.17918E+04       9   0.23464E-01   0.17289E+02 0.18464E+07 
c  r12          0.50038E+03      10   0.32239E+00   0.43185E+00 0.98197E+06 
c  r13          0.38271E+03      10   0.32191E+00   0.41199E+01 0.27199E+07 
c  r23          0.11469E+03      12   0.14556E+00   0.38649E+00 0.19205E+07 
c  epsilon      0.58319E+05      11   0.17295E-01   0.45118E+07 0.15643E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0068022                           104
a  r22                   -0.068168                            60
a  r33                    -0.15279                            76
a  r12                  -0.0040442                           124
a  r13                    -0.06736                           176
a  r23                   -0.013012                           114
a  epsilon                -0.25529                           132
a  Local Time Step      1.1635e-10                             9


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -14416           25906          4.3783          3.9139
v  Velocity[Y]              -53978           14801        -0.62307        -0.73646
v  Velocity[Z]              -17090           12497        -0.61812        -0.76892
v  ǁVelocityǁ              0.11682           59477          89.495          95.705
v  Pressure            -2.2578e+11       2.813e+11     -1.4504e+07     -1.5907e+07
v  r11                  5.9398e-09          2.7436        0.001706       0.0016862
v  r22                  7.2658e-08          5.0893        0.001791       0.0017688
v  r33                  4.4726e-07          8.3839       0.0018112       0.0017871
v  r12                    -0.52086         0.24117     -0.00010537     -9.7665e-05
v  r13                      -1.549         0.58748      3.0093e-05      3.2694e-05
v  r23                     -1.0538         0.47568      6.9655e-06      7.2788e-06
v  epsilon              1.7781e-13           13117        0.054275        0.051173
v  TurbVisc             3.1911e-05      2.0042e+08          204.68          194.84
v  CourantNb            6.1259e-07               1         0.86052         0.86721
v  FourierNb            4.9509e-07          583.26         0.39155         0.36345
v  total_pressure      -2.2578e+11       2.813e+11     -1.4402e+07     -1.5806e+07
v  Local Time Step           1e-09      9.8497e-05      2.9273e-05      3.0269e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010107          583.26          1.2521          1.2307


 TIME FOR THE TIME STEP               24:        0.44696E+02

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


 INSTANT    0.250000000E-03   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.982492763E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391206963E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.27783E-01 0.10753E+05
   Friction velocity        uet   :  0.26676E-02 0.67325E+03
   Friction velocity        uk    :  0.10790E-01 0.12433E+01
   Dimensionless distance   yplus :  0.24563E+02 0.37351E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1570 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11384E+08       6   0.52056E-01   0.56163E+11 0.39230E+07 
c  Velocity[X]                                      0.13598E+11 
c  Velocity[Y]                                      0.27375E+11 
c  Velocity[Z]                                      0.15189E+11 
c  Pressure     0.21170E+03     185   0.58047E-01   0.75185E+00 0.11185E+10 
c  r11          0.16776E+04       9   0.29446E+00   0.17426E+02 0.33807E+07 
c  r22          0.49961E+04       8   0.24321E+00   0.11543E+03 0.73996E+07 
c  r33          0.49663E+04       8   0.36165E+00   0.15169E+02 0.17241E+07 
c  r12          0.28409E+04       8   0.26818E+00   0.39084E+02 0.22108E+08 
c  r13          0.36708E+04       8   0.41618E+00   0.10512E+01 0.19711E+07 
c  r23          0.54774E+04       8   0.37385E+00   0.53983E+00 0.16681E+07 
c  epsilon      0.43751E+06       9   0.36996E+00   0.13891E+08 0.71394E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0019223                            60
a  r22                     -1.1026                            52
a  r33                   -0.067352                           119
a  r12                  -0.0046121                           133
a  r13                     -1.0532                           196
a  r23                    -0.14601                           153
a  epsilon               -0.014734                            88
a  Local Time Step      1.2798e-10                             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -17871           27206          4.4376          3.9462
v  Velocity[Y]              -43971           28113          -0.571        -0.72398
v  Velocity[Z]              -37663           23927        -0.55354        -0.59553
v  ǁVelocityǁ             0.069831           49744           94.72          100.88
v  Pressure            -5.7266e+11      3.3629e+11     -1.5637e+07     -1.7368e+07
v  r11                  9.9773e-09          3.2104       0.0018451       0.0018305
v  r22                  3.3356e-08          6.2056       0.0019477       0.0019299
v  r33                  9.5415e-08          8.3956       0.0019671       0.0019487
v  r12                     -1.5429         0.31756     -0.00011529     -0.00010787
v  r13                      -1.771         0.77578      3.5783e-05      3.8174e-05
v  r23                     -1.0175         0.69162      9.8972e-06      1.0286e-05
v  epsilon              1.9559e-13           23522        0.076598         0.07127
v  TurbVisc             2.6054e-05      1.8219e+08           187.6          173.84
v  CourantNb             2.508e-06               1         0.88538         0.89072
v  FourierNb            4.9389e-07          530.23         0.36101         0.33458
v  total_pressure      -5.7266e+11      3.3629e+11     -1.5535e+07     -1.7267e+07
v  Local Time Step           1e-09      0.00010835      2.7608e-05      2.8518e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010512          530.23          1.2464          1.2253


 TIME FOR THE TIME STEP               25:        0.47010E+02

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


 INSTANT    0.260000000E-03   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.805777252E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.394915913E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.96155E-01 0.18146E+05
   Friction velocity        uet   :  0.90121E-02 0.11593E+04
   Friction velocity        uk    :  0.10031E-01 0.13684E+01
   Dimensionless distance   yplus :  0.24872E+02 0.41111E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1764 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.11182E+08       6   0.10873E+00   0.75161E+11 0.47590E+07 
c  Velocity[X]                                      0.15248E+11 
c  Velocity[Y]                                      0.39299E+11 
c  Velocity[Z]                                      0.20613E+11 
c  Pressure     0.20713E+03     190   0.41763E-01   0.75265E+00 0.12028E+10 
c  r11          0.12738E+04      15   0.32095E+00   0.23711E+02 0.48788E+07 
c  r22          0.27273E+03      19   0.12778E+00   0.86279E+01 0.12530E+07 
c  r33          0.15360E+04      14   0.27577E+00   0.86060E+02 0.19362E+07 
c  r12          0.11411E+04       8   0.38537E+00   0.49945E+01 0.56504E+07 
c  r13          0.30222E+04       7   0.42568E+00   0.16322E+01 0.36747E+07 
c  r23          0.50987E+03       9   0.62010E-01   0.76473E+00 0.26452E+07 
c  epsilon      0.81306E+05      13   0.45149E+00   0.22265E+08 0.18036E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                   -0.024677                           100
a  r22                   -0.079983                            42
a  r33                   -0.061822                           147
a  r12                  -0.0041764                           115
a  r13                    -0.21789                           170
a  r23                    -0.26138                           132
a  epsilon              -0.0047239                            58
a  Local Time Step      1.4078e-10                             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -12987           21504          4.3776          3.8297
v  Velocity[Y]              -16813           37524        -0.57943        -0.78503
v  Velocity[Z]              -23589           11809        -0.63669        -0.70277
v  ǁVelocityǁ             0.025379           43927          99.481          105.54
v  Pressure            -5.2253e+11      2.6499e+11     -2.2508e+07      -2.385e+07
v  r11                  3.6937e-08          3.5705       0.0019804       0.0019729
v  r22                  6.6534e-08          6.9526       0.0021101       0.0021001
v  r33                  3.9518e-07           8.922       0.0021267       0.0021169
v  r12                     -1.5334         0.39946     -0.00012417      -0.0001171
v  r13                     -1.8507         0.98814      3.0631e-05      3.4335e-05
v  r23                    -0.97325         0.98814      1.3951e-05      1.4435e-05
v  epsilon              2.1514e-13           37236         0.11102         0.10199
v  TurbVisc             2.1858e-05      1.6563e+08          164.85           151.9
v  CourantNb            2.4392e-06               1         0.89865         0.90291
v  FourierNb            4.8203e-07          482.01         0.33207         0.30716
v  total_pressure      -5.2253e+11      2.6499e+11     -2.2406e+07     -2.3749e+07
v  Local Time Step           1e-09      0.00011918      2.5811e-05      2.6664e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00011303          482.01          1.2307          1.2101


 TIME FOR THE TIME STEP               26:        0.46002E+02

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


 INSTANT    0.270000000E-03   TIME STEP NUMBER              27
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.153989246E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.394434286E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.93655E-01 0.11586E+05
   Friction velocity        uet   :  0.91105E-02 0.72790E+03
   Friction velocity        uk    :  0.10686E-01 0.14468E+01
   Dimensionless distance   yplus :  0.25819E+02 0.43466E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1770 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.10513E+08       7   0.66751E-01   0.44173E+11 0.34849E+07 
c  Velocity[X]                                      0.12074E+11 
c  Velocity[Y]                                      0.16250E+11 
c  Velocity[Z]                                      0.15849E+11 
c  Pressure     0.15019E+03     204   0.64817E-01   0.65315E+00 0.13267E+10 
c  r11          0.15307E+03      12   0.91857E-02   0.58530E+01 0.47007E+06 
c  r22          0.36353E+03      10   0.90477E-01   0.43603E+01 0.44676E+06 
c  r33          0.12928E+04       9   0.22446E-01   0.76378E+03 0.27601E+07 
c  r12          0.12798E+03      11   0.31344E-01   0.84690E+00 0.61373E+06 
c  r13          0.67901E+02      12   0.52833E-01   0.89580E+00 0.99431E+06 
c  r23          0.91767E+02      11   0.43503E-01   0.94620E+00 0.11210E+07 
c  epsilon      0.61014E+05      13   0.17446E-01   0.57804E+08 0.97419E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                   -0.017895                            91
a  r22                 -0.00055258                            23
a  r33                   -0.070495                            67
a  r12                  -0.0047607                           146
a  r13                    -0.12378                           198
a  r23                    -0.20174                           122
a  epsilon               -0.032343                            48
a  Local Time Step      1.5486e-10                             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -26207           12881          4.3672          3.8202
v  Velocity[Y]              -11243           20520        -0.66461        -0.70315
v  Velocity[Z]              -29717           19813        -0.63369        -0.63458
v  ǁVelocityǁ               0.1478           37173          103.35          109.46
v  Pressure            -3.6471e+11       1.902e+11     -1.8042e+07     -1.9026e+07
v  r11                  8.7548e-08          4.0056       0.0021348       0.0021334
v  r22                  1.6153e-07          7.8769        0.002295       0.0022923
v  r33                  2.8159e-07          16.463        0.002316       0.0023143
v  r12                     -1.5239         0.72548     -0.00012617     -0.00012033
v  r13                     -1.9635          1.2019      2.8713e-05      3.3027e-05
v  r23                    -0.91851          1.3836      1.8269e-05      1.8259e-05
v  epsilon              2.3666e-13           59708         0.16775         0.15126
v  TurbVisc              1.608e-05      1.5057e+08          145.24          131.76
v  CourantNb            2.7361e-06               1         0.90364         0.90788
v  FourierNb            5.0429e-07          438.18         0.30447          0.2814
v  total_pressure      -3.6471e+11       1.902e+11      -1.794e+07     -1.8924e+07
v  Local Time Step           1e-09       0.0001311      2.3952e-05      2.4713e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010461          438.18          1.2081          1.1893


 TIME FOR THE TIME STEP               27:        0.48451E+02

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


 INSTANT    0.280000000E-03   TIME STEP NUMBER              28
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.419704894E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391534252E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12907E+00 0.17626E+05
   Friction velocity        uet   :  0.12706E-01 0.10468E+04
   Friction velocity        uk    :  0.10681E-01 0.15716E+01
   Dimensionless distance   yplus :  0.26530E+02 0.46844E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1867 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.92887E+07       6   0.61999E-01   0.59928E+11 0.43206E+07 
c  Velocity[X]                                      0.17917E+11 
c  Velocity[Y]                                      0.16266E+11 
c  Velocity[Z]                                      0.25745E+11 
c  Pressure     0.17975E+03     169   0.68641E-01   0.73598E+00 0.11985E+10 
c  r11          0.15798E+03      12   0.84629E-02   0.88510E+01 0.49002E+06 
c  r22          0.24837E+03      12   0.15920E-01   0.52388E+01 0.42382E+06 
c  r33          0.11374E+04       9   0.63885E-03   0.61589E+02 0.11009E+07 
c  r12          0.11539E+03      11   0.71454E-02   0.12010E+01 0.62001E+06 
c  r13          0.62015E+02      13   0.32490E-01   0.11878E+01 0.68840E+06 
c  r23          0.14334E+03      12   0.22860E-01   0.14774E+01 0.94987E+06 
c  epsilon      0.67439E+05      13   0.33894E-02   0.11346E+09 0.85413E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0065176                           152
a  r22                  -0.0024092                            26
a  r33                   -0.054116                            78
a  r12                   -0.005484                           170
a  r13                    -0.10322                           207
a  r23                    -0.21572                           120
a  epsilon               -0.016424                            91
a  Local Time Step      1.7035e-10                             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -36959           57429          4.5512          3.9632
v  Velocity[Y]              -21842           24736        -0.76201        -0.74214
v  Velocity[Z]              -24911           25873        -0.87857        -0.75619
v  ǁVelocityǁ             0.099784           66668          107.65          113.64
v  Pressure            -7.0695e+11      3.1007e+11     -1.9178e+07     -1.9964e+07
v  r11                  1.0201e-07          4.4521       0.0023108       0.0023167
v  r22                  1.7768e-07          8.8268       0.0025129       0.0025183
v  r33                  5.7168e-08          17.195        0.002533       0.0025403
v  r12                     -1.5137          1.1817     -0.00012975     -0.00012477
v  r13                     -2.1808          1.6408      3.1656e-05      3.6709e-05
v  r23                    -0.85886          1.8963      2.4344e-05      2.3682e-05
v  epsilon              1.1817e-11           91434         0.25389         0.22472
v  TurbVisc             1.3904e-05      1.3687e+08          131.77          120.57
v  CourantNb            2.1664e-06               1         0.91281         0.91631
v  FourierNb            5.3012e-07          398.33         0.28291         0.26126
v  total_pressure      -7.0695e+11      3.1007e+11     -1.9077e+07     -1.9862e+07
v  Local Time Step           1e-09      0.00014421      2.2998e-05      2.3724e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00011473          398.33          1.1957          1.1776


 TIME FOR THE TIME STEP               28:        0.48026E+02

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


 INSTANT    0.290000000E-03   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.759554838E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.395095620E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.21003E+00 0.75939E+04
   Friction velocity        uet   :  0.17908E-01 0.64211E+03
   Friction velocity        uk    :  0.11356E-01 0.16191E+01
   Dimensionless distance   yplus :  0.27839E+02 0.48641E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1934 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.90823E+07       6   0.56961E-01   0.61479E+11 0.44305E+07 
c  Velocity[X]                                      0.20544E+11 
c  Velocity[Y]                                      0.20671E+11 
c  Velocity[Z]                                      0.20264E+11 
c  Pressure     0.19177E+03     179   0.49426E-01   0.75615E+00 0.12957E+10 
c  r11          0.16437E+03      12   0.21307E-01   0.13396E+02 0.54020E+06 
c  r22          0.21609E+03      12   0.15092E-01   0.75625E+01 0.40268E+06 
c  r33          0.10102E+04      10   0.18471E-02   0.80357E+02 0.10627E+07 
c  r12          0.10853E+03      11   0.38370E-01   0.19721E+01 0.64613E+06 
c  r13          0.92769E+02      11   0.16165E+00   0.17221E+01 0.53565E+06 
c  r23          0.13016E+03      13   0.29938E-01   0.22208E+01 0.91964E+06 
c  epsilon      0.81450E+05      13   0.22945E-02   0.25879E+09 0.77986E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                   -0.004683                           107
a  r22                  -0.0033907                            29
a  r33                   -0.042694                            45
a  r12                  -0.0067724                           143
a  r13                    -0.10329                           180
a  r23                    -0.21105                            92
a  epsilon               -0.044735                            49
a  Local Time Step      1.8738e-10                             5


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -12107           32072          4.5475          3.9462
v  Velocity[Y]              -36128           22960         -1.0144        -0.87412
v  Velocity[Z]              -16971           30174         -0.7889        -0.61782
v  ǁVelocityǁ              0.14127           42099          111.81          117.64
v  Pressure            -2.7686e+10      6.9406e+11     -1.5982e+07     -1.6851e+07
v  r11                  7.9212e-08          5.7959        0.002507       0.0025203
v  r22                  4.5917e-08          10.165       0.0027669       0.0027805
v  r33                  6.2884e-08          14.579       0.0027821       0.0027999
v  r12                     -1.5024          1.8152     -0.00012746     -0.00012309
v  r13                     -2.3804          2.4165      4.0709e-05      4.5787e-05
v  r23                    -0.81729          2.5417      3.2812e-05      3.1317e-05
v  epsilon              3.0949e-11       1.437e+05         0.39031         0.34064
v  TurbVisc             1.0236e-05      2.7421e+06          13.279          14.244
v  CourantNb            2.5486e-06               1         0.91985          0.9233
v  FourierNb             5.648e-07           7.695         0.26179         0.24153
v  total_pressure      -2.7686e+10      6.9406e+11     -1.5881e+07      -1.675e+07
v  Local Time Step           1e-09      0.00015863      2.1872e-05      2.2549e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      9.9464e-05           7.695          1.1816          1.1648


 TIME FOR THE TIME STEP               29:        0.47471E+02

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


 INSTANT    0.300000000E-03   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612         0.468404471E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392125527E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.16141E+00 0.50991E+04
   Friction velocity        uet   :  0.13900E-01 0.39278E+03
   Friction velocity        uk    :  0.11433E-01 0.17325E+01
   Dimensionless distance   yplus :  0.25082E+02 0.52049E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       1997 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.84276E+07       6   0.68317E-01   0.39595E+11 0.33671E+07 
c  Velocity[X]                                      0.12595E+11 
c  Velocity[Y]                                      0.12824E+11 
c  Velocity[Z]                                      0.14176E+11 
c  Pressure     0.15596E+03     169   0.40546E-01   0.72395E+00 0.13283E+10 
c  r11          0.22156E+03      12   0.51451E-01   0.20120E+02 0.85836E+06 
c  r22          0.20807E+03      13   0.68439E-01   0.12681E+02 0.38456E+06 
c  r33          0.90644E+03      10   0.12777E-01   0.81615E+02 0.93380E+06 
c  r12          0.13405E+03      13   0.16038E+00   0.29220E+01 0.64525E+06 
c  r13          0.26783E+03      10   0.20228E+00   0.29045E+01 0.48703E+06 
c  r23          0.12819E+03      13   0.99450E-01   0.33258E+01 0.65630E+06 
c  epsilon      0.11793E+06      13   0.19257E-02   0.71526E+09 0.82276E+05 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0055271                            93
a  r22                  -0.0073816                            23
a  r33                    -0.03048                            40
a  r12                  -0.0086452                           123
a  r13                    -0.11421                           156
a  r23                    -0.21033                            67
a  epsilon               -0.024875                            25
a  Local Time Step      2.0612e-10                             4


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]              -11197           13115          4.4395          3.8087
v  Velocity[Y]             -9637.5           27273         -1.0347        -0.76871
v  Velocity[Z]              -15390          9326.8         -0.8741        -0.74214
v  ǁVelocityǁ              0.09334           28234          115.26          120.99
v  Pressure            -5.0947e+11      4.6917e+10     -2.2965e+07     -2.3838e+07
v  r11                  1.6287e-08          7.4686       0.0027291       0.0027505
v  r22                  2.1499e-07          12.214        0.003061       0.0030836
v  r33                  4.2299e-08          12.205       0.0030722       0.0031021
v  r12                     -1.4896          2.6282     -0.00012488     -0.00012038
v  r13                     -2.6598          3.5451      5.1119e-05      5.6413e-05
v  r23                    -0.77635          3.3186      4.4177e-05      4.1892e-05
v  epsilon              3.4044e-11      2.3986e+05         0.61284         0.53279
v  TurbVisc              8.255e-06      1.0449e+06          8.7943          9.8227
v  CourantNb            2.3954e-06               1         0.92815         0.93087
v  FourierNb            5.5343e-07          4.8516         0.24102         0.22187
v  total_pressure      -5.0947e+11      4.6917e+10     -2.2864e+07     -2.3737e+07
v  Local Time Step           1e-09      0.00017449       2.067e-05      2.1253e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010634          4.8516          1.1692          1.1527


 TIME FOR THE TIME STEP               30:        0.47133E+02

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


 INSTANT    0.310000000E-03   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.124382105E-13
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.394030639E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.20881E+00 0.56284E+04
   Friction velocity        uet   :  0.18554E-01 0.43524E+03
   Friction velocity        uk    :  0.11438E-01 0.18998E+01
   Dimensionless distance   yplus :  0.29232E+02 0.57074E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       2055 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.74234E+07       7   0.98159E-01   0.21477E+11 0.33149E+07 
c  Velocity[X]                                      0.54378E+10 
c  Velocity[Y]                                      0.97263E+10 
c  Velocity[Z]                                      0.63134E+10 
c  Pressure     0.11042E+03     154   0.23411E-01   0.58002E+00 0.17241E+10 
c  r11          0.44438E+03      11   0.70795E-01   0.30138E+02 0.14507E+07 
c  r22          0.53849E+03      12   0.22050E+00   0.22976E+02 0.38168E+06 
c  r33          0.10145E+04      11   0.13633E+00   0.14571E+03 0.18987E+07 
c  r12          0.31276E+03      10   0.20726E+00   0.43649E+01 0.68229E+06 
c  r13          0.62599E+03       9   0.19875E+00   0.59166E+01 0.10315E+07 
c  r23          0.23651E+03      12   0.20530E+00   0.45950E+01 0.73971E+06 
c  epsilon      0.20976E+06      13   0.95287E-02   0.13211E+10 0.12850E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0025767                           110
a  r22                   -0.002899                            26
a  r33                   -0.027669                            31
a  r12                   -0.010172                           121
a  r13                    -0.12957                           149
a  r23                    -0.21978                            65
a  epsilon                -0.19051                            37
a  Local Time Step      2.2672e-10                             3


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -7906.1           10403          4.5627          3.8815
v  Velocity[Y]             -7172.9           10002         -1.1541        -0.81027
v  Velocity[Z]             -7057.8          8113.4         -0.9003        -0.77938
v  ǁVelocityǁ             0.073589           12036          118.42          124.01
v  Pressure            -2.3822e+10      3.8174e+11     -1.8104e+07     -1.8901e+07
v  r11                  1.7916e-08          9.4715       0.0029786       0.0030091
v  r22                  2.3649e-07          13.683       0.0033973       0.0034297
v  r33                  1.0122e-07          15.151        0.003404       0.0034463
v  r12                     -1.4757           3.675     -0.00011891     -0.00011415
v  r13                     -2.8829          5.2687      6.5675e-05      7.1172e-05
v  r23                    -0.74356          4.1904      5.7627e-05       5.465e-05
v  epsilon              3.7448e-11      3.3312e+05         0.91545         0.81008
v  TurbVisc             8.1465e-06      9.4994e+05          7.8989          8.7071
v  CourantNb             1.057e-06               1           0.935         0.93699
v  FourierNb            5.5901e-07          4.4107         0.22383         0.20593
v  total_pressure      -2.3822e+10      3.8174e+11     -1.8003e+07       -1.88e+07
v  Local Time Step           1e-09      0.00019194      1.9676e-05      2.0218e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00013198          4.4107          1.1588          1.1429


 TIME FOR THE TIME STEP               31:        0.47446E+02

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


 INSTANT    0.320000000E-03   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.442367464E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.391371670E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.12484E+00 0.76090E+04
   Friction velocity        uet   :  0.71346E-02 0.49834E+03
   Friction velocity        uk    :  0.11371E-01 0.21053E+01
   Dimensionless distance   yplus :  0.29523E+02 0.62455E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       2103 outlet faces on       2770

   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.61616E+07       7   0.42077E-01   0.55516E+10 0.10677E+07 
c  Velocity[X]                                      0.17148E+10 
c  Velocity[Y]                                      0.18570E+10 
c  Velocity[Z]                                      0.19798E+10 
c  Pressure     0.81271E+02     143   0.15541E-01   0.47768E+00 0.10626E+10 
c  r11          0.27012E+03      11   0.21707E-02   0.47646E+02 0.44299E+06 
c  r22          0.20150E+03      12   0.22843E-02   0.31551E+02 0.34413E+06 
c  r33          0.76877E+03      11   0.50018E-03   0.16621E+03 0.72045E+06 
c  r12          0.10160E+03      12   0.69266E-02   0.48388E+01 0.47551E+06 
c  r13          0.84123E+02      11   0.36498E-02   0.10555E+02 0.44947E+06 
c  r23          0.95959E+02      13   0.41896E-02   0.47456E+01 0.45435E+06 
c  epsilon      0.50619E+06      13   0.13308E-03   0.75020E+10 0.28890E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0021681                           133
a  r22                  -0.0041909                            25
a  r33                   -0.026965                            32
a  r12                   -0.012658                           155
a  r13                    -0.15249                           162
a  r23                    -0.26343                            51
a  epsilon                -0.13076                            41
a  Local Time Step      2.4941e-10                             2


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -5492.5          8142.3          4.5816          3.8581
v  Velocity[Y]             -6996.5          8651.4         -1.2535        -0.83391
v  Velocity[Z]             -5877.5          5646.2        -0.97307        -0.81157
v  ǁVelocityǁ             0.074474          9023.6          121.43          126.89
v  Pressure            -2.7704e+10      1.2707e+11      -1.722e+07     -1.7858e+07
v  r11                  1.9707e-08          12.308       0.0032631       0.0033051
v  r22                  2.6014e-07          15.135       0.0037805       0.0038236
v  r33                  6.3794e-08           19.68       0.0037827        0.003838
v  r12                     -1.4606          4.6312     -0.00010979     -0.00010429
v  r13                     -2.9686          7.7776      8.3172e-05       8.934e-05
v  r23                     -0.7009          4.9985      7.2137e-05      6.8491e-05
v  epsilon              3.2848e-11      4.3217e+05          1.4131          1.3043
v  TurbVisc             8.7686e-06      8.6353e+05          7.5741          8.3483
v  CourantNb            2.3081e-06               1         0.94211         0.94326
v  FourierNb             5.262e-07          4.0095         0.20703         0.19039
v  total_pressure      -2.7704e+10      1.2707e+11     -1.7118e+07     -1.7757e+07
v  Local Time Step           1e-09      0.00021114      1.8659e-05      1.9149e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00012658          4.0095          1.1491          1.1336


 TIME FOR THE TIME STEP               32:        0.50988E+02

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


 INSTANT    0.330000000E-03   TIME STEP NUMBER              33
 ============================================================= 



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

  max_time_step                              33 (current: 33)

 Finished reading "control_file".



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2        2782        -0.392541432E+02
Smooth wall               5       51612        -0.389590275E-14
Rough wall                6           0         0.000000000E+00
Symmetry                  4           0         0.000000000E+00
Free outlet               3        2770         0.392783958E+02
Free inlet               13           0         0.000000000E+00
Convective inlet         15           0         0.000000000E+00
Free surface             14           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn :  0.24775E+00 0.61825E+04
   Friction velocity        uet   :  0.24441E-01 0.39091E+03
   Friction velocity        uk    :  0.11682E-01 0.25296E+01
   Dimensionless distance   yplus :  0.30571E+02 0.75514E+04
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :          0
   Total number of wall faces                   :      51612
------------------------------------------------------------


Incoming flow detained for       2129 outlet faces on       2770


 Write final restart files
   checkpoint at iteration         33, Physical time    0.33000E-03


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

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

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

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


 Time for restart files:    0.88156E+00



   ** INFORMATION ON CONVERGENCE
      --------------------------
-----------------------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive Time residual
-----------------------------------------------------------------------------
c  Velocity     0.54446E+07       6   0.35942E-01   0.35106E+10 0.67670E+06 
c  Velocity[X]                                      0.11073E+10 
c  Velocity[Y]                                      0.11869E+10 
c  Velocity[Z]                                      0.12164E+10 
c  Pressure     0.59849E+02     130   0.99530E-02   0.37474E+00 0.56075E+09 
c  r11          0.29427E+03      11   0.24808E-01   0.83772E+02 0.43104E+06 
c  r22          0.21975E+03      12   0.24255E-01   0.50554E+02 0.32700E+06 
c  r33          0.73690E+03      10   0.20322E-02   0.25765E+03 0.60295E+06 
c  r12          0.10927E+03      11   0.77622E-01   0.61091E+01 0.41265E+06 
c  r13          0.10167E+03      11   0.42256E-01   0.15864E+02 0.40371E+06 
c  r23          0.10459E+03      12   0.29339E-01   0.10384E+02 0.47150E+06 
c  epsilon      0.16061E+07      13   0.44131E-03   0.74456E+11 0.70901E+06 
-----------------------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  r11                  -0.0025111                           150
a  r22                  -0.0011825                            13
a  r33                   -0.029917                            22
a  r12                   -0.017198                           183
a  r13                     -0.1835                           155
a  r23                    -0.32395                            50
a  epsilon                -0.58381                            34
a  Local Time Step      2.7434e-10                             1


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

   field                   minimum         maximum        set mean    spatial mean
-  ---------------  --------------  --------------  --------------  --------------
v  Velocity[X]             -4670.8          6406.6          4.6177          3.8549
v  Velocity[Y]             -6812.2          7140.2          -1.333        -0.84007
v  Velocity[Z]               -4997          5475.8         -1.0703        -0.86774
v  ǁVelocityǁ             0.080686          7430.8          124.28          129.62
v  Pressure            -1.1279e+10      2.7559e+10     -1.8456e+07     -1.9105e+07
v  r11                  2.3159e-09          17.879       0.0035904       0.0036466
v  r22                  2.8616e-07          16.603       0.0042182       0.0042739
v  r33                  3.1437e-07          28.652       0.0042166       0.0042858
v  r12                     -1.6237          5.6219     -9.6623e-05     -8.9622e-05
v  r13                      -3.195          10.851      0.00010463      0.00011184
v  r23                    -0.81957          6.1193      8.8388e-05      8.4309e-05
v  epsilon              3.6133e-11      5.2929e+05          2.3931          2.3399
v  TurbVisc             9.5182e-06      9.8729e+05          7.3784          7.9835
v  CourantNb            2.4057e-06               1         0.94977         0.95026
v  FourierNb            4.4871e-07          3.6452         0.19063         0.17529
v  total_pressure      -1.1279e+10      2.7559e+10     -1.8355e+07     -1.9004e+07
v  Local Time Step           1e-09      0.00023225       1.767e-05      1.8124e-05


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier      0.00010666          3.6452          1.1404          1.1255


 TIME FOR THE TIME STEP               33:        0.51482E+02

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



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



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


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




   ** TIME FOR FINAL WRITING:    0.15872E-04
      -----------------------                                



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




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


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

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:           1482.727 s
  System CPU time:           90.627 s
  Total CPU time:         12610.996 s

  Elapsed time:            1587.993 s
  CPU / elapsed time          0.991

Memory use summary:

  Total memory used:                              11.713 GiB
                             local minimum:        1.452 GiB  (rank 1)
                             local maximum:        1.477 GiB  (rank 5)
  Theoretical instrumented dynamic memory:         1.313 GiB
                             local minimum:      159.876 MiB  (rank 1)
                             local maximum:      176.328 MiB  (rank 7)
