command: 
 ./cs_solver --param M157Full.xml --logp 1 --mpi

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

                                  (R)
                      Code_Saturne

                      Version 3.3.2


  Copyright (C) 1998-2014 EDF S.A., France

  build Mi 17 Dez 2014 16:12:36 CET
  MPI version 2.1 (Open MPI 1.7.2)


  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:                Di 06 Jan 2015 17:18:40 CET
  System:              Linux 3.11.10-21-desktop
  Machine:             aeroDeltaKroeger
  Processor:           model name	: AMD Opteron(TM) Processor 6220
  Memory:              32219 MB
  User:                kroeger ()
  Directory:           /home/kroeger/codeSaturnTest/M157/RESU/20150106-1718
  MPI ranks:           7 (appnum attribute: 0)
  I/O read method:     standard input and output, serial access
  I/O write method:    standard input and output, serial access
  I/O rank step:        1

  External libraries for partitioning:
    SCOTCH 6.0.0

 Reading metadata from file: "mesh_input/mesh_01"
 Reading metadata from file: "mesh_input/mesh_02"

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

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


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




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


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

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

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


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

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


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


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

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

       OMEGAX =    0.00000E+00 (Rotation vector x component )
       OMEGAY =    0.00000E+00 (Rotation vector y component )
       OMEGAZ =    0.00000E+00 (Rotation vector z component )
       ICORIO =          0 (Coriolis source terms       )

  -- Continuous phase:

       RO0    =    0.11786E+01 (Reference density           )
       VISCL0 =    0.18300E-04 (Ref. molecular dyn. visc.   )
       CP0    =    0.10172E+04 (Ref. specific heat          )
       ICP    =              0 (> 0: variable CP (usphyv)   )
       P0     =    0.10132E+06 (Ref. total pressure         )
       PRED0  =    0.00000E+00 (Ref. reduced pressure       )
       T0     =    0.29315E+03 (Ref. temperature            )

       IROVAR =              0 (Density constant(0) or not(1)
       IVIVAR =              0 (Molec. visc cst.(0) or not(1)

       Initial reference point for pressure
       XYZP0  =    0.00000E+00   0.00000E+00   0.00000E+00

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


 ** HOMOGENEOUS MIXTURE MODEL FOR CAVITATION
    ----------------------------------------

       ICAVIT =             -1 (-1: single phase flow       )
                               ( 0: no vap./cond. model     )
                               ( 1: Merkle's model        )


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


 ** THERMAL MODEL
    -------------
 --- Continuous phase:

   - Commons
       ITHERM =              0 (0:  no thermal model        )
                               (10: temperature C           )
                               (11: temperature K           )
                               (20: enthalpy                )
                               (30: total energy            )
       ISCALT =             -1 (Thermal scalar number       )


 ** TURBULENCE
    ----------

 --- Continuous phase:

   - Commons
       ITURB  =             60 (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)     )

   - k-omega SST         (ITURB = 60)
       ALMAX  =   -0.99900E+03 (Characteristic length       )
       UREF   =    0.10000E+01 (Characteristic velocity     )
       IKECOU =              0 (k-epsilon coupling mode     )
       IGRAKE =              1 (Account for gravity         )
       RELAXV =    0.10000E+01 for k      (Relaxation)
       RELAXV =    0.10000E+01 for omega  (Relaxation)

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

 --- Constants

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

   - k-omega SST         (ITURB = 60)
       CKWSK1 =    0.11765E+01 (sigma_k1 constant           )
       CKWSK2 =    0.10000E+01 (sigma_k2 constant           )
       CKWSW1 =    0.20000E+01 (sigma_omega1 constant       )
       CKWSW2 =    0.11682E+01 (sigma_omega2 constant       )
       CKWBT1 =    0.75000E-01 (beta1 constant              )
       CKWBT2 =    0.82800E-01 (beta2 constant              )
       CKWGM1 =    0.53933E+00 (gamma1 constant             )
       CKWGM2 =    0.41667E+00 (gamma2 constant             )
       CKWA1  =    0.31000E+00 (a1 constant to compute mu_t )
       CKWC1  =    0.10000E+02 (c1 const. for prod. limiter )
       CMU    =    0.90000E-01 (Cmu (or Beta*) constant for )
                                    omega/epsilon conversion)


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


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

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


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


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

    UNSTEADY ALGORITHM

 --- Time step parameters

       IDTVAR =              2 (0 cst; 1,2 var (t, t-space  )
       IPTLRO =              0 (1: rho-related DT clipping  )
       COUMAX =    0.10000E+01 (Maximum target CFL          )
       FOUMAX =    0.10000E+02 (Maximum target Fourier      )
       VARRDT =    0.10000E+00 (For var. DT, max. increase  )
       DTMIN  =    0.10000E-01 (Minimum time step           )
       DTMAX  =    0.10000E+03 (Maximum time step           )
       DTREF  =    0.10000E+00 (Reference time step         )

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

 --- Frozen velocity field

       ICCVFG =              0 (1: frozen velocity field    )

 --- Per-variable properties

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

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

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

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


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

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

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


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


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

  -- Continuous phase:

       IREVMC =              0 (Velocity reconstruction mode)

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

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


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


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

       IMRGRA =              0 (Reconstruction mode         )
       ANOMAX =    0.78540E+00 (Non-ortho angle: limit for  )
                               (least squares ext. neighbors)

-------------------------------------------------------------------
 Variable         NSWRGR NSWRSM      EPSRGR      EPSRSM      EXTRAG
-------------------------------------------------------------------
 Velocity            100      1  0.1000E-04  0.1000E-06  0.0000E+00
 Pressure            100      2  0.1000E-04  0.1000E-06  0.0000E+00
 k                   100      1  0.1000E-04  0.1000E-06  0.0000E+00
 omega               100      1  0.1000E-04  0.1000E-06  0.0000E+00
-----------------------------------------------------------

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


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


 ** WALL DISTANCE COMPUTATION
    -------------------------

       ICDPAR =              1 ( 1: std, reread if restart
                               (-1: std, recomputed if restrt
                               ( 2: old, reread if restart
                               (-2: old, recomputed if restrt


       NITMAY =          10000 (Nb iter for iter resolution )
       NSWRSY =              1 (Nb iter for rhs reconstr.   )
       NSWRGY =            100 (Nb iter for grad. reconstr. )
       IMLIGY =             -1 (Gradient limitation method  )
       IRCFLY =              1 (Conv. Diff. flow reconstr.  )
       ISCHCY =              1 (Convective scheme           )
       ISSTPY =              0 (Slope tet use               )
       IMGRPY =              0 (Multigrid algorithm         )
       IWARNY =              0 (Verbosity level             )
       NTCMXY =           1000 (Nb iter for steady convect. )

       BLENCY =    0.00000E+00 (2nd order conv. scheme prop.)
       EPSILY =    0.10000E-07 (Iterative solver precision  )
       EPSRSY =    0.10000E-04 (rhs reconstruction precision)
       EPSRGY =    0.10000E-04 (Gradient reconstr. precision)
       CLIMGY =    0.15000E+01 (Coeff. for grad. limitation )
       EXTRAY =    0.00000E+00 (Coeff. for grad. extrapolat.)
       COUMXY =    0.50000E+04 (Max CFL for convection      )
       EPSCVY =    0.10000E-07 (Precision for steady conv.  )
       YPLMXY =    0.20000E+03 (y+ max w. damping influence )


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


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

--------------------------------------------------
 Variable         IRESOL NITMAX      EPSILO IDIRCL
--------------------------------------------------
 Velocity             -1  10000  0.1000E-07      1
 Pressure             -1  10000  0.1000E-07      1
 k                    -1  10000  0.1000E-07      1
 omega                -1  10000  0.1000E-07      1
-----------------------------------

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


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


 ** MULTIGRID
    ---------

       NCEGRM =             30 (Max nb cells coarsest grid  )
       NGRMAX =             25 (Max number of levels        )
--------------------------------------
 Variable           IMGR NCYMAX NITMGF
--------------------------------------                       
 Velocity              0    100     10
 Pressure              0    100     10
 k                     0    100     10
 omega                 0    100     10
------------------------------

       IMGR   =  0 ou 1        (1: multigrid activated      )
       NCYMAX =                (Max number  of cycles       )
       NITMGF =                (Max nb iter on coarsest grid)


  Multigrid rank merge parameters:
    mean  coarse cells merge threshold: 300
    total coarse cells merge threshold: 500
    minimum ranks merge threshold:      1
    merge stride:                       1

  Multigrid coarsening type: algebraic, face traveral by criteria

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


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

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


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

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

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


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


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

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

 --- Post-processed variables

       Number Name
Velocity
Pressure
k
omega
turbulent_viscosity
CourantNb
FourierNb
total_pressure
Local Time Step
         --           --

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

       Number Name                  Nb. probes (-1: all)
         2 Velocity[X]                   -1
         3 Velocity[Y]                   -1
         4 Velocity[Z]                   -1
         5 Pressure                      -1
         6 k                             -1
         7 omega                         -1
         8 Density                       -1
         9 LamVisc                       -1
        10 turbulent_viscos              -1
        11 CourantNb                     -1
        12 FourierNb                     -1
        13 total_pressure                -1
        14 Local Time Step               -1
         --           --                --

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

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

         2 Velocity                       0
         5 Pressure                       0
         6 k                              0
         7 omega                          0
        10 turbulent_viscos            -999
        11 CourantNb                   -999
        12 FourierNb                   -999
        13 total_pressure              -999
        14 Local Time Step             -999
         --           --                --

 --- Additional post-processing variables (ipstdv)
       ipstfo =              7 (Force exerted  at boundary)
       ipstyp =              1 (Yplus          at boundary)
       ipstft =              1 (Thermal flow   at boundary)
       ipsttb =              0 (Temperature    at boundary)
       ipstnu =              0 (Nusselt        at boundary)


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


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

       IALE   =              0 (1: activated                )
       NALINF =              0 (Fluid initialization
                                                  iterations)


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


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

  -1: name: results
      directory: postprocessing
      format: EnSight Gold
      options: 
      time dependency: fixed mesh
      output: every 10 time steps and at calculation end


 Reading file:        mesh_input/mesh_01
 Finished reading:    mesh_input/mesh_01

 Reading file:        mesh_input/mesh_02
 Finished reading:    mesh_input/mesh_02
 No "partition_input/domain_number_7" file available;

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

 Partitioning finished (0.00413 s)


 -------------------------------------------------------
  Joining number 1:

  Selection criteria: "all[] and (not(row02Outlet or row03Inlet))"

  Parameters for the joining operation:
    Shortest incident edge fraction:           0.05000
    Maximum angle between joined face planes: 15.00000

  Advanced joining parameters:
    Verbosity level:                                 1
    Visualization level:                             1
    Deepest level reachable in tree building:       30
    Max boxes by leaf:                              25
    Max ratio of linked boxes / init. boxes:   5.00000
    Max ratio of boxes for distribution:       2.00000
    Merge step tolerance multiplier:           1.00000
    Pre-merge factor:                          0.05000
    Tolerance computation mode:                      1
    Intersection computation mode:                   1
    Max. number of equiv. breaks:                  500
    Max. number of subfaces by face:               200

  Before joining
     Number of cells:          376624
     Number of interior faces: 920296
     Number of boundary faces: 419152
     Number of vertices:       597384

  Global number of boundary faces selected for joining:     415696

  Element selection successfully done.
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

     338675 |    0.000013 |  0.0000000000e+00  -1.9589765779e-01  -2.7050930362e-01 | ORI
      66059 |    0.006800 | -1.9984014443e-15   1.1000000000e+01  -8.4000000000e+00 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 3D

  Global number of intersections detected:       464537
    Vertex-Vertex intersections:          414873
    Other intersections:                   49664

  Joining operation is non-conforming.

  Global number of new vertices to create:      25781

  Equivalences broken for 0 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 53210 global element couples.

  Max size of a merge set of vertices: 4

  Excessive transitivity for 0 set(s) of vertices.

  Edge removed for 54 faces (global).
  Join mesh cleaning done.

  Edge removed for 24 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Global number of faces after splitting:     401660

  Global configuration after the joining operation:
     Global number of border faces to add:     385224

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0

  After joining
     Number of cells:          376624
     Number of interior faces: 936732
     Number of boundary faces: 388680
     Number of vertices:       575605


  Joining  1 completed (26.3 s).

  All joining operations successfully finished:

    Wall clock time:                  26.3


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

 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 =              53800
    maximum value =              53804

      1 : [      53800 ;      53801 [ =          1
      2 : [      53801 ;      53802 [ =          0
      3 : [      53802 ;      53803 [ =          0
      4 : [      53803 ;      53804 ] =          6

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

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

    minimum value =              56435
    maximum value =              58171

      1 : [      56435 ;      56782 [ =          1
      2 : [      56782 ;      57129 [ =          1
      3 : [      57129 ;      57476 [ =          1
      4 : [      57476 ;      57823 [ =          2
      5 : [      57823 ;      58171 ] =          2

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

 Histogram of the number of ghost cells per rank:

    minimum value =               2631
    maximum value =               4367

      1 : [       2631 ;       2978 [ =          1
      2 : [       2978 ;       3325 [ =          1
      3 : [       3325 ;       3672 [ =          1
      4 : [       3672 ;       4019 [ =          2
      5 : [       4019 ;       4367 ] =          2

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

 Histogram of the number of interior faces per rank:

    minimum value =             135346
    maximum value =             137046

      1 : [     135346 ;     135686 [ =          4
      2 : [     135686 ;     136026 [ =          2
      3 : [     136026 ;     136366 [ =          0
      4 : [     136366 ;     136706 [ =          0
      5 : [     136706 ;     137046 ] =          1

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

 Histogram of the number of boundary faces per rank:

    minimum value =              54904
    maximum value =              55872

      1 : [      54904 ;      55097 [ =          1
      2 : [      55097 ;      55291 [ =          0
      3 : [      55291 ;      55484 [ =          2
      4 : [      55484 ;      55678 [ =          1
      5 : [      55678 ;      55872 ] =          3

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

 Histogram of the number of interior faces per cell:

    minimum value =                  3
    maximum value =                 11

      1 : [          3 ;          4 [ =      12048
      2 : [          4 ;          6 [ =     364000
      3 : [          6 ;          7 [ =        432
      4 : [          7 ;          9 [ =         96
      5 : [          9 ;         11 ] =         48

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

 Histogram of the number of neighboring domains per rank:

    minimum value =                  3
    maximum value =                  6

      1 : [          3 ;          4 [ =          1
      2 : [          4 ;          5 [ =          1
      3 : [          5 ;          6 ] =          5

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

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

 Start unwarping algorithm


  Histogram of the boundary faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.46280e+01

      1 : [ 0.00000e+00 ; 1.46280e+00 [ =     388632
      2 : [ 1.46280e+00 ; 2.92559e+00 [ =          0
      3 : [ 2.92559e+00 ; 4.38839e+00 [ =          0
      4 : [ 4.38839e+00 ; 5.85118e+00 [ =          0
      5 : [ 5.85118e+00 ; 7.31398e+00 [ =          0
      6 : [ 7.31398e+00 ; 8.77678e+00 [ =          0
      7 : [ 8.77678e+00 ; 1.02396e+01 [ =          0
      8 : [ 1.02396e+01 ; 1.17024e+01 [ =          0
      9 : [ 1.17024e+01 ; 1.31652e+01 [ =          0
     10 : [ 1.31652e+01 ; 1.46280e+01 ] =         48

  Histogram of the interior faces warping before unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.68512e+01

      1 : [ 0.00000e+00 ; 2.10640e+00 [ =     936708
      2 : [ 2.10640e+00 ; 4.21280e+00 [ =          0
      3 : [ 4.21280e+00 ; 6.31920e+00 [ =          0
      4 : [ 6.31920e+00 ; 8.42560e+00 [ =          0
      5 : [ 8.42560e+00 ; 1.05320e+01 [ =          0
      6 : [ 1.05320e+01 ; 1.26384e+01 [ =          0
      7 : [ 1.26384e+01 ; 1.47448e+01 [ =          0
      8 : [ 1.47448e+01 ; 1.68512e+01 ] =         24

Unwarping algorithm converged at iteration 51 

  Histogram of the boundary faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.46722e+01

      1 : [ 0.00000e+00 ; 1.46280e+00 [ =     388632
      2 : [ 1.46280e+00 ; 2.92559e+00 [ =          0
      3 : [ 2.92559e+00 ; 4.38839e+00 [ =          0
      4 : [ 4.38839e+00 ; 5.85118e+00 [ =          0
      5 : [ 5.85118e+00 ; 7.31398e+00 [ =          0
      6 : [ 7.31398e+00 ; 8.77678e+00 [ =          0
      7 : [ 8.77678e+00 ; 1.02396e+01 [ =          0
      8 : [ 1.02396e+01 ; 1.17024e+01 [ =          0
      9 : [ 1.17024e+01 ; 1.31652e+01 [ =          0
     10 : [ 1.31652e+01 ; 1.46280e+01 ] =         48

  Histogram of the interior faces warping after unwarping algorithm:

    minimum value =         0.00000e+00
    maximum value =         1.67264e+01

      1 : [ 0.00000e+00 ; 2.10640e+00 [ =     936708
      2 : [ 2.10640e+00 ; 4.21280e+00 [ =          0
      3 : [ 4.21280e+00 ; 6.31920e+00 [ =          0
      4 : [ 6.31920e+00 ; 8.42560e+00 [ =          0
      5 : [ 8.42560e+00 ; 1.05320e+01 [ =          0
      6 : [ 1.05320e+01 ; 1.26384e+01 [ =          0
      7 : [ 1.26384e+01 ; 1.47448e+01 [ =          0
      8 : [ 1.47448e+01 ; 1.68512e+01 ] =         24

 End unwarping algorithm


 Writing file:        mesh_output
 Finished writing:    mesh_output

 Renumbering mesh:

Checking mesh renumbering for threads:
-------------------------------------


 Histogram of volume mesh matrix bandwidth per rank:

    minimum value =              42750
    maximum value =              57495

      1 : [      42750 ;      45699 [ =          1
      2 : [      45699 ;      48648 [ =          0
      3 : [      48648 ;      51597 [ =          0
      4 : [      51597 ;      54546 [ =          1
      5 : [      54546 ;      57495 ] =          5

 Histogram of volume mesh matrix profile/lines per rank:

    minimum value =               3606
    maximum value =               8947

      1 : [       3606 ;       4674 [ =          3
      2 : [       4674 ;       5742 [ =          2
      3 : [       5742 ;       6810 [ =          1
      4 : [       6810 ;       7878 [ =          0
      5 : [       7878 ;       8947 ] =          1

 Mesh coordinates:               minimum    and maximum
                       X : -6.2077834e-09  2.7200001e-01
                       Y : -2.5000000e+01  3.0000000e+01
                       Z : -1.4234303e+01  1.4234303e+01
 Mesh
     Number of cells:          376624
     Number of interior faces: 936732
     Number of boundary faces: 388680
     Number of vertices:       575605

 Groups:
    "row01Farfield_001"
       cells:                 20000
    "row01Farfield_002"
       cells:                  2000
    "row01Farfield_003"
       cells:                 20000
    "row01Farfield_004"
       cells:                  4000
    "row01Inlet"
       boundary faces:          200
    "row01Interface"
       interior faces:         2464
    "row01InviscidWall"
       boundary faces:        46520
    "row01Outlet"
       boundary faces:          200
    "row02Blade"
       boundary faces:         3840
    "row02Inlet"
       interior faces:         2464
    "row02InviscidWall"
       boundary faces:       149760
    "row02Outlet"
       boundary faces:         1728
    "row02Vane_001"
       cells:                  2016
    "row02Vane_002"
       cells:                  7680
    "row02Vane_003"
       cells:                   120
    "row02Vane_004"
       cells:                   120
    "row02Vane_005"
       cells:                   120
    "row02Vane_006"
       cells:                   120
    "row02Vane_007"
       cells:                  2304
    "row02Vane_008"
       cells:                  2016
    "row02Vane_009"
       cells:                  7680
    "row02Vane_010"
       cells:                   120
    "row02Vane_011"
       cells:                   120
    "row02Vane_012"
       cells:                   120
    "row02Vane_013"
       cells:                   120
    "row02Vane_014"
       cells:                  2304
    "row02Vane_015"
       cells:                  2016
    "row02Vane_016"
       cells:                  7680
    "row02Vane_017"
       cells:                   120
    "row02Vane_018"
       cells:                   120
    "row02Vane_019"
       cells:                   120
    "row02Vane_020"
       cells:                   120
    "row02Vane_021"
       cells:                  2304
    "row02Vane_022"
       cells:                  2016
    "row02Vane_023"
       cells:                  7680
    "row02Vane_024"
       cells:                   120
    "row02Vane_025"
       cells:                   120
    "row02Vane_026"
       cells:                   120
    "row02Vane_027"
       cells:                   120
    "row02Vane_028"
       cells:                  2304
    "row02Vane_029"
       cells:                  2016
    "row02Vane_030"
       cells:                  7680
    "row02Vane_031"
       cells:                   120
    "row02Vane_032"
       cells:                   120
    "row02Vane_033"
       cells:                   120
    "row02Vane_034"
       cells:                   120
    "row02Vane_035"
       cells:                  2304
    "row02Vane_036"
       cells:                  2016
    "row02Vane_037"
       cells:                  7680
    "row02Vane_038"
       cells:                   120
    "row02Vane_039"
       cells:                   120
    "row02Vane_040"
       cells:                   120
    "row02Vane_041"
       cells:                   120
    "row02Vane_042"
       cells:                  2304
    "row02Vane_043"
       cells:                  2016
    "row02Vane_044"
       cells:                  7680
    "row02Vane_045"
       cells:                   120
    "row02Vane_046"
       cells:                   120
    "row02Vane_047"
       cells:                   120
    "row02Vane_048"
       cells:                   120
    "row02Vane_049"
       cells:                  2304
    "row02Vane_050"
       cells:                  2016
    "row02Vane_051"
       cells:                  7680
    "row02Vane_052"
       cells:                   120
    "row02Vane_053"
       cells:                   120
    "row02Vane_054"
       cells:                   120
    "row02Vane_055"
       cells:                   120
    "row02Vane_056"
       cells:                  2304
    "row02Vane_057"
       cells:                  2016
    "row02Vane_058"
       cells:                  7680
    "row02Vane_059"
       cells:                   120
    "row02Vane_060"
       cells:                   120
    "row02Vane_061"
       cells:                   120
    "row02Vane_062"
       cells:                   120
    "row02Vane_063"
       cells:                  2304
    "row02Vane_064"
       cells:                  2016
    "row02Vane_065"
       cells:                  7680
    "row02Vane_066"
       cells:                   120
    "row02Vane_067"
       cells:                   120
    "row02Vane_068"
       cells:                   120
    "row02Vane_069"
       cells:                   120
    "row02Vane_070"
       cells:                  2304
    "row02Vane_071"
       cells:                  2016
    "row02Vane_072"
       cells:                  7680
    "row02Vane_073"
       cells:                   120
    "row02Vane_074"
       cells:                   120
    "row02Vane_075"
       cells:                   120
    "row02Vane_076"
       cells:                   120
    "row02Vane_077"
       cells:                  2304
    "row02Vane_078"
       cells:                  2016
    "row02Vane_079"
       cells:                  7680
    "row02Vane_080"
       cells:                   120
    "row02Vane_081"
       cells:                   120
    "row02Vane_082"
       cells:                   120
    "row02Vane_083"
       cells:                   120
    "row02Vane_084"
       cells:                  2304
    "row03BladeWall"
       boundary faces:         3840
    "row03Blade_001"
       cells:                  2016
    "row03Blade_002"
       cells:                  7680
    "row03Blade_003"
       cells:                   120
    "row03Blade_004"
       cells:                   120
    "row03Blade_005"
       cells:                   120
    "row03Blade_006"
       cells:                   120
    "row03Blade_007"
       cells:                  2304
    "row03Blade_008"
       cells:                  2592
    "row03Blade_009"
       cells:                  2016
    "row03Blade_010"
       cells:                  7680
    "row03Blade_011"
       cells:                   120
    "row03Blade_012"
       cells:                   120
    "row03Blade_013"
       cells:                   120
    "row03Blade_014"
       cells:                   120
    "row03Blade_015"
       cells:                  2304
    "row03Blade_016"
       cells:                  2592
    "row03Blade_017"
       cells:                  2016
    "row03Blade_018"
       cells:                  7680
    "row03Blade_019"
       cells:                   120
    "row03Blade_020"
       cells:                   120
    "row03Blade_021"
       cells:                   120
    "row03Blade_022"
       cells:                   120
    "row03Blade_023"
       cells:                  2304
    "row03Blade_024"
       cells:                  2592
    "row03Blade_025"
       cells:                  2016
    "row03Blade_026"
       cells:                  7680
    "row03Blade_027"
       cells:                   120
    "row03Blade_028"
       cells:                   120
    "row03Blade_029"
       cells:                   120
    "row03Blade_030"
       cells:                   120
    "row03Blade_031"
       cells:                  2304
    "row03Blade_032"
       cells:                  2592
    "row03Blade_033"
       cells:                  2016
    "row03Blade_034"
       cells:                  7680
    "row03Blade_035"
       cells:                   120
    "row03Blade_036"
       cells:                   120
    "row03Blade_037"
       cells:                   120
    "row03Blade_038"
       cells:                   120
    "row03Blade_039"
       cells:                  2304
    "row03Blade_040"
       cells:                  2592
    "row03Blade_041"
       cells:                  2016
    "row03Blade_042"
       cells:                  7680
    "row03Blade_043"
       cells:                   120
    "row03Blade_044"
       cells:                   120
    "row03Blade_045"
       cells:                   120
    "row03Blade_046"
       cells:                   120
    "row03Blade_047"
       cells:                  2304
    "row03Blade_048"
       cells:                  2592
    "row03Blade_049"
       cells:                  2016
    "row03Blade_050"
       cells:                  7680
    "row03Blade_051"
       cells:                   120
    "row03Blade_052"
       cells:                   120
    "row03Blade_053"
       cells:                   120
    "row03Blade_054"
       cells:                   120
    "row03Blade_055"
       cells:                  2304
    "row03Blade_056"
       cells:                  2592
    "row03Blade_057"
       cells:                  2016
    "row03Blade_058"
       cells:                  7680
    "row03Blade_059"
       cells:                   120
    "row03Blade_060"
       cells:                   120
    "row03Blade_061"
       cells:                   120
    "row03Blade_062"
       cells:                   120
    "row03Blade_063"
       cells:                  2304
    "row03Blade_064"
       cells:                  2592
    "row03Blade_065"
       cells:                  2016
    "row03Blade_066"
       cells:                  7680
    "row03Blade_067"
       cells:                   120
    "row03Blade_068"
       cells:                   120
    "row03Blade_069"
       cells:                   120
    "row03Blade_070"
       cells:                   120
    "row03Blade_071"
       cells:                  2304
    "row03Blade_072"
       cells:                  2592
    "row03Blade_073"
       cells:                  2016
    "row03Blade_074"
       cells:                  7680
    "row03Blade_075"
       cells:                   120
    "row03Blade_076"
       cells:                   120
    "row03Blade_077"
       cells:                   120
    "row03Blade_078"
       cells:                   120
    "row03Blade_079"
       cells:                  2304
    "row03Blade_080"
       cells:                  2592
    "row03Blade_081"
       cells:                  2016
    "row03Blade_082"
       cells:                  7680
    "row03Blade_083"
       cells:                   120
    "row03Blade_084"
       cells:                   120
    "row03Blade_085"
       cells:                   120
    "row03Blade_086"
       cells:                   120
    "row03Blade_087"
       cells:                  2304
    "row03Blade_088"
       cells:                  2592
    "row03Blade_089"
       cells:                  2016
    "row03Blade_090"
       cells:                  7680
    "row03Blade_091"
       cells:                   120
    "row03Blade_092"
       cells:                   120
    "row03Blade_093"
       cells:                   120
    "row03Blade_094"
       cells:                   120
    "row03Blade_095"
       cells:                  2304
    "row03Blade_096"
       cells:                  2592
    "row03Inlet"
       boundary faces:         1728
    "row03InviscidWall"
       boundary faces:       180864

 --- Information on the volumes
       Minimum control volume      =  1.3255791e-08
       Maximum control volume      =  8.6193480e-02
       Total volume for the domain =  3.0741166e+02

  Criterion 1: Orthogonality:
    Number of bad cells detected: 312 -->   0 %

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

  Criterion 3: Least-Squares Gradient Quality:
    Number of bad cells detected: 69816 -->  19 %

  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 (0.196 s)
  Global number of boundary faces selected for joining:       3456
  Global min/max. tolerance:

 Glob. Num. |  Tolerance  |              Coordinates

      87200 |    0.000001 |  0.0000000000e+00  -5.4481406453e-01  -3.1155752226e-01 | ORI
     299068 |    0.000048 |  1.3600000000e-01  -6.2626714278e-01   4.0989429275e-02 | ORI
  Determination of possible face intersections:

    bounding-box tree layout: 2D

  Global number of intersections detected:        15240
    Vertex-Vertex intersections:             340
    Other intersections:                   14900

  Global number of new vertices to create:       6900

  Equivalences broken for 0 edges.

  Edge intersections and vertex creation done.

  Pre-merge for 11767 global element couples.

  Max size of a merge set of vertices: 3

  Excessive transitivity for 12 set(s) of vertices.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Edge removed for 0 faces (global).
  Join mesh cleaning done.

  Merge vertices and mesh update done.

  Mesh cleaning done for degenerate faces.
    Global number of cleaned interior faces:        0
    Global number of cleaned border faces:          0
                                                             
       ALMAX  =    0.67361E+01 (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          0.1400E+02  0.1400E+02
  Velocity          0.0000E+00  0.0000E+00
  Pressure          0.0000E+00  0.0000E+00
  k                 0.6000E-03  0.6000E-03
  omega             0.3636E-02  0.3636E-02
 ---------------------------------

                dt  0.1000E+00  0.1000E+00
 ---------------------------------



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

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



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



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


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




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


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


 -----------------------------------------
 Property           Min. value  Max. value
 -----------------------------------------
  density           0.1179E+01  0.1179E+01
  molecular_viscos  0.1830E-04  0.1830E-04
  turbulent_viscos  0.1945E+00  0.1945E+00
 -----------------------------------------



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

-------------------------------------------------------------------------
Boundary type          Code    Nb faces
-------------------------------------------------------------------------
Inlet                     2         200
Smooth wall               5        7680
Rough wall                6           0
Symmetry                  4      377144
Free outlet               3         200
Free inlet               13           0
Undefined                 1           0
-------------------------------------------------------------------------


Boundary faces with free inlet/outlet detected
Update of reference point for total pressure
 XYZP0 =    0.68000E-01   0.30000E+02  -0.10000E+00



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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200         0.000000000E+00
Smooth wall               5        7680         0.000000000E+00
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144         0.000000000E+00
Free outlet               3         200         0.000000000E+00
Free inlet               13           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 0.13515E+02
   Friction velocity        uet   :  0.16117E-01 0.18313E+01
   Friction velocity        uk    :  0.15968E-01 0.33077E+01
   Dimensionless distance   yplus :  0.22430E+00 0.15784E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :          0
   Nb of faces within the viscous sub-layer     :        324
   Total number of wall faces                   :       7680
------------------------------------------------------------


@                                                            
@ @@ WARNING: Wall distance calculation                      
@    =========                                               
@  The laplacian solution does not respect the maximum       
@  principle. We recompute the laplacien without             
@  reconstructions.                                          

                                                             
 ** WALL DISTANCE                                            
    -------------                                            
                                                             
  Min distance =    0.21204E-04 Max distance =    0.35542E+02
                                                             
     (Distance calculation done in       3679 iterations)


   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.51625E+03   10000   0.42841E+00   0.40027E+02 
c  VelocityY    0.51625E+03   10000   0.42841E+00   0.00000E+00 
c  VelocityZ    0.51625E+03   10000   0.42841E+00   0.00000E+00 
c  Pressure     0.61721E+01    6249   0.31754E+00   0.10021E+01 
c  k            0.24674E+04    8803   0.20947E-01   0.10031E+01 
c  omega        0.12790E+14   10000   0.12852E+01   0.60816E+25 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step        7.66e-08                         19468


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0099          3.0099       8.456e-11     -6.5615e-16
v  Velocity[Y]                 -38.119          94.931          12.659          19.738
v  Velocity[Z]                 -61.521          75.421         0.52118       0.0015735
v  ǁVelocityǁ                  0.11421          94.958          14.314          19.848
v  Pressure                     38.556          4046.9          2306.6          2125.1
v  k                        0.00040975          34.304          1.5549       0.0083636
v  omega                        59.047      1.1345e+14      2.0036e+12      3.7315e+09
v  turbulent_viscosity         0.19447         0.19447         0.19447         0.19447
v  CourantNb                         0               0               0               0
v  FourierNb                    1.2042      1.3055e+06          6298.6          5.3541
v  total_pressure           1.0136e+05      1.0537e+05      1.0363e+05      1.0345e+05
v  Local Time Step                0.01            0.11         0.01558         0.10734


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.2042      1.3055e+06          6298.6          5.3541


 TIME FOR THE TIME STEP                1:        0.19102E+03

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


 INSTANT    0.200000000E+00   TIME STEP NUMBER               2
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.314412807E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.15975E+03 0.34954E+01
   Friction velocity        uet   :  0.18859E-01 0.80467E+01
   Friction velocity        uk    :  0.32490E+00 0.33840E+01
   Dimensionless distance   yplus :  0.22848E+01 0.18850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       7212
   Nb of faces within the viscous sub-layer     :          2
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.27819E+04     566   0.61849E-02   0.41082E+01 
c  VelocityY    0.27819E+04     566   0.61849E-02   0.00000E+00 
c  VelocityZ    0.27819E+04     566   0.61849E-02   0.00000E+00 
c  Pressure     0.16551E+01    7239   0.26998E+00   0.10023E+01 
c  k            0.19457E+03      31   0.25056E-04   0.10022E+01 
c  omega        0.22914E+23       2   0.40852E-13   0.15204E+25 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.5078e-10                             2
a  omega          
a  Local Time Step       6.794e-06                         45956


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6253          2.6253      1.8591e-09     -3.9164e-11
v  Velocity[Y]                 -20.859          85.013          12.397          20.015
v  Velocity[Z]                 -58.575           56.97          0.3377       0.0014504
v  ǁVelocityǁ                 0.063997          85.075          13.571          20.135
v  Pressure                    -72.804          1763.5          756.15          780.15
v  k                        2.8201e-12        0.036829      6.4762e-05       0.0026416
v  omega                        58.585      5.6727e+13      1.0018e+12      1.8657e+09
v  turbulent_viscosity      2.8489e-15      0.00026124      4.8042e-07      1.8609e-05
v  CourantNb                   0.42243          7112.3          90.983          1.3945
v  FourierNb                1.8146e-05          288.33         0.63855      0.00045546
v  total_pressure           1.0125e+05      1.0309e+05      1.0208e+05      1.0211e+05
v  Local Time Step                0.01           0.121        0.010726        0.043141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81146          7127.9          91.621           1.395


 TIME FOR THE TIME STEP                2:        0.29574E+02

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


 INSTANT    0.300000000E+00   TIME STEP NUMBER               3
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.463605220E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35023E+03 0.19960E+01
   Friction velocity        uet   :  0.50765E-01 0.63420E+01
   Friction velocity        uk    :  0.79825E-01 0.31484E+01
   Dimensionless distance   yplus :  0.26944E+00 0.35753E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5280
   Nb of faces within the viscous sub-layer     :        456
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29487E+04     557   0.49453E-02   0.14579E+01 
c  VelocityY    0.29487E+04     557   0.49453E-02   0.00000E+00 
c  VelocityZ    0.29487E+04     557   0.49453E-02   0.00000E+00 
c  Pressure     0.11881E+01    7233   0.17854E+00   0.75859E+00 
c  k            0.14138E+01      68   0.95312E-08   0.24047E-04 
c  omega        0.57284E+22       2   0.81700E-13   0.38010E+24 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3154e-09                            52
a  omega          
a  Local Time Step      7.5005e-06                         46072


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5404          2.5404      1.0627e-08     -6.5087e-11
v  Velocity[Y]                 -14.173          73.458          11.143          20.082
v  Velocity[Z]                 -55.289          45.882         0.24113       0.0012007
v  ǁVelocityǁ                  0.12081          74.124          12.475          20.207
v  Pressure                    -149.69          684.57          182.18          259.17
v  k                         1.871e-22        0.044873      5.9615e-05       0.0029149
v  omega                        58.128      2.8363e+13      5.0089e+11      9.3287e+08
v  turbulent_viscosity       7.375e-25      0.00032923      4.4291e-07      1.8713e-05
v  CourantNb                  0.044629          4545.2          78.028          1.3873
v  FourierNb                1.7952e-05          288.33         0.62266       0.0004685
v  total_pressure           1.0118e+05      1.0201e+05      1.0151e+05      1.0158e+05
v  Local Time Step                0.01          0.1331        0.010746        0.044302


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34198          4560.7          78.651          1.3877


 TIME FOR THE TIME STEP                3:        0.31824E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.194252845E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29913E+03 0.14356E+01
   Friction velocity        uet   :  0.52209E-01 0.56346E+01
   Friction velocity        uk    :  0.67641E-01 0.23632E+01
   Dimensionless distance   yplus :  0.16954E+00 0.33935E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       5084
   Nb of faces within the viscous sub-layer     :        768
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29247E+04     549   0.42428E-02   0.83964E+00 
c  VelocityY    0.29247E+04     549   0.42428E-02   0.00000E+00 
c  VelocityZ    0.29247E+04     549   0.42428E-02   0.00000E+00 
c  Pressure     0.84159E+00    7188   0.13400E+00   0.49789E+00 
c  k            0.14516E+01      70   0.19120E-07   0.10348E-03 
c  omega        0.14321E+22       2   0.16340E-12   0.95025E+23 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2613e-09                          4941
a  omega          
a  Local Time Step      9.2566e-06                         46108


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4876          2.4876      5.1226e-10     -9.7354e-11
v  Velocity[Y]                 -16.212          55.641          9.6638          20.067
v  Velocity[Z]                 -47.461          35.039          0.2221      0.00088386
v  ǁVelocityǁ                  0.11014          57.318          11.595          20.196
v  Pressure                    -399.82          293.99         -75.471          20.261
v  k                             1e-24        0.059204      6.8137e-05       0.0040749
v  omega                        39.485      1.4182e+13      2.5044e+11      4.6644e+08
v  turbulent_viscosity      9.8915e-35      0.00075595      6.3992e-07      3.9826e-05
v  CourantNb                   0.14921          2797.1          65.222          1.3846
v  FourierNb                1.7826e-05          161.89         0.61776      0.00066214
v  total_pressure           1.0093e+05      1.0162e+05      1.0125e+05      1.0135e+05
v  Local Time Step                0.01         0.14641        0.010748        0.044858


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25098          2803.1           65.84          1.3853


 TIME FOR THE TIME STEP                4:        0.32418E+02

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


 INSTANT    0.500000000E+00   TIME STEP NUMBER               5
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.235543211E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.19311E+03 0.12516E+01
   Friction velocity        uet   :  0.35259E-01 0.44846E+01
   Friction velocity        uk    :  0.35259E-01 0.21678E+01
   Dimensionless distance   yplus :  0.17200E+00 0.29195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4958
   Nb of faces within the viscous sub-layer     :        912
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28940E+04     534   0.29327E-02   0.71074E+00 
c  VelocityY    0.28940E+04     534   0.29327E-02   0.00000E+00 
c  VelocityZ    0.28940E+04     534   0.29327E-02   0.00000E+00 
c  Pressure     0.53468E+00    7070   0.72647E-01   0.29342E+00 
c  k            0.15861E+01      71   0.51575E-07   0.15515E-03 
c  omega        0.35803E+21       2   0.32680E-12   0.23755E+23 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.9854e-09                         11429
a  omega          
a  Local Time Step      1.1756e-05                         46085


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6561          2.6561     -1.5854e-08     -9.4335e-11
v  Velocity[Y]                 -16.325          39.199          8.3199          20.056
v  Velocity[Z]                  -38.85          33.432         0.24485      0.00056726
v  ǁVelocityǁ                 0.053377          43.536           11.02          20.189
v  Pressure                    -374.11          269.37         -105.54          4.8626
v  k                             1e-24        0.073494      8.4148e-05       0.0056799
v  omega                        25.447      7.0909e+12      1.2522e+11      2.3322e+08
v  turbulent_viscosity      8.6858e-38       0.0017672      1.2273e-06      9.6714e-05
v  CourantNb                  0.067614          2489.2          57.861          1.3832
v  FourierNb                1.7738e-05          122.83         0.61199       0.0011637
v  total_pressure           1.0095e+05      1.0159e+05      1.0122e+05      1.0133e+05
v  Local Time Step                0.01         0.14894         0.01075        0.045058


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26707          2502.5          58.473          1.3844


 TIME FOR THE TIME STEP                5:        0.30080E+02

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


 INSTANT    0.600000000E+00   TIME STEP NUMBER               6
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.305906867E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.12274E+03 0.12521E+01
   Friction velocity        uet   :  0.38871E-01 0.33780E+01
   Friction velocity        uk    :  0.38871E-01 0.21051E+01
   Dimensionless distance   yplus :  0.10215E+00 0.25416E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4816
   Nb of faces within the viscous sub-layer     :        928
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28876E+04     507   0.19384E-02   0.57085E+00 
c  VelocityY    0.28876E+04     507   0.19384E-02   0.00000E+00 
c  VelocityZ    0.28876E+04     507   0.19384E-02   0.00000E+00 
c  Pressure     0.37710E+00    7108   0.57930E-01   0.19839E+00 
c  k            0.17937E+01      71   0.82505E-07   0.17629E-03 
c  omega        0.89507E+20       2   0.65361E-12   0.59388E+22 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.8735e-09                         13598
a  omega          
a  Local Time Step       1.645e-05                         46037


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1234          2.1234      -1.356e-08     -9.1655e-11
v  Velocity[Y]                 -21.522          28.345          7.2492          20.049
v  Velocity[Z]                 -32.378          28.761         0.29817      0.00032698
v  ǁVelocityǁ                 0.022736          33.621          10.674          20.185
v  Pressure                    -342.75          284.04         -85.335          33.308
v  k                             1e-24        0.086046      0.00010499       0.0075001
v  omega                        18.488      3.5454e+12      6.2611e+10      1.1661e+08
v  turbulent_viscosity      1.6768e-37        0.003404      2.4169e-06       0.0002071
v  CourantNb                  0.022385          2381.5           53.05          1.3805
v  FourierNb                1.7673e-05          122.83         0.60586       0.0021086
v  total_pressure           1.0098e+05      1.0161e+05      1.0124e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010752         0.04515


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.069046          2394.8          53.655          1.3826


 TIME FOR THE TIME STEP                6:        0.31636E+02

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


 INSTANT    0.700000000E+00   TIME STEP NUMBER               7
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.506059197E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.68904E+02 0.16870E+01
   Friction velocity        uet   :  0.48147E-01 0.27355E+01
   Friction velocity        uk    :  0.49497E-01 0.19920E+01
   Dimensionless distance   yplus :  0.14592E+00 0.20959E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4764
   Nb of faces within the viscous sub-layer     :        894
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28918E+04     473   0.18713E-02   0.51600E+00 
c  VelocityY    0.28918E+04     473   0.18713E-02   0.00000E+00 
c  VelocityZ    0.28918E+04     473   0.18713E-02   0.00000E+00 
c  Pressure     0.29430E+00    7126   0.59082E-01   0.15012E+00 
c  k            0.20411E+01      72   0.10690E-06   0.17680E-03 
c  omega        0.22377E+20       3   0.13072E-11   0.14847E+22 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0892e-08                         14051
a  omega          
a  Local Time Step      1.9438e-05                         46035


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9571          1.9571     -1.4984e-08     -7.8773e-11
v  Velocity[Y]                 -23.678           25.61          6.5236          20.047
v  Velocity[Z]                 -31.885          23.452         0.37493      0.00019588
v  ǁVelocityǁ                 0.034655          32.628          10.513          20.187
v  Pressure                    -337.93          284.64         -74.834          46.789
v  k                             1e-24        0.094696      0.00012867       0.0093623
v  omega                        15.379      1.7727e+12      3.1306e+10      5.8305e+07
v  turbulent_viscosity      3.3696e-37       0.0053374      4.2385e-06       0.0003687
v  CourantNb                  0.011162          2290.3           49.44          1.3786
v  FourierNb                1.7623e-05          122.83         0.60644       0.0034126
v  total_pressure           1.0099e+05      1.0161e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14847        0.010748         0.04498


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16573          2303.6          50.046           1.382


 TIME FOR THE TIME STEP                7:        0.29980E+02

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


 INSTANT    0.800000000E+00   TIME STEP NUMBER               8
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.341838807E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61430E+02 0.18249E+01
   Friction velocity        uet   :  0.19405E-01 0.26339E+01
   Friction velocity        uk    :  0.19405E-01 0.18626E+01
   Dimensionless distance   yplus :  0.50994E-01 0.19544E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4600
   Nb of faces within the viscous sub-layer     :        948
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28963E+04     454   0.24873E-02   0.49626E+00 
c  VelocityY    0.28963E+04     454   0.24873E-02   0.00000E+00 
c  VelocityZ    0.28963E+04     454   0.24873E-02   0.00000E+00 
c  Pressure     0.27418E+00    7085   0.58775E-01   0.13694E+00 
c  k            0.22862E+01      72   0.92931E-07   0.17075E-03 
c  omega        0.55942E+19       3   0.26144E-11   0.37119E+21 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5597e-08                         13683
a  omega          
a  Local Time Step      1.9956e-05                         46009


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6225          1.6225     -9.5911e-09      1.9289e-11
v  Velocity[Y]                 -24.638          25.619          6.0948          20.047
v  Velocity[Z]                 -30.077          20.796         0.44041       0.0001234
v  ǁVelocityǁ                 0.034334          30.438          10.461          20.189
v  Pressure                    -327.87          275.12         -74.929          47.174
v  k                             1e-24         0.10094      0.00015431        0.011184
v  omega                        14.016      8.8636e+11      1.5653e+10      2.9152e+07
v  turbulent_viscosity      6.8725e-37       0.0069858      6.5473e-06      0.00056084
v  CourantNb                  0.081327          2162.7          46.913          1.3778
v  FourierNb                1.7593e-05          122.83          0.6078       0.0048872
v  total_pressure             1.01e+05       1.016e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14831        0.010746        0.044818


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25046            2176          47.521          1.3827


 TIME FOR THE TIME STEP                8:        0.28375E+02

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


 INSTANT    0.900000000E+00   TIME STEP NUMBER               9
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.408519623E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50004E+02 0.18284E+01
   Friction velocity        uet   :  0.14285E-01 0.23820E+01
   Friction velocity        uk    :  0.14281E-01 0.19588E+01
   Dimensionless distance   yplus :  0.84090E-01 0.18005E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4506
   Nb of faces within the viscous sub-layer     :       1128
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.28990E+04     445   0.28863E-02   0.48115E+00 
c  VelocityY    0.28990E+04     445   0.28863E-02   0.00000E+00 
c  VelocityZ    0.28990E+04     445   0.28863E-02   0.00000E+00 
c  Pressure     0.23996E+00    7085   0.56680E-01   0.11778E+00 
c  k            0.25116E+01      73   0.73493E-07   0.16080E-03 
c  omega        0.13985E+19       3   0.52288E-11   0.92795E+20 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7865e-08                         13216
a  omega          
a  Local Time Step      2.0597e-05                         45958


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4779          1.4779     -3.6632e-08      1.3111e-10
v  Velocity[Y]                 -24.694          25.652           5.881          20.046
v  Velocity[Z]                 -27.069          21.687         0.48636      7.3677e-05
v  ǁVelocityǁ                 0.017503          27.354          10.463          20.191
v  Pressure                     -316.1           264.9         -77.486          44.548
v  k                             1e-24         0.10509      0.00018104        0.012914
v  omega                        13.423      4.4318e+11      7.8264e+09      1.4576e+07
v  turbulent_viscosity      1.3957e-36       0.0081337      9.1843e-06      0.00076395
v  CourantNb                  0.026369          2011.9          45.707          1.3777
v  FourierNb                 1.757e-05          122.83         0.60678       0.0063848
v  total_pressure           1.0101e+05      1.0159e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14825        0.010747        0.044761


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.08302          2025.2          46.314          1.3841


 TIME FOR THE TIME STEP                9:        0.29785E+02

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


 INSTANT    0.100000000E+01   TIME STEP NUMBER              10
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.269288136E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47102E+02 0.17978E+01
   Friction velocity        uet   :  0.17153E-01 0.20560E+01
   Friction velocity        uk    :  0.17152E-01 0.19834E+01
   Dimensionless distance   yplus :  0.78831E-01 0.18642E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4412
   Nb of faces within the viscous sub-layer     :       1146
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29009E+04     445   0.25615E-02   0.49099E+00 
c  VelocityY    0.29009E+04     445   0.25615E-02   0.00000E+00 
c  VelocityZ    0.29009E+04     445   0.25615E-02   0.00000E+00 
c  Pressure     0.26131E+00    7013   0.54367E-01   0.12748E+00 
c  k            0.27105E+01      73   0.61103E-07   0.15001E-03 
c  omega        0.34963E+18       3   0.10458E-10   0.23199E+20 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.0325e-07                         12690
a  omega          
a  Local Time Step      2.1151e-05                         45826


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3562          1.3562     -1.4645e-08      2.7586e-10
v  Velocity[Y]                 -21.516          28.141          5.8157          20.049
v  Velocity[Z]                 -24.801          23.304         0.53934      2.3829e-05
v  ǁVelocityǁ                 0.018073          28.338          10.473          20.196
v  Pressure                    -336.86          264.39         -78.239          43.215
v  k                             1e-24         0.10772      0.00020831        0.014528
v  omega                        12.649      2.2159e+11      3.9132e+09      7.2882e+06
v  turbulent_viscosity      2.7914e-36       0.0088278      1.2059e-05      0.00096742
v  CourantNb                  0.032474          1964.3          45.287          1.3782
v  FourierNb                1.7551e-05          122.83         0.60617       0.0078284
v  total_pressure           1.0099e+05      1.0159e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14824        0.010749        0.044767


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.19014          1977.6          45.894          1.3861


 TIME FOR THE TIME STEP               10:        0.30578E+02

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


 INSTANT    0.110000000E+01   TIME STEP NUMBER              11
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.320636481E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.71344E+02 0.23613E+01
   Friction velocity        uet   :  0.11423E-01 0.24839E+01
   Friction velocity        uk    :  0.11415E-01 0.21309E+01
   Dimensionless distance   yplus :  0.72826E-01 0.21243E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4412
   Nb of faces within the viscous sub-layer     :       1194
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29026E+04     460   0.24636E-02   0.52287E+00 
c  VelocityY    0.29026E+04     460   0.24636E-02   0.00000E+00 
c  VelocityZ    0.29026E+04     460   0.24636E-02   0.00000E+00 
c  Pressure     0.27214E+00    7031   0.53887E-01   0.13260E+00 
c  k            0.28910E+01      74   0.64194E-07   0.13995E-03 
c  omega        0.87409E+17       3   0.20915E-10   0.57996E+19 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.324e-07                         12149
a  omega          
a  Local Time Step       2.151e-05                         45731


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2495          1.2495     -4.4331e-08      4.5668e-10
v  Velocity[Y]                 -23.726          30.064          5.8192          20.049
v  Velocity[Z]                 -25.898          24.439         0.55484     -4.8914e-06
v  ǁVelocityǁ                 0.026359          30.304          10.527          20.198
v  Pressure                     -357.2          265.25         -76.797          42.626
v  k                             1e-24         0.10888      0.00023584         0.01602
v  omega                        12.114      1.1079e+11      1.9566e+09      3.6441e+06
v  turbulent_viscosity      5.4035e-36       0.0092201      1.5111e-05       0.0011655
v  CourantNb                  0.038967          1961.5          45.136           1.379
v  FourierNb                1.7535e-05          122.83         0.60658       0.0092131
v  total_pressure           1.0097e+05      1.0159e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14847        0.010752        0.044876


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.065239          1974.8          45.742          1.3882


 TIME FOR THE TIME STEP               11:        0.29098E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.664003156E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78322E+02 0.25977E+01
   Friction velocity        uet   :  0.14891E-01 0.26189E+01
   Friction velocity        uk    :  0.14891E-01 0.21808E+01
   Dimensionless distance   yplus :  0.41968E-01 0.21829E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4490
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29044E+04     474   0.20850E-02   0.57206E+00 
c  VelocityY    0.29044E+04     474   0.20850E-02   0.00000E+00 
c  VelocityZ    0.29044E+04     474   0.20850E-02   0.00000E+00 
c  Pressure     0.26577E+00    7000   0.54321E-01   0.12915E+00 
c  k            0.30634E+01      74   0.70967E-07   0.13035E-03 
c  omega        0.21852E+17       3   0.41831E-10   0.14499E+19 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.8975e-07                         11573
a  omega          
a  Local Time Step      2.1651e-05                         45524


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.168           1.168     -1.3197e-08      5.0293e-10
v  Velocity[Y]                 -24.349          30.179          5.8571          20.049
v  Velocity[Z]                 -26.147          28.156          0.5438     -8.9255e-05
v  ǁVelocityǁ                 0.019602           30.57          10.575            20.2
v  Pressure                     -363.7          268.56         -74.078          42.813
v  k                             1e-24         0.10995      0.00026325        0.017384
v  omega                        11.489      5.5397e+10       9.783e+08      1.8221e+06
v  turbulent_viscosity      1.0807e-35       0.0094114      1.8296e-05       0.0013554
v  CourantNb                  0.065778          1980.7          45.397            1.38
v  FourierNb                1.7522e-05          288.33         0.60791        0.010448
v  total_pressure           1.0096e+05      1.0159e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14843        0.010752        0.044919


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25832            1994          46.004          1.3905


 TIME FOR THE TIME STEP               12:        0.30343E+02

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


 INSTANT    0.130000000E+01   TIME STEP NUMBER              13
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.537513146E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.78040E+02 0.27044E+01
   Friction velocity        uet   :  0.15164E-01 0.26223E+01
   Friction velocity        uk    :  0.15160E-01 0.23204E+01
   Dimensionless distance   yplus :  0.38575E-01 0.21741E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4494
   Nb of faces within the viscous sub-layer     :       1126
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29063E+04     480   0.20287E-02   0.61759E+00 
c  VelocityY    0.29063E+04     480   0.20287E-02   0.00000E+00 
c  VelocityZ    0.29063E+04     480   0.20287E-02   0.00000E+00 
c  Pressure     0.26546E+00    6983   0.57164E-01   0.12852E+00 
c  k            0.32281E+01      73   0.30931E-06   0.12193E-03 
c  omega        0.54630E+16       3   0.83671E-10   0.36249E+18 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.1312e-06                         10987
a  omega          
a  Local Time Step      2.0557e-05                         45346


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0202          1.0202      1.0051e-07     -6.9022e-09
v  Velocity[Y]                 -23.695          28.843          5.8958           20.05
v  Velocity[Z]                 -25.576          30.862         0.51915     -0.00015788
v  ǁVelocityǁ                 0.021679          31.087          10.586          20.202
v  Pressure                    -361.98          272.68         -71.291          43.286
v  k                             1e-24         0.11077      0.00029071        0.018625
v  omega                        11.089      2.7699e+10      4.8915e+08      9.1109e+05
v  turbulent_viscosity      2.1614e-35       0.0095754      2.1567e-05       0.0015347
v  CourantNb                  0.049735          2015.4          45.689          1.3812
v  FourierNb                1.7512e-05          288.33         0.60762        0.011555
v  total_pressure           1.0096e+05       1.016e+05      1.0125e+05      1.0137e+05
v  Local Time Step                0.01         0.14845        0.010754        0.044967


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17264          2028.7          46.296          1.3928


 TIME FOR THE TIME STEP               13:        0.29649E+02

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


 INSTANT    0.140000000E+01   TIME STEP NUMBER              14
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.230964312E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.72983E+02 0.27625E+01
   Friction velocity        uet   :  0.22843E-01 0.25368E+01
   Friction velocity        uk    :  0.22843E-01 0.23450E+01
   Dimensionless distance   yplus :  0.38708E-01 0.21217E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4418
   Nb of faces within the viscous sub-layer     :       1140
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29083E+04     483   0.25020E-02   0.64897E+00 
c  VelocityY    0.29083E+04     483   0.25020E-02   0.00000E+00 
c  VelocityZ    0.29083E+04     483   0.25020E-02   0.00000E+00 
c  Pressure     0.28710E+00    6944   0.59716E-01   0.13862E+00 
c  k            0.33901E+01      73   0.41537E-06   0.11471E-03 
c  omega        0.13658E+16       3   0.16744E-09   0.90620E+17 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2425e-06                         10401
a  omega          
a  Local Time Step       1.838e-05                         45322


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0092          1.0092      1.6453e-07     -3.3302e-09
v  Velocity[Y]                 -22.852          27.917          5.9544           20.05
v  Velocity[Z]                 -25.635          31.653         0.49365     -0.00023391
v  ǁVelocityǁ                 0.025226          32.076           10.58          20.204
v  Pressure                    -382.11          276.78         -69.409          43.755
v  k                             1e-24         0.11347       0.0003181        0.019747
v  omega                        10.605      1.3849e+10      2.4458e+08      4.5558e+05
v  turbulent_viscosity      4.3463e-35       0.0099039      2.4889e-05       0.0017031
v  CourantNb                  0.026921          2061.5          45.708          1.3823
v  FourierNb                1.7503e-05          288.33         0.60776        0.012523
v  total_pressure           1.0094e+05       1.016e+05      1.0126e+05      1.0137e+05
v  Local Time Step                0.01         0.14851        0.010756        0.044984


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.048523          2074.7          46.316          1.3949


 TIME FOR THE TIME STEP               14:        0.29155E+02

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


 INSTANT    0.150000000E+01   TIME STEP NUMBER              15
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.340660174E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58914E+02 0.26589E+01
   Friction velocity        uet   :  0.28610E-01 0.26047E+01
   Friction velocity        uk    :  0.28579E-01 0.22528E+01
   Dimensionless distance   yplus :  0.86498E-01 0.19761E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4484
   Nb of faces within the viscous sub-layer     :       1134
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29103E+04     484   0.25594E-02   0.69736E+00 
c  VelocityY    0.29103E+04     484   0.25594E-02   0.00000E+00 
c  VelocityZ    0.29103E+04     484   0.25594E-02   0.00000E+00 
c  Pressure     0.31986E+00    6929   0.58725E-01   0.15415E+00 
c  k            0.35498E+01      72   0.66055E-06   0.10866E-03 
c  omega        0.34144E+15       3   0.33599E-09   0.22655E+17 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -5.014e-06                          9842
a  omega          
a  Local Time Step      2.0795e-05                         45420


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.99837         0.99837      2.7721e-07     -1.6795e-09
v  Velocity[Y]                  -21.48          27.824          6.0528          20.051
v  Velocity[Z]                 -26.342          30.835          0.4691     -0.00028854
v  ǁVelocityǁ                0.0098545           31.27          10.602          20.207
v  Pressure                    -400.08          281.44         -67.973          44.317
v  k                             1e-24         0.11944      0.00034513        0.020759
v  omega                        10.268      6.9247e+09      1.2229e+08      2.2782e+05
v  turbulent_viscosity      8.7654e-35        0.010274      2.8231e-05       0.0018605
v  CourantNb                  0.068281          2140.5          45.614          1.3836
v  FourierNb                1.7495e-05          288.34         0.60911        0.013365
v  total_pressure           1.0092e+05      1.0161e+05      1.0126e+05      1.0137e+05
v  Local Time Step                0.01         0.14858        0.010756        0.044977


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15398          2153.8          46.223          1.3969


 TIME FOR THE TIME STEP               15:        0.29426E+02

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


 INSTANT    0.160000000E+01   TIME STEP NUMBER              16
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.289015583E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52370E+02 0.26199E+01
   Friction velocity        uet   :  0.21305E-01 0.25310E+01
   Friction velocity        uk    :  0.21305E-01 0.22019E+01
   Dimensionless distance   yplus :  0.11219E+00 0.19092E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4490
   Nb of faces within the viscous sub-layer     :       1150
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29123E+04     490   0.24764E-02   0.74652E+00 
c  VelocityY    0.29123E+04     490   0.24764E-02   0.00000E+00 
c  VelocityZ    0.29123E+04     490   0.24764E-02   0.00000E+00 
c  Pressure     0.32659E+00    6968   0.51043E-01   0.15680E+00 
c  k            0.37106E+01      70   0.33487E-06   0.10387E-03 
c  omega        0.85360E+14       3   0.68222E-09   0.56635E+16 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -9.711e-06                          9262
a  omega          
a  Local Time Step      2.0761e-05                         45588


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97134         0.97134      2.7818e-07     -6.1936e-10
v  Velocity[Y]                 -20.149          27.536          6.1596          20.052
v  Velocity[Z]                  -26.12          29.392         0.46104     -0.00029266
v  ǁVelocityǁ                 0.033195          30.019          10.631           20.21
v  Pressure                    -406.78           289.8         -65.732          44.914
v  k                             1e-24         0.12653       0.0003741        0.021666
v  omega                        9.8959      3.4623e+09      6.1145e+07      1.1394e+05
v  turbulent_viscosity      1.7171e-34        0.010678       3.156e-05        0.002007
v  CourantNb                  0.036801          2200.9          45.859          1.3851
v  FourierNb                1.7489e-05          288.33          0.6079        0.014123
v  total_pressure           1.0092e+05      1.0161e+05      1.0126e+05      1.0137e+05
v  Local Time Step                0.01         0.14891        0.010756        0.044996


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16766          2214.2          46.467          1.3992


 TIME FOR THE TIME STEP               16:        0.31709E+02

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


 INSTANT    0.170000000E+01   TIME STEP NUMBER              17
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.294032961E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48977E+02 0.27043E+01
   Friction velocity        uet   :  0.22779E-01 0.23952E+01
   Friction velocity        uk    :  0.22779E-01 0.23114E+01
   Dimensionless distance   yplus :  0.11321E+00 0.18943E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4512
   Nb of faces within the viscous sub-layer     :       1108
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29142E+04     492   0.24104E-02   0.77804E+00 
c  VelocityY    0.29142E+04     492   0.24104E-02   0.00000E+00 
c  VelocityZ    0.29142E+04     492   0.24104E-02   0.00000E+00 
c  Pressure     0.33128E+00    7001   0.46890E-01   0.15889E+00 
c  k            0.38812E+01      68   0.54367E-06   0.99343E-04 
c  omega        0.21340E+14       3   0.14497E-08   0.14158E+16 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.1374e-05                          8788
a  omega          
a  Local Time Step       2.041e-05                         45663


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.87605         0.87605      8.6768e-08     -3.2157e-11
v  Velocity[Y]                 -18.579          27.031          6.2543          20.052
v  Velocity[Z]                 -28.028          27.573         0.49169     -0.00029237
v  ǁVelocityǁ                 0.025245          29.643          10.661          20.212
v  Pressure                    -399.36          299.56         -61.681          45.566
v  k                             1e-24         0.13626      0.00040735        0.022476
v  omega                        9.6094      1.7312e+09      3.0573e+07           57002
v  turbulent_viscosity      3.4341e-34        0.011242      3.4844e-05       0.0021426
v  CourantNb                  0.056603          2259.2          46.205          1.3865
v  FourierNb                1.7484e-05          288.33         0.60674         0.01479
v  total_pressure           1.0093e+05      1.0162e+05      1.0126e+05      1.0137e+05
v  Local Time Step                0.01         0.14882        0.010757        0.045006


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.058089          2272.5          46.811          1.4012


 TIME FOR THE TIME STEP               17:        0.30873E+02

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


 INSTANT    0.180000000E+01   TIME STEP NUMBER              18
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.134107153E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52576E+02 0.28242E+01
   Friction velocity        uet   :  0.32822E-01 0.23923E+01
   Friction velocity        uk    :  0.32672E-01 0.26073E+01
   Dimensionless distance   yplus :  0.15269E+00 0.19165E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4512
   Nb of faces within the viscous sub-layer     :       1096
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29163E+04     495   0.20856E-02   0.78975E+00 
c  VelocityY    0.29163E+04     495   0.20856E-02   0.00000E+00 
c  VelocityZ    0.29163E+04     495   0.20856E-02   0.00000E+00 
c  Pressure     0.30735E+00    7028   0.46784E-01   0.14662E+00 
c  k            0.40652E+01      66   0.13349E-05   0.95541E-04 
c  omega        0.53349E+13       4   0.28166E-08   0.35398E+15 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.0069e-05                          8310
a  omega          
a  Local Time Step      2.0051e-05                         45686


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.7989         0.79891      1.7477e-06     -1.1961e-10
v  Velocity[Y]                 -20.849          27.134          6.3525          20.051
v  Velocity[Z]                 -28.694          26.282         0.53537     -0.00029206
v  ǁVelocityǁ                  0.02754           30.81          10.734          20.213
v  Pressure                    -379.94          309.68         -56.938          46.212
v  k                             1e-24         0.14613      0.00044945        0.023196
v  omega                        9.2802      8.6568e+08      1.5288e+07           28529
v  turbulent_viscosity      6.8679e-34        0.011775      3.8047e-05       0.0022673
v  CourantNb                  0.086465          2306.5          46.239          1.3876
v  FourierNb                 1.748e-05          288.33         0.60668        0.015356
v  total_pressure           1.0095e+05      1.0163e+05      1.0127e+05      1.0137e+05
v  Local Time Step                0.01         0.14861        0.010757        0.044982


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.12341          2319.8          46.845          1.4029


 TIME FOR THE TIME STEP               18:        0.30962E+02

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


 INSTANT    0.190000000E+01   TIME STEP NUMBER              19
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.307397786E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52637E+02 0.27720E+01
   Friction velocity        uet   :  0.16348E-01 0.24619E+01
   Friction velocity        uk    :  0.16348E-01 0.24099E+01
   Dimensionless distance   yplus :  0.78440E-01 0.18628E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4514
   Nb of faces within the viscous sub-layer     :       1086
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29185E+04     499   0.18630E-02   0.78827E+00 
c  VelocityY    0.29185E+04     499   0.18630E-02   0.00000E+00 
c  VelocityZ    0.29185E+04     499   0.18630E-02   0.00000E+00 
c  Pressure     0.28677E+00    7027   0.47540E-01   0.13605E+00 
c  k            0.42629E+01      64   0.13575E-05   0.92342E-04 
c  omega        0.13337E+13       5   0.56848E-08   0.88498E+14 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015725                          7759
a  omega          
a  Local Time Step      1.8204e-05                         45677


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80905         0.80909      1.4345e-06     -5.0539e-10
v  Velocity[Y]                 -17.891          27.538          6.4318           20.05
v  Velocity[Z]                 -28.398           27.27         0.60831     -0.00028169
v  ǁVelocityǁ                 0.014217          29.835           10.81          20.214
v  Pressure                    -369.28          319.29         -52.283          46.674
v  k                             1e-24          0.2143      0.00050765        0.023834
v  omega                        9.0629      4.3297e+08      7.6448e+06           14290
v  turbulent_viscosity      1.3903e-33        0.012442      4.1172e-05       0.0023819
v  CourantNb                  0.075342          2342.2          46.556          1.3884
v  FourierNb                1.7479e-05          288.33         0.60695        0.015857
v  total_pressure           1.0096e+05      1.0164e+05      1.0127e+05      1.0137e+05
v  Local Time Step                0.01         0.14849        0.010757        0.044958


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.28348          2355.5          47.163          1.4042


 TIME FOR THE TIME STEP               19:        0.30024E+02

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


 INSTANT    0.200000000E+01   TIME STEP NUMBER              20
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.598742940E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50011E+02 0.27767E+01
   Friction velocity        uet   :  0.14159E-01 0.23551E+01
   Friction velocity        uk    :  0.16366E-01 0.24077E+01
   Dimensionless distance   yplus :  0.12118E+00 0.18115E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4407
   Nb of faces within the viscous sub-layer     :       1156
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29209E+04     499   0.22305E-02   0.77814E+00 
c  VelocityY    0.29209E+04     499   0.22305E-02   0.00000E+00 
c  VelocityZ    0.29209E+04     499   0.22305E-02   0.00000E+00 
c  Pressure     0.28258E+00    7033   0.47232E-01   0.13324E+00 
c  k            0.44774E+01      61   0.18787E-05   0.88999E-04 
c  omega        0.33341E+12       6   0.11733E-07   0.22125E+14 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031916                          7151
a  omega          
a  Local Time Step      1.5364e-05                         45677


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.6848         0.68488      3.4602e-07     -3.2322e-10
v  Velocity[Y]                 -18.226          27.912          6.4777           20.05
v  Velocity[Z]                 -29.143          27.153         0.66142     -0.00022415
v  ǁVelocityǁ                 0.012857          29.751           10.87          20.215
v  Pressure                    -374.08          327.91         -48.198          47.185
v  k                             1e-24         0.34274      0.00059816        0.024399
v  omega                        8.8383      2.1671e+08      3.8235e+06          7168.9
v  turbulent_viscosity      2.8238e-33        0.013258      4.4164e-05       0.0024853
v  CourantNb                  0.059669          2369.2          46.752          1.3889
v  FourierNb                 1.748e-05          288.33         0.60939        0.016294
v  total_pressure           1.0095e+05      1.0165e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14845        0.010756        0.044937


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.096458          2382.5          47.362          1.4052


 TIME FOR THE TIME STEP               20:        0.32516E+02

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


 INSTANT    0.210000000E+01   TIME STEP NUMBER              21
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.587153644E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45630E+02 0.27860E+01
   Friction velocity        uet   :  0.20676E-01 0.24362E+01
   Friction velocity        uk    :  0.20466E-01 0.24061E+01
   Dimensionless distance   yplus :  0.10633E+00 0.17035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4341
   Nb of faces within the viscous sub-layer     :       1134
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29234E+04     499   0.24566E-02   0.73997E+00 
c  VelocityY    0.29234E+04     499   0.24566E-02   0.00000E+00 
c  VelocityZ    0.29234E+04     499   0.24566E-02   0.00000E+00 
c  Pressure     0.30565E+00    7011   0.48506E-01   0.14435E+00 
c  k            0.47071E+01      58   0.48537E-05   0.85555E-04 
c  omega        0.83344E+11       9   0.22657E-07   0.55311E+13 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060612                          6408
a  omega          
a  Local Time Step      1.5265e-05                         45677


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.62268         0.62275      1.6488e-06     -1.3952e-10
v  Velocity[Y]                 -17.494          28.246          6.4672           20.05
v  Velocity[Z]                 -27.726           27.78         0.71968     -0.00022577
v  ǁVelocityǁ                 0.013812          29.081          10.903          20.217
v  Pressure                    -370.27          335.36         -45.485           47.62
v  k                             1e-24          0.9183      0.00072311        0.024903
v  omega                        8.6353      1.0873e+08       1.913e+06          3606.7
v  turbulent_viscosity      5.5607e-33        0.013986      4.7001e-05       0.0025773
v  CourantNb                  0.084701          2383.1          46.799          1.3895
v  FourierNb                1.7481e-05          288.33         0.61099        0.016662
v  total_pressure           1.0095e+05      1.0166e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14843        0.010756        0.044909


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.085666          2396.4           47.41          1.4061


 TIME FOR THE TIME STEP               21:        0.30600E+02

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


 INSTANT    0.220000000E+01   TIME STEP NUMBER              22
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.372744392E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45268E+02 0.28371E+01
   Friction velocity        uet   :  0.12438E-01 0.23880E+01
   Friction velocity        uk    :  0.12313E-01 0.24934E+01
   Dimensionless distance   yplus :  0.64857E-01 0.16853E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4279
   Nb of faces within the viscous sub-layer     :       1135
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29259E+04     497   0.23967E-02   0.68857E+00 
c  VelocityY    0.29259E+04     497   0.23967E-02   0.00000E+00 
c  VelocityZ    0.29259E+04     497   0.23967E-02   0.00000E+00 
c  Pressure     0.30143E+00    6926   0.51308E-01   0.14183E+00 
c  k            0.49499E+01      60   0.35042E-05   0.81634E-04 
c  omega        0.20835E+11      16   0.43812E-07   0.13827E+13 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00090725                          5555
a  omega          
a  Local Time Step      1.8098e-05                         45688


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.50421          0.5043      2.1889e-06      1.3386e-10
v  Velocity[Y]                 -17.735          28.549          6.4114           20.05
v  Velocity[Z]                 -28.107          27.907         0.75917     -0.00016633
v  ǁVelocityǁ                 0.013117          30.214          10.928          20.219
v  Pressure                    -357.66          341.48         -43.663          47.869
v  k                             1e-24         0.60183      0.00092028        0.025353
v  omega                        8.4091      5.5039e+07      9.5788e+05          1824.3
v  turbulent_viscosity       1.112e-32        0.015147      4.9685e-05       0.0026586
v  CourantNb                  0.022465          2362.9          46.608          1.3898
v  FourierNb                1.7484e-05          288.34         0.61251        0.016983
v  total_pressure           1.0097e+05      1.0167e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14871        0.010756        0.044902


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier        0.096455          2376.2           47.22          1.4068


 TIME FOR THE TIME STEP               22:        0.28640E+02

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


 INSTANT    0.230000000E+01   TIME STEP NUMBER              23
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.545991118E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44103E+02 0.28621E+01
   Friction velocity        uet   :  0.14725E-01 0.23705E+01
   Friction velocity        uk    :  0.14909E-01 0.24501E+01
   Dimensionless distance   yplus :  0.10429E+00 0.16601E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4155
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29285E+04     492   0.23015E-02   0.64377E+00 
c  VelocityY    0.29285E+04     492   0.23015E-02   0.00000E+00 
c  VelocityZ    0.29285E+04     492   0.23015E-02   0.00000E+00 
c  Pressure     0.30939E+00    7038   0.54390E-01   0.14478E+00 
c  k            0.52050E+01      84   0.31461E-05   0.78332E-04 
c  omega        0.52095E+10      27   0.93460E-07   0.34565E+12 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023956                          4657
a  omega          
a  Local Time Step      1.9445e-05                         45651


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.41449         0.41467      3.4907e-06      6.7427e-10
v  Velocity[Y]                 -17.529          28.814          6.3268           20.05
v  Velocity[Z]                 -27.896          28.272         0.76223     -0.00018206
v  ǁVelocityǁ                  0.01512            31.2          10.954          20.222
v  Pressure                     -362.5          347.86         -42.091          48.122
v  k                             1e-24         0.89873       0.0012359        0.025756
v  omega                        8.2042      2.8755e+07      4.8069e+05          931.84
v  turbulent_viscosity      2.3243e-32        0.016519      5.2235e-05       0.0027301
v  CourantNb                   0.14864          2323.5          46.265          1.3899
v  FourierNb                1.7488e-05          288.38         0.61305        0.017248
v  total_pressure           1.0096e+05      1.0167e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14858        0.010756        0.044887


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.14945          2336.7          46.878          1.4072


 TIME FOR THE TIME STEP               23:        0.28870E+02

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


 INSTANT    0.240000000E+01   TIME STEP NUMBER              24
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.570846870E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43403E+02 0.29152E+01
   Friction velocity        uet   :  0.18279E-01 0.23743E+01
   Friction velocity        uk    :  0.18279E-01 0.25232E+01
   Dimensionless distance   yplus :  0.58003E-01 0.16255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4041
   Nb of faces within the viscous sub-layer     :       1120
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29312E+04     483   0.24134E-02   0.61021E+00 
c  VelocityY    0.29312E+04     483   0.24134E-02   0.00000E+00 
c  VelocityZ    0.29312E+04     483   0.24134E-02   0.00000E+00 
c  Pressure     0.31729E+00    7062   0.55158E-01   0.14811E+00 
c  k            0.54687E+01     111   0.68140E-05   0.75059E-04 
c  omega        0.13042E+10      44   0.25573E-06   0.86386E+11 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.5244e-05                          3744
a  omega          
a  Local Time Step      1.8633e-05                         45660


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.36542         0.36602      2.1887e-06      8.9743e-10
v  Velocity[Y]                 -17.974           29.32          6.2392           20.05
v  Velocity[Z]                   -27.3          28.636         0.74305     -0.00017134
v  ǁVelocityǁ                 0.013862          31.859          10.922          20.224
v  Pressure                    -369.55          353.14         -40.955          48.195
v  k                             1e-24          1.8348       0.0017103        0.026124
v  omega                        8.0392      1.6631e+07      2.4258e+05          484.63
v  turbulent_viscosity       4.823e-32         0.01762      5.4683e-05       0.0027931
v  CourantNb                  0.025171          2278.4          46.148            1.39
v  FourierNb                1.7492e-05          288.55         0.61562        0.017444
v  total_pressure           1.0096e+05      1.0168e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14836        0.010756        0.044838


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.09834          2291.7          46.763          1.4074


 TIME FOR THE TIME STEP               24:        0.28874E+02

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


 INSTANT    0.250000000E+01   TIME STEP NUMBER              25
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.117039448E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42996E+02 0.29677E+01
   Friction velocity        uet   :  0.12138E-01 0.23495E+01
   Friction velocity        uk    :  0.19521E-01 0.24726E+01
   Dimensionless distance   yplus :  0.63240E-01 0.16125E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3972
   Nb of faces within the viscous sub-layer     :       1102
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29337E+04     470   0.23758E-02   0.59377E+00 
c  VelocityY    0.29337E+04     470   0.23758E-02   0.00000E+00 
c  VelocityZ    0.29337E+04     470   0.23758E-02   0.00000E+00 
c  Pressure     0.33314E+00    7090   0.55008E-01   0.15567E+00 
c  k            0.57406E+01     130   0.10900E-04   0.72468E-04 
c  omega        0.32852E+09      69   0.10447E-05   0.21595E+11 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013106                          2828
a  omega          
a  Local Time Step      1.8608e-05                         45708


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.29052         0.29143     -1.6949e-07      8.8905e-10
v  Velocity[Y]                 -18.167          31.901          6.1604          20.051
v  Velocity[Z]                 -26.821          28.845         0.68967     -0.00040739
v  ǁVelocityǁ                0.0029446          32.292          10.877          20.227
v  Pressure                    -375.67          357.63         -40.232          48.011
v  k                             1e-24          1.0352       0.0023471         0.02646
v  omega                        7.9197      1.2277e+07      1.2412e+05          260.17
v  turbulent_viscosity      9.8327e-32        0.018672      5.7075e-05       0.0028493
v  CourantNb                  0.058665          2249.2          45.696          1.3899
v  FourierNb                1.7497e-05          289.21         0.61545        0.017612
v  total_pressure           1.0095e+05      1.0168e+05      1.0128e+05      1.0137e+05
v  Local Time Step                0.01         0.14828        0.010756        0.044802


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.10336          2262.5          46.312          1.4075


 TIME FOR THE TIME STEP               25:        0.28771E+02

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


 INSTANT    0.260000000E+01   TIME STEP NUMBER              26
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.129096258E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42196E+02 0.30114E+01
   Friction velocity        uet   :  0.75716E-02 0.23360E+01
   Friction velocity        uk    :  0.15600E-01 0.26285E+01
   Dimensionless distance   yplus :  0.75606E-01 0.15731E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       4055
   Nb of faces within the viscous sub-layer     :       1084
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29361E+04     466   0.22975E-02   0.56978E+00 
c  VelocityY    0.29361E+04     466   0.22975E-02   0.00000E+00 
c  VelocityZ    0.29361E+04     466   0.22975E-02   0.00000E+00 
c  Pressure     0.30631E+00    7091   0.52249E-01   0.14273E+00 
c  k            0.60329E+01     148   0.69549E-05   0.70426E-04 
c  omega        0.85519E+08      98   0.39857E-05   0.54047E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5611e-10                          1881
a  omega          
a  Local Time Step      1.7699e-05                         45706


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25944         0.26066     -1.7145e-06      7.6602e-10
v  Velocity[Y]                 -19.684           31.93          6.0832          20.051
v  Velocity[Z]                 -26.491          28.982         0.62159     -0.00066716
v  ǁVelocityǁ                 0.010364          32.877          10.829          20.229
v  Pressure                    -381.36          361.66         -39.179          47.624
v  k                             1e-24          1.4025       0.0032462        0.026771
v  omega                        7.7955      1.1691e+07           65449          147.18
v  turbulent_viscosity      1.5874e-31        0.020157      5.9451e-05       0.0028999
v  CourantNb                  0.078232          2233.2           45.33          1.3899
v  FourierNb                1.7503e-05          291.77          0.6177        0.017762
v  total_pressure           1.0094e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14832        0.010756        0.044787


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16167          2246.5          45.948          1.4077


 TIME FOR THE TIME STEP               26:        0.29050E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.603723726E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40200E+02 0.31007E+01
   Friction velocity        uet   :  0.94531E-02 0.24041E+01
   Friction velocity        uk    :  0.25784E-01 0.27427E+01
   Dimensionless distance   yplus :  0.11210E+00 0.15660E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3947
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04     466   0.24464E-02   0.54242E+00 
c  VelocityY    0.29383E+04     466   0.24464E-02   0.00000E+00 
c  VelocityZ    0.29383E+04     466   0.24464E-02   0.00000E+00 
c  Pressure     0.31288E+00    6819   0.50766E-01   0.14502E+00 
c  k            0.63585E+01     163   0.11122E-04   0.68845E-04 
c  omega        0.26857E+08     125   0.28238E-04   0.13695E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012557                          1141
a  omega          
a  Local Time Step      1.7239e-05                         45715


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22245         0.22298       7.995e-07      5.5534e-10
v  Velocity[Y]                 -20.285          31.154          6.0064          20.051
v  Velocity[Z]                  -28.64          33.057         0.53013     -0.00080808
v  ǁVelocityǁ                 0.014094          33.167          10.781          20.231
v  Pressure                    -390.88           365.8          -37.57          47.138
v  k                             1e-24          2.0525       0.0044311        0.027062
v  omega                        7.6862       2.576e+07           36413          89.973
v  turbulent_viscosity      1.7859e-31        0.021458      6.1862e-05       0.0029461
v  CourantNb                  0.064008          2227.5          45.094          1.3901
v  FourierNb                1.7509e-05          301.16         0.62032        0.017896
v  total_pressure           1.0093e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14865        0.010756        0.044788


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16039          2240.8          45.714           1.408


 TIME FOR THE TIME STEP               27:        0.29585E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.609058379E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39732E+02 0.32111E+01
   Friction velocity        uet   :  0.37374E-02 0.25271E+01
   Friction velocity        uk    :  0.23545E-01 0.26917E+01
   Dimensionless distance   yplus :  0.88451E-01 0.15115E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3898
   Nb of faces within the viscous sub-layer     :       1064
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04     469   0.24814E-02   0.52207E+00 
c  VelocityY    0.29403E+04     469   0.24814E-02   0.00000E+00 
c  VelocityZ    0.29403E+04     469   0.24814E-02   0.00000E+00 
c  Pressure     0.32461E+00    7015   0.54036E-01   0.15011E+00 
c  k            0.67363E+01     184   0.13744E-04   0.68126E-04 
c  omega        0.15224E+08     143   0.34263E-04   0.35851E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00021464                           715
a  omega          
a  Local Time Step      1.5947e-05                         45667


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21832         0.21909      1.3851e-08      3.9272e-10
v  Velocity[Y]                 -19.419           31.35          5.9326          20.051
v  Velocity[Z]                 -32.204          28.801          0.4264      -0.0010435
v  ǁVelocityǁ                0.0094197          33.757          10.721          20.232
v  Pressure                    -418.81          369.76         -35.502          46.533
v  k                             1e-24          3.0345        0.005961        0.027338
v  omega                        7.5917      1.2775e+07           22020          60.725
v  turbulent_viscosity      1.8004e-31        0.022548      6.4366e-05        0.002989
v  CourantNb                   0.12937          2237.8          45.177          1.3906
v  FourierNb                1.7516e-05          334.08         0.62571        0.018006
v  total_pressure           1.0091e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14858        0.010756        0.044781


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.14195          2251.1          45.803          1.4086


 TIME FOR THE TIME STEP               28:        0.31553E+02

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


 INSTANT    0.290000000E+01   TIME STEP NUMBER              29
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.954962233E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60198E+02 0.41137E+01
   Friction velocity        uet   :  0.83854E-02 0.28160E+01
   Friction velocity        uk    :  0.16695E-01 0.28010E+01
   Dimensionless distance   yplus :  0.17564E+00 0.17276E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3525
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04     475   0.25949E-02   0.50117E+00 
c  VelocityY    0.29421E+04     475   0.25949E-02   0.00000E+00 
c  VelocityZ    0.29421E+04     475   0.25949E-02   0.00000E+00 
c  Pressure     0.32475E+00    6926   0.54115E-01   0.15032E+00 
c  k            0.71884E+01     194   0.98876E-05   0.70059E-04 
c  omega        0.12886E+08     150   0.26923E-04   0.10701E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4064e-05                           361
a  omega          
a  Local Time Step      1.7035e-05                         45665


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21466         0.21516     -4.6689e-06        2.29e-10
v  Velocity[Y]                 -19.273          30.482          5.8597           20.05
v  Velocity[Z]                 -32.697          28.613         0.33985       -0.001253
v  ǁVelocityǁ                 0.014233           34.17          10.679          20.234
v  Pressure                    -448.18          371.09         -34.363          45.836
v  k                             1e-24           4.197       0.0076733          0.0276
v  omega                        7.4921      1.1727e+07           15059          45.528
v  turbulent_viscosity      2.5777e-31          0.0234      6.7029e-05       0.0030295
v  CourantNb                  0.047844          2248.7          45.059          1.3911
v  FourierNb                1.7524e-05          362.35         0.63368        0.018089
v  total_pressure           1.0088e+05       1.017e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14836        0.010755        0.044753


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.21874            2262          45.693          1.4092


 TIME FOR THE TIME STEP               29:        0.30348E+02

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


 INSTANT    0.300000000E+01   TIME STEP NUMBER              30
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.160101172E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46581E+02 0.60305E+01
   Friction velocity        uet   :  0.31332E-02 0.28858E+01
   Friction velocity        uk    :  0.14833E-01 0.28217E+01
   Dimensionless distance   yplus :  0.48859E-01 0.14565E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       3166
   Nb of faces within the viscous sub-layer     :       1165
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29438E+04     482   0.26295E-02   0.50373E+00 
c  VelocityY    0.29438E+04     482   0.26295E-02   0.00000E+00 
c  VelocityZ    0.29438E+04     482   0.26295E-02   0.00000E+00 
c  Pressure     0.32333E+00    7097   0.51267E-01   0.14948E+00 
c  k            0.77241E+01     219   0.16913E-04   0.79337E-04 
c  omega        0.12796E+08     151   0.17435E-03   0.15507E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00029324                           196
a  omega          
a  Local Time Step      1.6645e-05                         45661


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21288          0.2133     -7.1157e-06      1.5397e-10
v  Velocity[Y]                 -19.586          29.949          5.8304           20.05
v  Velocity[Z]                 -35.211           28.08         0.28049      -0.0013879
v  ǁVelocityǁ                0.0080905          37.498          10.669          20.236
v  Pressure                    -478.34          368.78         -34.246          44.998
v  k                             1e-24           5.266       0.0097549        0.027853
v  omega                          7.41      4.9804e+07           12407          37.426
v  turbulent_viscosity      2.5645e-31        0.023846      6.9929e-05       0.0030681
v  CourantNb                   0.10344          2248.4          44.716          1.3915
v  FourierNb                1.7533e-05          385.51         0.64442        0.018165
v  total_pressure           1.0085e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14822        0.010756         0.04473


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.10499          2261.7           45.36          1.4096


 TIME FOR THE TIME STEP               30:        0.30217E+02

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


 INSTANT    0.310000000E+01   TIME STEP NUMBER              31
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.254284998E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50328E+02 0.70665E+01
   Friction velocity        uet   :  0.18968E-02 0.31348E+01
   Friction velocity        uk    :  0.24996E-01 0.27543E+01
   Dimensionless distance   yplus :  0.13087E+00 0.14856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2925
   Nb of faces within the viscous sub-layer     :       1076
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29453E+04     496   0.28215E-02   0.53031E+00 
c  VelocityY    0.29453E+04     496   0.28215E-02   0.00000E+00 
c  VelocityZ    0.29453E+04     496   0.28215E-02   0.00000E+00 
c  Pressure     0.34917E+00    7103   0.46535E-01   0.16046E+00 
c  k            0.82836E+01     262   0.16951E-04   0.94328E-04 
c  omega        0.21186E+08     131   0.56611E-04   0.10169E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.9721e-05                           123
a  omega          
a  Local Time Step      1.6421e-05                         45694


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21031         0.21177     -8.0351e-06     -9.1458e-11
v  Velocity[Y]                 -19.226          29.664          5.8431           20.05
v  Velocity[Z]                 -34.767          28.698         0.25452      -0.0014515
v  ǁVelocityǁ                 0.014298          36.717            10.7          20.238
v  Pressure                    -502.65          364.89         -33.885          44.231
v  k                             1e-24           6.165        0.012427        0.028101
v  omega                         7.329      2.6142e+07           10560          32.855
v  turbulent_viscosity       2.978e-31        0.024185      7.3215e-05       0.0031053
v  CourantNb                  0.044791          2230.7           44.55          1.3917
v  FourierNb                1.7545e-05          387.84         0.65857        0.018251
v  total_pressure           1.0082e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14817        0.010757         0.04473


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2615          2244.1          45.208          1.4099


 TIME FOR THE TIME STEP               31:        0.29873E+02

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


 INSTANT    0.320000000E+01   TIME STEP NUMBER              32
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.209438161E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.48718E+02 0.77883E+01
   Friction velocity        uet   :  0.28938E-02 0.30592E+01
   Friction velocity        uk    :  0.40411E-01 0.28909E+01
   Dimensionless distance   yplus :  0.68814E-01 0.14678E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2795
   Nb of faces within the viscous sub-layer     :       1085
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29466E+04     511   0.28433E-02   0.55228E+00 
c  VelocityY    0.29466E+04     511   0.28433E-02   0.00000E+00 
c  VelocityZ    0.29466E+04     511   0.28433E-02   0.00000E+00 
c  Pressure     0.32093E+00    7066   0.45558E-01   0.14716E+00 
c  k            0.87337E+01     291   0.25650E-04   0.13002E-03 
c  omega        0.14578E+08     139   0.79596E-04   0.90162E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.4563e-06                             7
a  omega          
a  Local Time Step      1.6092e-05                         45696


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20648         0.20982       3.273e-06     -2.0518e-10
v  Velocity[Y]                 -18.914          29.989          5.9019          20.051
v  Velocity[Z]                 -35.576          29.743         0.25873      -0.0016339
v  ǁVelocityǁ                  0.01009           36.37          10.766          20.241
v  Pressure                    -520.58             360         -33.184           43.57
v  k                        4.8864e-20          6.1453        0.015989        0.028344
v  omega                        7.2529      3.1626e+07          9715.8           30.13
v  turbulent_viscosity      5.2243e-31        0.024445      7.7135e-05       0.0031415
v  CourantNb                  0.079578          2217.7          44.595          1.3917
v  FourierNb                1.7559e-05          401.34         0.67903        0.018347
v  total_pressure            1.008e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14822        0.010757        0.044746


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23494          2231.4          45.274            1.41


 TIME FOR THE TIME STEP               32:        0.30491E+02

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


 INSTANT    0.330000000E+01   TIME STEP NUMBER              33
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.309117502E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46697E+02 0.84276E+01
   Friction velocity        uet   :  0.36720E-02 0.30603E+01
   Friction velocity        uk    :  0.21106E-01 0.29556E+01
   Dimensionless distance   yplus :  0.76354E-01 0.15017E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2720
   Nb of faces within the viscous sub-layer     :       1036
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29477E+04     511   0.29540E-02   0.56147E+00 
c  VelocityY    0.29477E+04     511   0.29540E-02   0.00000E+00 
c  VelocityZ    0.29477E+04     511   0.29540E-02   0.00000E+00 
c  Pressure     0.33051E+00    7063   0.47662E-01   0.15175E+00 
c  k            0.91811E+01     323   0.36594E-04   0.21144E-03 
c  omega        0.14738E+08     134   0.14619E-03   0.14455E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027974                            10
a  omega          
a  Local Time Step      1.5798e-05                         45697


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20314          0.2089       1.621e-05      6.8649e-11
v  Velocity[Y]                 -19.046          29.863          5.9957          20.051
v  Velocity[Z]                  -35.36          31.308         0.29147      -0.0019008
v  ǁVelocityǁ                 0.027719          35.869          10.841          20.244
v  Pressure                    -526.47          358.47         -32.998          42.967
v  k                        6.5234e-17          6.8287        0.021307        0.028584
v  omega                        7.1899      6.6289e+07          9115.4          28.323
v  turbulent_viscosity      4.9373e-26        0.024716      8.1959e-05       0.0031769
v  CourantNb                  0.096491          2213.8          45.013          1.3917
v  FourierNb                1.7577e-05          393.89         0.70974        0.018457
v  total_pressure            1.008e+05      1.0168e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14856        0.010758        0.044778


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25221          2228.6          45.723          1.4102


 TIME FOR THE TIME STEP               33:        0.29832E+02

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


 INSTANT    0.340000000E+01   TIME STEP NUMBER              34
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.176097144E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44118E+02 0.90838E+01
   Friction velocity        uet   :  0.26952E-02 0.29957E+01
   Friction velocity        uk    :  0.14334E-01 0.29072E+01
   Dimensionless distance   yplus :  0.50225E-01 0.15435E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2583
   Nb of faces within the viscous sub-layer     :       1076
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29487E+04     502   0.29559E-02   0.51297E+00 
c  VelocityY    0.29487E+04     502   0.29559E-02   0.00000E+00 
c  VelocityZ    0.29487E+04     502   0.29559E-02   0.00000E+00 
c  Pressure     0.34630E+00    7005   0.46735E-01   0.15791E+00 
c  k            0.94212E+01     355   0.91831E-04   0.35013E-03 
c  omega        0.28860E+08     105   0.34503E-04   0.46577E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00092341                            15
a  omega          
a  Local Time Step      1.5511e-05                         45700


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.19795         0.20334      5.1663e-06      3.3435e-10
v  Velocity[Y]                 -19.332          30.152          6.0627          20.051
v  Velocity[Z]                   -34.3          31.606         0.30765      -0.0019954
v  ǁVelocityǁ                 0.010481          34.941           10.85          20.245
v  Pressure                    -515.07          362.45         -33.787          42.022
v  k                        8.2638e-16          9.4915        0.028774        0.028824
v  omega                        7.1205      3.4028e+07          8615.8          27.055
v  turbulent_viscosity      6.5819e-23        0.024973      8.8148e-05       0.0032119
v  CourantNb                  0.061307          2225.5          45.679           1.392
v  FourierNb                1.7599e-05          395.14         0.76124        0.018586
v  total_pressure           1.0081e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14847        0.010759        0.044819


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25286          2242.6          46.441          1.4106


 TIME FOR THE TIME STEP               34:        0.29300E+02

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


 INSTANT    0.350000000E+01   TIME STEP NUMBER              35
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.162009179E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42197E+02 0.96368E+01
   Friction velocity        uet   :  0.52934E-03 0.28973E+01
   Friction velocity        uk    :  0.23525E-01 0.30660E+01
   Dimensionless distance   yplus :  0.47673E-01 0.15892E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2405
   Nb of faces within the viscous sub-layer     :       1094
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29496E+04     495   0.29005E-02   0.45836E+00 
c  VelocityY    0.29496E+04     495   0.29005E-02   0.00000E+00 
c  VelocityZ    0.29496E+04     495   0.29005E-02   0.00000E+00 
c  Pressure     0.33682E+00    6979   0.45722E-01   0.15364E+00 
c  k            0.98963E+01     373   0.19361E-03   0.64481E-03 
c  omega        0.14609E+08     118   0.13818E-03   0.13205E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024167                            10
a  omega          
a  Local Time Step      1.5323e-05                         45702


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.19281         0.19997     -2.2103e-05      9.6948e-10
v  Velocity[Y]                 -20.452          30.976          6.1152           20.05
v  Velocity[Z]                 -29.751          32.267         0.30546      -0.0021279
v  ǁVelocityǁ                0.0074309          32.317          10.872          20.247
v  Pressure                    -487.19          365.88         -34.941          40.929
v  k                        5.0376e-14          11.878         0.03754        0.029065
v  omega                        7.0634      4.7887e+07          8917.4          26.118
v  turbulent_viscosity      8.7167e-22        0.025251      9.6289e-05       0.0032464
v  CourantNb                  0.030211          2231.5          45.831          1.3921
v  FourierNb                1.7628e-05          382.36         0.84227         0.01871
v  total_pressure           1.0084e+05      1.0169e+05      1.0129e+05      1.0137e+05
v  Local Time Step                0.01         0.14828         0.01076        0.044827


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2276          2252.9          46.673          1.4108


 TIME FOR THE TIME STEP               35:        0.30340E+02

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


 INSTANT    0.360000000E+01   TIME STEP NUMBER              36
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.115296925E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32610E+02 0.10186E+02
   Friction velocity        uet   :  0.16939E-02 0.28411E+01
   Friction velocity        uk    :  0.16174E-01 0.28965E+01
   Dimensionless distance   yplus :  0.11859E+00 0.16263E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2385
   Nb of faces within the viscous sub-layer     :       1112
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29503E+04     487   0.31987E-02   0.42917E+00 
c  VelocityY    0.29503E+04     487   0.31987E-02   0.00000E+00 
c  VelocityZ    0.29503E+04     487   0.31987E-02   0.00000E+00 
c  Pressure     0.33838E+00    7015   0.46478E-01   0.15401E+00 
c  k            0.10386E+02     384   0.32441E-03   0.10275E-02 
c  omega        0.21235E+08     105   0.44293E-04   0.49510E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00032376                             7
a  omega          
a  Local Time Step      1.4997e-05                         45717


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.18903         0.19266     -2.9177e-05      2.8864e-10
v  Velocity[Y]                 -21.658           31.68          6.1351           20.05
v  Velocity[Z]                  -35.35           32.66         0.28415      -0.0022674
v  ǁVelocityǁ                0.0036588          35.439          10.977          20.249
v  Pressure                    -458.09          367.62         -36.467          39.829
v  k                        1.6863e-12          20.136        0.049417        0.029313
v  omega                        7.0085      2.4966e+07          8626.2          25.309
v  turbulent_viscosity      5.5814e-20        0.025533      0.00010719       0.0032809
v  CourantNb                  0.045055          2229.6          45.841           1.392
v  FourierNb                1.7663e-05          389.59         0.96225        0.018852
v  total_pressure           1.0087e+05      1.0169e+05      1.0129e+05      1.0136e+05
v  Local Time Step                0.01         0.14819         0.01076         0.04482


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16865          2258.9          46.803          1.4109


 TIME FOR THE TIME STEP               36:        0.30707E+02

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


 INSTANT    0.370000000E+01   TIME STEP NUMBER              37
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271557770E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43982E+02 0.10582E+02
   Friction velocity        uet   :  0.28295E-02 0.29925E+01
   Friction velocity        uk    :  0.93305E-02 0.28388E+01
   Dimensionless distance   yplus :  0.78121E-01 0.16559E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2337
   Nb of faces within the viscous sub-layer     :       1081
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29509E+04     475   0.33467E-02   0.42763E+00 
c  VelocityY    0.29509E+04     475   0.33467E-02   0.00000E+00 
c  VelocityZ    0.29509E+04     475   0.33467E-02   0.00000E+00 
c  Pressure     0.35938E+00    6854   0.48143E-01   0.16334E+00 
c  k            0.11085E+02     392   0.49626E-03   0.13536E-02 
c  omega        0.13800E+08     112   0.33562E-04   0.19605E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033109                             8
a  omega          
a  Local Time Step      1.5047e-05                         45768


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.18526         0.18761     -1.9842e-05     -1.7614e-09
v  Velocity[Y]                 -31.755          30.732          6.1848           20.05
v  Velocity[Z]                 -26.633          32.733         0.24747      -0.0024134
v  ǁVelocityǁ                 0.021754          32.817          11.082          20.252
v  Pressure                    -469.92          368.82         -38.202          38.892
v  k                        2.0827e-12          22.242        0.065516        0.029568
v  omega                        6.9558      1.4465e+07          8284.2          24.611
v  turbulent_viscosity      3.7011e-18        0.025777      0.00012196       0.0033152
v  CourantNb                  0.034038          2200.8           46.31          1.3921
v  FourierNb                1.7707e-05          403.49          1.1468        0.019044
v  total_pressure           1.0086e+05      1.0169e+05      1.0129e+05      1.0136e+05
v  Local Time Step                0.01          0.1482        0.010761        0.044825


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.26419          2243.2          47.457          1.4112


 TIME FOR THE TIME STEP               37:        0.28892E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.959535301E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39668E+02 0.10954E+02
   Friction velocity        uet   :  0.37179E-02 0.28086E+01
   Friction velocity        uk    :  0.17768E-01 0.25767E+01
   Dimensionless distance   yplus :  0.71371E-01 0.17217E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2300
   Nb of faces within the viscous sub-layer     :       1122
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29512E+04     461   0.31499E-02   0.46616E+00 
c  VelocityY    0.29512E+04     461   0.31499E-02   0.00000E+00 
c  VelocityZ    0.29512E+04     461   0.31499E-02   0.00000E+00 
c  Pressure     0.34729E+00    6855   0.49490E-01   0.15842E+00 
c  k            0.11586E+02     401   0.54234E-03   0.18867E-02 
c  omega        0.12843E+08     114   0.47326E-04   0.33920E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027101                             5
a  omega          
a  Local Time Step      1.4669e-05                         45792


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.18259         0.18395     -1.0557e-05     -9.6984e-10
v  Velocity[Y]                 -22.999          30.891          6.2688          20.051
v  Velocity[Z]                 -26.492          32.832         0.19699      -0.0025019
v  ǁVelocityǁ                  0.01261           33.03           11.13          20.255
v  Pressure                    -479.97          370.43         -40.005          37.981
v  k                        7.1397e-12          24.639        0.087289        0.029833
v  omega                        6.9123       2.101e+07          8402.5          24.058
v  turbulent_viscosity      9.9993e-19        0.025996      0.00014175       0.0033494
v  CourantNb                    0.1306          2363.1          46.693          1.3923
v  FourierNb                1.7761e-05          389.33          1.4183        0.019318
v  total_pressure           1.0085e+05       1.017e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14845        0.010763        0.044865


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.21294          2379.6          48.112          1.4116


 TIME FOR THE TIME STEP               38:        0.28555E+02

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


 INSTANT    0.390000000E+01   TIME STEP NUMBER              39
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.517175736E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29904E+02 0.11211E+02
   Friction velocity        uet   :  0.30276E-02 0.23475E+01
   Friction velocity        uk    :  0.15540E-01 0.25434E+01
   Dimensionless distance   yplus :  0.45125E-01 0.18824E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2259
   Nb of faces within the viscous sub-layer     :       1131
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29512E+04     450   0.33822E-02   0.52906E+00 
c  VelocityY    0.29512E+04     450   0.33822E-02   0.00000E+00 
c  VelocityZ    0.29512E+04     450   0.33822E-02   0.00000E+00 
c  Pressure     0.33394E+00    7030   0.49930E-01   0.15241E+00 
c  k            0.12133E+02     407   0.46019E-03   0.27474E-02 
c  omega        0.13313E+08     114   0.24790E-03   0.36556E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9408e-05                             5
a  omega          
a  Local Time Step      1.5071e-05                         45791


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17756         0.17901     -6.5618e-06     -1.4072e-09
v  Velocity[Y]                 -19.572          32.428          6.3245          20.051
v  Velocity[Z]                 -26.698          32.828         0.15285      -0.0026532
v  ǁVelocityǁ                  0.01885          32.979          11.124          20.257
v  Pressure                    -488.29          372.53         -41.608          36.872
v  k                        1.4216e-11          30.054         0.11704        0.030117
v  omega                        6.8647      9.5455e+07          9240.7          23.571
v  turbulent_viscosity      1.1537e-17        0.026128      0.00016799       0.0033835
v  CourantNb                   0.11568          2213.6          46.692          1.3922
v  FourierNb                1.7825e-05           419.5          1.8006        0.019685
v  total_pressure           1.0084e+05       1.017e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14849        0.010765        0.044931


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.18021          2230.9          48.493          1.4119


 TIME FOR THE TIME STEP               39:        0.29004E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.630781730E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30382E+02 0.11359E+02
   Friction velocity        uet   :  0.17701E-02 0.27979E+01
   Friction velocity        uk    :  0.29478E-01 0.26750E+01
   Dimensionless distance   yplus :  0.72335E-01 0.20651E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2302
   Nb of faces within the viscous sub-layer     :       1055
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29512E+04     437   0.34016E-02   0.61252E+00 
c  VelocityY    0.29512E+04     437   0.34016E-02   0.00000E+00 
c  VelocityZ    0.29512E+04     437   0.34016E-02   0.00000E+00 
c  Pressure     0.35899E+00    6969   0.49713E-01   0.16326E+00 
c  k            0.12751E+02     414   0.36249E-03   0.42486E-02 
c  omega        0.56410E+08      85   0.44708E-04   0.23252E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -9.3099e-05                             4
a  omega          
a  Local Time Step      1.5255e-05                         45812


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17427         0.17678      1.1556e-05     -1.5278e-09
v  Velocity[Y]                  -20.64          35.239          6.2988          20.051
v  Velocity[Z]                 -27.139          32.949         0.11161      -0.0029616
v  ǁVelocityǁ                0.0084028          35.296          11.071           20.26
v  Pressure                    -497.71          374.12         -43.296          35.562
v  k                        2.7711e-11          29.636         0.15627        0.030426
v  omega                        6.8259      5.6288e+07          9143.8          23.055
v  turbulent_viscosity      1.0607e-16        0.026158      0.00020299       0.0034177
v  CourantNb                  0.067797          2097.1          46.349           1.392
v  FourierNb                1.7901e-05          505.91           2.319         0.02012
v  total_pressure           1.0083e+05       1.017e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010766        0.044948


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20944          2195.4          48.668          1.4121


 TIME FOR THE TIME STEP               40:        0.29134E+02

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


 INSTANT    0.410000000E+01   TIME STEP NUMBER              41
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.103732585E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30981E+02 0.11505E+02
   Friction velocity        uet   :  0.96614E-03 0.29424E+01
   Friction velocity        uk    :  0.17209E-01 0.32698E+01
   Dimensionless distance   yplus :  0.45041E-01 0.20962E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2076
   Nb of faces within the viscous sub-layer     :        929
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29509E+04     428   0.36111E-02   0.69715E+00 
c  VelocityY    0.29509E+04     428   0.36111E-02   0.00000E+00 
c  VelocityZ    0.29509E+04     428   0.36111E-02   0.00000E+00 
c  Pressure     0.37466E+00    7059   0.58250E-01   0.17026E+00 
c  k            0.13788E+02     424   0.49557E-03   0.70206E-02 
c  omega        0.27602E+08      98   0.13607E-03   0.52108E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024099                             6
a  omega          
a  Local Time Step      1.5483e-05                         45806


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17072         0.17302     -7.1155e-07      1.2985e-09
v  Velocity[Y]                 -20.342           36.36          6.2103          20.051
v  Velocity[Z]                 -27.531          33.144        0.082985      -0.0034981
v  ǁVelocityǁ                 0.011082          36.784          10.997          20.262
v  Pressure                    -504.01          376.05         -44.754          34.165
v  k                        3.7007e-11          31.678         0.20558        0.030764
v  omega                        6.7875      1.0818e+08          9548.4          22.614
v  turbulent_viscosity      1.1632e-16        0.026239      0.00024881       0.0034522
v  CourantNb                  0.038108          2122.3           45.66          1.3916
v  FourierNb                1.7989e-05          632.89          2.9972        0.020686
v  total_pressure           1.0082e+05       1.017e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14838        0.010767        0.044984


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15462            2193          48.657          1.4123


 TIME FOR THE TIME STEP               41:        0.28958E+02

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


 INSTANT    0.420000000E+01   TIME STEP NUMBER              42
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.401710140E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31035E+02 0.17471E+02
   Friction velocity        uet   :  0.93505E-03 0.31349E+01
   Friction velocity        uk    :  0.20272E-01 0.30919E+01
   Dimensionless distance   yplus :  0.62790E-01 0.25388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       2084
   Nb of faces within the viscous sub-layer     :        914
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29503E+04     424   0.36848E-02   0.78027E+00 
c  VelocityY    0.29503E+04     424   0.36848E-02   0.00000E+00 
c  VelocityZ    0.29503E+04     424   0.36848E-02   0.00000E+00 
c  Pressure     0.36866E+00    7057   0.67396E-01   0.16788E+00 
c  k            0.15323E+02     434   0.59516E-03   0.95851E-02 
c  omega        0.79173E+08      81   0.19433E-04   0.16751E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00025424                             4
a  omega          
a  Local Time Step      1.5622e-05                         45798


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.16726         0.16863     -3.8159e-05     -1.0343e-09
v  Velocity[Y]                 -20.738          33.523          6.1036          20.051
v  Velocity[Z]                 -27.781          32.938        0.036439      -0.0039345
v  ǁVelocityǁ                 0.011442          33.988          10.888          20.264
v  Pressure                     -508.8          378.91         -46.109          33.001
v  k                        9.9747e-11          23.226         0.26278        0.031126
v  omega                        6.7534      5.4335e+07          8887.9          22.135
v  turbulent_viscosity      9.6309e-18        0.026371      0.00030763       0.0034868
v  CourantNb                  0.049108          2100.8          45.146          1.3915
v  FourierNb                1.8089e-05          740.51          3.8884        0.021411
v  total_pressure           1.0082e+05       1.017e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010768        0.045037


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23509          2194.1          49.034          1.4129


 TIME FOR THE TIME STEP               42:        0.29013E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.369390771E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32291E+02 0.17272E+02
   Friction velocity        uet   :  0.99811E-03 0.27274E+01
   Friction velocity        uk    :  0.22676E-01 0.30613E+01
   Dimensionless distance   yplus :  0.10948E+00 0.25256E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1844
   Nb of faces within the viscous sub-layer     :        934
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29495E+04     420   0.36818E-02   0.85432E+00 
c  VelocityY    0.29495E+04     420   0.36818E-02   0.00000E+00 
c  VelocityZ    0.29495E+04     420   0.36818E-02   0.00000E+00 
c  Pressure     0.36901E+00    7030   0.65574E-01   0.16814E+00 
c  k            0.17495E+02     442   0.51519E-03   0.12249E-01 
c  omega        0.24250E+08     103   0.33722E-04   0.58200E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002892                             2
a  omega          
a  Local Time Step      1.5516e-05                         45766


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.16173         0.16337     -0.00015411      3.8094e-09
v  Velocity[Y]                 -21.048          31.275           6.053          20.052
v  Velocity[Z]                 -28.619          32.725        -0.02425      -0.0043876
v  ǁVelocityǁ                 0.014198          34.337          10.796          20.266
v  Pressure                    -515.48           381.4          -47.17          32.257
v  k                         1.836e-10          29.267         0.33145        0.031524
v  omega                        6.7227       2.794e+07          8481.9          21.676
v  turbulent_viscosity       2.574e-16        0.026441      0.00038136       0.0035215
v  CourantNb                  0.051913          2026.6          44.823          1.3915
v  FourierNb                1.8203e-05          945.37          5.0429        0.022308
v  total_pressure           1.0081e+05      1.0171e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14857        0.010769        0.045083


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15939          2202.8          49.866          1.4138


 TIME FOR THE TIME STEP               43:        0.31499E+02

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


 INSTANT    0.440000000E+01   TIME STEP NUMBER              44
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.612089169E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31849E+02 0.15324E+02
   Friction velocity        uet   :  0.12801E-02 0.28416E+01
   Friction velocity        uk    :  0.74358E-02 0.27416E+01
   Dimensionless distance   yplus :  0.60390E-01 0.23076E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1732
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29486E+04     419   0.36814E-02   0.91564E+00 
c  VelocityY    0.29486E+04     419   0.36814E-02   0.00000E+00 
c  VelocityZ    0.29486E+04     419   0.36814E-02   0.00000E+00 
c  Pressure     0.38924E+00    7096   0.62196E-01   0.17779E+00 
c  k            0.23166E+02     445   0.54022E-03   0.15271E-01 
c  omega        0.14317E+08     111   0.43287E-04   0.50861E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.5576e-05                         45802


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.15549         0.15831     -0.00022209      -6.395e-09
v  Velocity[Y]                 -21.324          31.377          6.0784          20.052
v  Velocity[Z]                 -28.242          32.601       -0.075285      -0.0047636
v  ǁVelocityǁ                 0.028653          34.266          10.766          20.268
v  Pressure                    -520.02          383.18         -46.804          31.592
v  k                        3.3774e-10          38.941          0.4079        0.031959
v  omega                        6.6933      1.5177e+07          8619.6          21.313
v  turbulent_viscosity      2.6736e-15        0.026457      0.00047304       0.0035567
v  CourantNb                  0.049637          2030.2          44.286          1.3913
v  FourierNb                 1.833e-05          1160.1          6.4995        0.023434
v  total_pressure            1.008e+05      1.0171e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14894         0.01077        0.045141


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.17388          2365.9          50.785          1.4148


 TIME FOR THE TIME STEP               44:        0.30671E+02

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


 INSTANT    0.450000000E+01   TIME STEP NUMBER              45
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.126378209E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31309E+02 0.12394E+02
   Friction velocity        uet   :  0.57047E-03 0.28112E+01
   Friction velocity        uk    :  0.10629E-01 0.32253E+01
   Dimensionless distance   yplus :  0.93584E-01 0.23775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1587
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29475E+04     430   0.40142E-02   0.95616E+00 
c  VelocityY    0.29475E+04     430   0.40142E-02   0.00000E+00 
c  VelocityZ    0.29475E+04     430   0.40142E-02   0.00000E+00 
c  Pressure     0.37974E+00    7047   0.63297E-01   0.17307E+00 
c  k            0.33871E+02     443   0.48837E-03   0.20197E-01 
c  omega        0.13429E+08     118   0.11377E-03   0.11424E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.5493e-05                         45807


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.15253         0.15634     -0.00020122     -1.1523e-08
v  Velocity[Y]                 -21.611          31.408          6.1491          20.051
v  Velocity[Z]                 -28.622          32.244       -0.089296      -0.0050449
v  ǁVelocityǁ                 0.031706          32.348          10.805          20.269
v  Pressure                     -522.3          383.73          -45.02          30.992
v  k                        6.1363e-10          33.764         0.49426        0.032446
v  omega                        6.6686      4.0518e+07          9057.4          20.991
v  turbulent_viscosity      1.0406e-15        0.026487      0.00058263       0.0035918
v  CourantNb                   0.12411          2186.7          44.127          1.3913
v  FourierNb                1.8473e-05          1407.8           8.272        0.024765
v  total_pressure            1.008e+05      1.0171e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14906        0.010771        0.045175


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15895          2480.8          52.399          1.4161


 TIME FOR THE TIME STEP               45:        0.30343E+02

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


 INSTANT    0.460000000E+01   TIME STEP NUMBER              46
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.312913161E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29634E+02 0.12795E+02
   Friction velocity        uet   :  0.15087E-02 0.29288E+01
   Friction velocity        uk    :  0.20921E-01 0.30144E+01
   Dimensionless distance   yplus :  0.83276E-01 0.25093E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1677
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29463E+04     443   0.40934E-02   0.99686E+00 
c  VelocityY    0.29463E+04     443   0.40934E-02   0.00000E+00 
c  VelocityZ    0.29463E+04     443   0.40934E-02   0.00000E+00 
c  Pressure     0.39046E+00    7027   0.63324E-01   0.17712E+00 
c  k            0.43465E+02     443   0.49711E-03   0.29979E-01 
c  omega        0.17459E+08     111   0.43303E-04   0.55713E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.4672e-05                         45810


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.1513         0.15234     -7.6482e-05     -2.4377e-09
v  Velocity[Y]                 -25.532          31.354          6.2378          20.052
v  Velocity[Z]                 -28.436          31.671        -0.07537      -0.0053452
v  ǁVelocityǁ                 0.016033          32.984           10.83          20.271
v  Pressure                    -525.89          382.12         -43.088          30.435
v  k                        1.1039e-09          23.954          0.6018        0.033016
v  omega                        6.6443      2.1592e+07          8945.5          20.683
v  turbulent_viscosity       8.454e-16        0.026487      0.00071039       0.0036272
v  CourantNb                  0.045587          2488.9          44.484          1.3914
v  FourierNb                1.8625e-05          1735.5           10.23        0.026268
v  total_pressure            1.008e+05      1.0171e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14831        0.010772        0.045211


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.16578          2761.1          54.714          1.4176


 TIME FOR THE TIME STEP               46:        0.31365E+02

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


 INSTANT    0.470000000E+01   TIME STEP NUMBER              47
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.822451786E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30071E+02 0.12846E+02
   Friction velocity        uet   :  0.27714E-03 0.29624E+01
   Friction velocity        uk    :  0.19283E-01 0.26805E+01
   Dimensionless distance   yplus :  0.12195E+00 0.26494E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1781
   Nb of faces within the viscous sub-layer     :       1055
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29451E+04     451   0.40573E-02   0.10275E+01 
c  VelocityY    0.29451E+04     451   0.40573E-02   0.00000E+00 
c  VelocityZ    0.29451E+04     451   0.40573E-02   0.00000E+00 
c  Pressure     0.37881E+00    7063   0.62202E-01   0.17218E+00 
c  k            0.54353E+02     520   0.81619E-03   0.51459E-01 
c  omega        0.13969E+08     115   0.15021E-03   0.16603E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00013511                             1
a  omega          
a  Local Time Step      1.4171e-05                         45819


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.15031         0.13826      0.00025379      5.1012e-09
v  Velocity[Y]                 -24.405          31.327          6.2938          20.052
v  Velocity[Z]                 -28.236           31.48       -0.045706      -0.0056806
v  ǁVelocityǁ                 0.012763          32.227          10.795          20.273
v  Pressure                    -526.49          380.48         -40.931          29.891
v  k                         1.969e-09          47.274         0.73399        0.033679
v  omega                        6.6244       6.115e+07          9371.7          20.411
v  turbulent_viscosity      2.4461e-16        0.026517      0.00086495       0.0036632
v  CourantNb                  0.050108          2573.9          44.917          1.3914
v  FourierNb                1.8792e-05          2066.5          12.695        0.028105
v  total_pressure            1.008e+05      1.0171e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01          0.1477        0.010774         0.04527


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.12049          3164.2          57.612          1.4195


 TIME FOR THE TIME STEP               47:        0.31404E+02

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


 INSTANT    0.480000000E+01   TIME STEP NUMBER              48
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.150938583E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31083E+02 0.12787E+02
   Friction velocity        uet   :  0.39110E-03 0.24641E+01
   Friction velocity        uk    :  0.22219E-01 0.25941E+01
   Dimensionless distance   yplus :  0.10698E+00 0.27638E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1789
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29435E+04     458   0.42149E-02   0.10282E+01 
c  VelocityY    0.29435E+04     458   0.42149E-02   0.00000E+00 
c  VelocityZ    0.29435E+04     458   0.42149E-02   0.00000E+00 
c  Pressure     0.39123E+00    6975   0.58938E-01   0.17877E+00 
c  k            0.64511E+02     635   0.11362E-02   0.77163E-01 
c  omega        0.26451E+08     111   0.38056E-04   0.75113E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00049697                             2
a  omega          
a  Local Time Step      1.3854e-05                         45794


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.14558         0.12422      0.00050271      2.5113e-09
v  Velocity[Y]                 -30.106          31.303          6.3052          20.053
v  Velocity[Z]                 -28.025          31.261       -0.014251      -0.0060169
v  ǁVelocityǁ                 0.019695          32.174           10.79          20.275
v  Pressure                    -527.21          379.39         -38.885          29.488
v  k                        5.4534e-10          53.421         0.88693        0.034439
v  omega                        6.6056      3.1534e+07          9066.1          20.083
v  turbulent_viscosity      1.2743e-15        0.026508       0.0010482       0.0036996
v  CourantNb                  0.065509          2118.5          45.001          1.3912
v  FourierNb                1.8975e-05          2347.3          15.812         0.03034
v  total_pressure            1.008e+05       1.017e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14774        0.010776         0.04535


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.22861          3595.3          60.814          1.4216


 TIME FOR THE TIME STEP               48:        0.30056E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.115923854E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28887E+02 0.12815E+02
   Friction velocity        uet   :  0.11511E-02 0.29913E+01
   Friction velocity        uk    :  0.46186E-02 0.25876E+01
   Dimensionless distance   yplus :  0.17997E-01 0.28652E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1780
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04     499   0.39745E-02   0.10435E+01 
c  VelocityY    0.29419E+04     499   0.39745E-02   0.00000E+00 
c  VelocityZ    0.29419E+04     499   0.39745E-02   0.00000E+00 
c  Pressure     0.36602E+00    7055   0.58782E-01   0.16679E+00 
c  k            0.75134E+02     784   0.16112E-02   0.13055E+00 
c  omega        0.14650E+08     129   0.42126E-04   0.40767E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045224                             2
a  omega          
a  Local Time Step      1.3741e-05                         45784


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.13344         0.13898      0.00068181      5.6151e-09
v  Velocity[Y]                 -22.444           31.27          6.2761          20.052
v  Velocity[Z]                 -28.071          31.077         0.00503      -0.0063879
v  ǁVelocityǁ                 0.018024          31.828           10.84          20.276
v  Pressure                    -528.52          377.04         -37.815          29.087
v  k                        6.1286e-09          74.682          1.0801        0.035315
v  omega                        6.5895      1.7454e+07          8846.6          19.785
v  turbulent_viscosity      7.8657e-17        0.026404       0.0012536       0.0037361
v  CourantNb                  0.018998          2077.7          45.009          1.3912
v  FourierNb                1.9174e-05          2637.3          19.314        0.032879
v  total_pressure            1.008e+05       1.017e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14923        0.010778        0.045433


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24979          3991.9          64.323          1.4241


 TIME FOR THE TIME STEP               49:        0.29764E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.104297351E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28625E+02 0.12622E+02
   Friction velocity        uet   :  0.15712E-02 0.22653E+01
   Friction velocity        uk    :  0.21538E-01 0.26407E+01
   Dimensionless distance   yplus :  0.75934E-01 0.28557E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1616
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04     619   0.41783E-02   0.10686E+01 
c  VelocityY    0.29402E+04     619   0.41783E-02   0.00000E+00 
c  VelocityZ    0.29402E+04     619   0.41783E-02   0.00000E+00 
c  Pressure     0.36070E+00    7089   0.61982E-01   0.16437E+00 
c  k            0.88170E+02     937   0.26822E-02   0.16142E+00 
c  omega        0.13186E+08     187   0.11212E-02   0.70860E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.15502                             8
a  omega          
a  Local Time Step      1.3441e-05                         45709


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.13264         0.12852      0.00075286      1.0002e-08
v  Velocity[Y]                 -35.714          31.238          6.2986          20.051
v  Velocity[Z]                 -28.075          31.012        0.043203      -0.0068439
v  ǁVelocityǁ                 0.024732          37.387          10.925          20.277
v  Pressure                    -526.75          373.93         -37.771          28.909
v  k                        8.0618e-12          49.424          1.2999        0.036305
v  omega                        6.5766      4.1483e+08           13647           19.84
v  turbulent_viscosity      7.9588e-15        0.026298       0.0014864        0.003773
v  CourantNb                  0.065475          2118.9          44.932          1.3913
v  FourierNb                1.9383e-05          3350.9          23.603         0.03593
v  total_pressure            1.008e+05       1.017e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14806         0.01078        0.045463


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.13417          4342.5          68.535          1.4272


 TIME FOR THE TIME STEP               50:        0.31848E+02

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


 INSTANT    0.510000000E+01   TIME STEP NUMBER              51
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.484150736E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.58297E+02 0.12591E+02
   Friction velocity        uet   :  0.57759E-03 0.32105E+01
   Friction velocity        uk    :  0.18516E-01 0.26466E+01
   Dimensionless distance   yplus :  0.16678E+00 0.28720E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1559
   Nb of faces within the viscous sub-layer     :        952
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04     743   0.43145E-02   0.10799E+01 
c  VelocityY    0.29385E+04     743   0.43145E-02   0.00000E+00 
c  VelocityZ    0.29385E+04     743   0.43145E-02   0.00000E+00 
c  Pressure     0.36940E+00    7088   0.54086E-01   0.16791E+00 
c  k            0.10253E+03    1105   0.13200E-02   0.23724E+00 
c  omega        0.96866E+09      37   0.51107E-05   0.17996E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.069882                            11
a  omega               -1.3911e+05                             2
a  Local Time Step      1.3604e-05                         45705


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.1394          0.1329       0.0008131      1.3825e-08
v  Velocity[Y]                 -25.774          31.163          6.3754          20.051
v  Velocity[Z]                 -28.096          31.012        0.095251      -0.0071618
v  ǁVelocityǁ                 0.024617          32.259           10.98          20.279
v  Pressure                    -527.06           370.6         -37.671          29.035
v  k                        1.4862e-08          40.195          1.4997        0.037361
v  omega                        4.0883      2.0778e+08           11206          19.413
v  turbulent_viscosity      2.7495e-17        0.026178       0.0017425       0.0038097
v  CourantNb                   0.12278          2344.4          45.496          1.3918
v  FourierNb                1.9606e-05          4829.8          28.363        0.039427
v  total_pressure            1.008e+05       1.017e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14934        0.010781        0.045514


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.21987            5032          73.858          1.4312


 TIME FOR THE TIME STEP               51:        0.33806E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.627525776E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29788E+02 0.13113E+02
   Friction velocity        uet   :  0.22185E-02 0.25623E+01
   Friction velocity        uk    :  0.18489E-01 0.27564E+01
   Dimensionless distance   yplus :  0.43202E-01 0.28900E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1511
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29369E+04     936   0.40356E-02   0.10679E+01 
c  VelocityY    0.29369E+04     936   0.40356E-02   0.00000E+00 
c  VelocityZ    0.29369E+04     936   0.40356E-02   0.00000E+00 
c  Pressure     0.37919E+00    7003   0.48736E-01   0.17235E+00 
c  k            0.11520E+03    1224   0.83680E-03   0.23480E+00 
c  omega        0.24348E+09      98   0.10368E-04   0.49018E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.027444                             9
a  omega               -1.2167e+05                             2
a  Local Time Step      1.3567e-05                         45703


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.15179         0.12023      0.00082615      1.5081e-08
v  Velocity[Y]                 -22.779          31.048          6.4404          20.052
v  Velocity[Z]                 -28.528           30.85         0.15842      -0.0076557
v  ǁVelocityǁ                 0.017638          32.626          10.982          20.282
v  Pressure                    -526.84          368.89         -36.582          29.421
v  k                        8.1416e-09          50.428          1.6928        0.038482
v  omega                         6.554      1.0415e+08           10043          19.102
v  turbulent_viscosity        1.48e-14        0.026186       0.0020076       0.0038469
v  CourantNb                  0.073695          2982.9          45.877          1.3922
v  FourierNb                1.9848e-05          4974.2          33.164         0.04306
v  total_pressure            1.008e+05      1.0169e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14807        0.010782        0.045583


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27863          5025.9          79.041          1.4352


 TIME FOR THE TIME STEP               52:        0.37134E+02

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


 INSTANT    0.530000000E+01   TIME STEP NUMBER              53
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.364825296E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33557E+02 0.13312E+02
   Friction velocity        uet   :  0.50310E-03 0.24700E+01
   Friction velocity        uk    :  0.16687E-01 0.30127E+01
   Dimensionless distance   yplus :  0.81428E-01 0.28842E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1501
   Nb of faces within the viscous sub-layer     :        955
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    1097   0.42229E-02   0.10632E+01 
c  VelocityY    0.29353E+04    1097   0.42229E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    1097   0.42229E-02   0.00000E+00 
c  Pressure     0.36456E+00    7015   0.44742E-01   0.16518E+00 
c  k            0.12638E+03    1348   0.66652E-03   0.29060E+00 
c  omega        0.62932E+08     162   0.21564E-04   0.14470E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0018835                             2
a  omega          
a  Local Time Step      1.3895e-05                         45729


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.16884          0.1435      0.00089774      2.3054e-08
v  Velocity[Y]                 -22.835          31.016          6.4719          20.052
v  Velocity[Z]                 -28.172          30.721         0.23818       -0.007899
v  ǁVelocityǁ                 0.008786          32.353          10.933          20.283
v  Pressure                    -523.16          367.86         -34.884          29.238
v  k                        1.4788e-08          53.047          1.8522        0.039632
v  omega                        6.5457      5.2558e+07          9285.1          18.808
v  turbulent_viscosity      2.4645e-15        0.026281       0.0022812       0.0038848
v  CourantNb                  0.081439          2219.7          45.932          1.3923
v  FourierNb                2.0102e-05          5840.6          37.782        0.046693
v  total_pressure            1.008e+05      1.0169e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14891        0.010784        0.045645


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20123          5856.8          83.713          1.4389


 TIME FOR THE TIME STEP               53:        0.38553E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.297119818E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31773E+02 0.13830E+02
   Friction velocity        uet   :  0.14346E-02 0.26110E+01
   Friction velocity        uk    :  0.20202E-01 0.31319E+01
   Dimensionless distance   yplus :  0.11696E+00 0.29621E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1304
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29340E+04    1004   0.42015E-02   0.10769E+01 
c  VelocityY    0.29340E+04    1004   0.42015E-02   0.00000E+00 
c  VelocityZ    0.29340E+04    1004   0.42015E-02   0.00000E+00 
c  Pressure     0.38130E+00    6874   0.43935E-01   0.17269E+00 
c  k            0.13294E+03    1443   0.73817E-03   0.28586E+00 
c  omega        0.22248E+08     266   0.11640E-03   0.27751E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056086                             4
a  omega                    -93778                             1
a  Local Time Step      1.4283e-05                         45747


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.16525         0.14354      0.00094885      3.2759e-08
v  Velocity[Y]                 -22.992          30.858          6.4322          20.053
v  Velocity[Z]                 -28.141          30.565         0.28599      -0.0083472
v  ǁVelocityǁ                 0.010643          32.335          10.864          20.285
v  Pressure                    -521.81          367.13         -33.251          28.997
v  k                         2.124e-09          56.226          1.9739        0.040819
v  omega                        6.5383      1.2677e+08          9259.3          18.555
v  turbulent_viscosity      2.1562e-15        0.026327       0.0025545       0.0039233
v  CourantNb                  0.043377          2264.7          45.428           1.392
v  FourierNb                2.0368e-05          6910.5          41.019        0.049865
v  total_pressure            1.008e+05      1.0169e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14756        0.010784         0.04567


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24522          6926.7          86.447          1.4419


 TIME FOR THE TIME STEP               54:        0.37666E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.344238863E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32234E+02 0.19309E+02
   Friction velocity        uet   :  0.19297E-03 0.24421E+01
   Friction velocity        uk    :  0.21266E-01 0.26653E+01
   Dimensionless distance   yplus :  0.13294E+00 0.39193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1183
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29328E+04    1080   0.41387E-02   0.10840E+01 
c  VelocityY    0.29328E+04    1080   0.41387E-02   0.00000E+00 
c  VelocityZ    0.29328E+04    1080   0.41387E-02   0.00000E+00 
c  Pressure     0.36977E+00    6662   0.43261E-01   0.16703E+00 
c  k            0.13486E+03    1516   0.71249E-03   0.25456E+00 
c  omega        0.63858E+08     157   0.86835E-04   0.11329E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5163e+05                             3
a  Local Time Step      1.4228e-05                         45756


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17473         0.15061       0.0010216      4.9785e-08
v  Velocity[Y]                 -25.173          30.803          6.3547          20.052
v  Velocity[Z]                 -28.046          30.265           0.309      -0.0086911
v  ǁVelocityǁ                 0.021225          32.046          10.775          20.286
v  Pressure                    -518.91           366.9         -31.994           28.71
v  k                        4.1739e-08          45.707           2.105         0.04212
v  omega                        6.5331      2.6558e+08          9945.4          18.389
v  turbulent_viscosity      4.8987e-15        0.027398       0.0028188        0.003963
v  CourantNb                  0.028549            2276          45.002          1.3919
v  FourierNb                2.0573e-05          8069.2          43.366        0.052663
v  total_pressure           1.0081e+05      1.0169e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14715        0.010784         0.04571


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27125          8086.9          88.367          1.4445


 TIME FOR THE TIME STEP               55:        0.37976E+02

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


 INSTANT    0.560000000E+01   TIME STEP NUMBER              56
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.139969283E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34034E+02 0.20101E+02
   Friction velocity        uet   :  0.56677E-03 0.29075E+01
   Friction velocity        uk    :  0.11431E-01 0.28026E+01
   Dimensionless distance   yplus :  0.12492E+00 0.30095E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1058
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29317E+04    1198   0.40015E-02   0.10753E+01 
c  VelocityY    0.29317E+04    1198   0.40015E-02   0.00000E+00 
c  VelocityZ    0.29317E+04    1198   0.40015E-02   0.00000E+00 
c  Pressure     0.37023E+00    6828   0.41666E-01   0.16872E+00 
c  k            0.15049E+03    1566   0.64457E-03   0.25652E+00 
c  omega        0.27749E+09      77   0.18957E-04   0.11975E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00079655                             4
a  omega          
a  Local Time Step      1.4646e-05                         45794


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.1826         0.14113       0.0010882      7.5662e-08
v  Velocity[Y]                 -22.865          30.705          6.3069          20.052
v  Velocity[Z]                 -27.784          30.894         0.30158      -0.0091194
v  ǁVelocityǁ                0.0059015          35.179          10.676          20.288
v  Pressure                    -516.83          368.88          -29.41          29.213
v  k                        1.0356e-08          53.368          2.2131        0.043511
v  omega                        6.5295       2.339e+08          9975.8          18.187
v  turbulent_viscosity      2.0327e-14        0.030089       0.0030882       0.0040035
v  CourantNb                  0.010529            2234          45.072           1.392
v  FourierNb                2.0585e-05          9065.3          46.571        0.055773
v  total_pressure           1.0081e+05      1.0169e+05       1.013e+05      1.0135e+05
v  Local Time Step                0.01          0.1476        0.010785        0.045738


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30566            9085          91.643          1.4478


 TIME FOR THE TIME STEP               56:        0.40074E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.214007341E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31804E+02 0.20064E+02
   Friction velocity        uet   :  0.17087E-02 0.29124E+01
   Friction velocity        uk    :  0.28707E-01 0.27966E+01
   Dimensionless distance   yplus :  0.17816E+00 0.30056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :       1029
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29308E+04    1316   0.41317E-02   0.10397E+01 
c  VelocityY    0.29308E+04    1316   0.41317E-02   0.00000E+00 
c  VelocityZ    0.29308E+04    1316   0.41317E-02   0.00000E+00 
c  Pressure     0.35486E+00    6912   0.41329E-01   0.16161E+00 
c  k            0.17400E+03    1603   0.55195E-03   0.30994E+00 
c  omega        0.26576E+09      68   0.99488E-05   0.31524E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00023365                             1
a  omega          
a  Local Time Step      1.4841e-05                         45765


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17761         0.18539       0.0010122      1.0105e-07
v  Velocity[Y]                 -23.053          30.595           6.273          20.052
v  Velocity[Z]                 -30.405          30.686          0.2926       -0.009665
v  ǁVelocityǁ                 0.012981          36.537           10.59           20.29
v  Pressure                    -518.02          371.51          -26.62           29.82
v  k                        2.8444e-08          58.695          2.3355        0.045002
v  omega                        6.5271      1.1705e+08          9160.1          17.921
v  turbulent_viscosity      1.8652e-15        0.032334       0.0033499        0.004045
v  CourantNb                  0.044677          2231.7          45.035          1.3917
v  FourierNb                2.0604e-05          9875.7          50.262        0.059122
v  total_pressure           1.0081e+05       1.017e+05       1.013e+05      1.0135e+05
v  Local Time Step                0.01         0.14762        0.010786        0.045779


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.29619            9898          95.297          1.4508


 TIME FOR THE TIME STEP               57:        0.40460E+02

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


 INSTANT    0.580000000E+01   TIME STEP NUMBER              58
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.786931195E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31178E+02 0.19928E+02
   Friction velocity        uet   :  0.25652E-02 0.30992E+01
   Friction velocity        uk    :  0.17320E-01 0.26947E+01
   Dimensionless distance   yplus :  0.99793E-01 0.30255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        937
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29301E+04    1411   0.41260E-02   0.99641E+00 
c  VelocityY    0.29301E+04    1411   0.41260E-02   0.00000E+00 
c  VelocityZ    0.29301E+04    1411   0.41260E-02   0.00000E+00 
c  Pressure     0.33840E+00    6958   0.43394E-01   0.15365E+00 
c  k            0.20625E+03    1608   0.49483E-03   0.45935E+00 
c  omega        0.68634E+08     129   0.27786E-04   0.19758E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.3045e-05                             1
a  omega          
a  Local Time Step      1.4834e-05                         45716


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.16401         0.27166      0.00085786      1.3804e-07
v  Velocity[Y]                 -23.087          30.477          6.2715          20.052
v  Velocity[Z]                 -31.134          30.993         0.28285      -0.0099785
v  ǁVelocityǁ                0.0084774          35.974           10.54          20.292
v  Pressure                    -520.38          373.24         -23.383          30.687
v  k                        3.3062e-08          60.291          2.4709        0.046624
v  omega                        6.5247      5.8762e+07          9070.4          17.766
v  turbulent_viscosity      1.2277e-14         0.03496       0.0036155       0.0040877
v  CourantNb                  0.021942          2251.3          44.496          1.3909
v  FourierNb                2.0699e-05           11813          53.849        0.062574
v  total_pressure            1.008e+05       1.017e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.15323        0.010787        0.045818


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.15158           12054          98.346          1.4535


 TIME FOR THE TIME STEP               58:        0.40840E+02

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


 INSTANT    0.590000000E+01   TIME STEP NUMBER              59
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.846169619E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30654E+02 0.17878E+02
   Friction velocity        uet   :  0.22620E-03 0.29924E+01
   Friction velocity        uk    :  0.20864E-01 0.28823E+01
   Dimensionless distance   yplus :  0.10716E+00 0.30430E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        893
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29294E+04    1509   0.40615E-02   0.95643E+00 
c  VelocityY    0.29294E+04    1509   0.40615E-02   0.00000E+00 
c  VelocityZ    0.29294E+04    1509   0.40615E-02   0.00000E+00 
c  Pressure     0.35297E+00    6974   0.44336E-01   0.16018E+00 
c  k            0.24969E+03    1569   0.46975E-03   0.63489E+00 
c  omega        0.30072E+08     216   0.93108E-04   0.31042E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.4258e-05                             1
a  omega          
a  Local Time Step      1.3616e-05                         45701


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.19856         0.35189      0.00064353      1.7456e-07
v  Velocity[Y]                 -23.152          30.392          6.2953          20.053
v  Velocity[Z]                 -30.899          29.839         0.29021       -0.010302
v  ǁVelocityǁ                0.0097742          33.566            10.5          20.294
v  Pressure                    -526.74          373.08         -20.423          31.407
v  k                        3.5309e-09          61.613          2.5975        0.048365
v  omega                        6.5234      1.2298e+08          9297.3          17.613
v  turbulent_viscosity      2.2397e-14          0.0441       0.0038824       0.0041318
v  CourantNb                   0.10427          2558.2          44.067          1.3902
v  FourierNb                2.0819e-05           12855          56.585        0.065864
v  total_pressure            1.008e+05       1.017e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14924        0.010788        0.045853


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34289           13110          100.65          1.4561


 TIME FOR THE TIME STEP               59:        0.41973E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.445461418E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29546E+02 0.14804E+02
   Friction velocity        uet   :  0.38020E-03 0.28279E+01
   Friction velocity        uk    :  0.11227E-01 0.29743E+01
   Dimensionless distance   yplus :  0.10076E+00 0.30554E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        822
   Nb of faces within the viscous sub-layer     :        943
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29289E+04    1598   0.43192E-02   0.90716E+00 
c  VelocityY    0.29289E+04    1598   0.43192E-02   0.00000E+00 
c  VelocityZ    0.29289E+04    1598   0.43192E-02   0.00000E+00 
c  Pressure     0.39680E+00    6959   0.44695E-01   0.18165E+00 
c  k            0.30249E+03    1344   0.44484E-03   0.73204E+00 
c  omega        0.61476E+08     136   0.23069E-04   0.11708E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -43469                             1
a  Local Time Step      1.4209e-05                         45726


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25164         0.37939      0.00019796      2.2425e-07
v  Velocity[Y]                 -24.416          30.277          6.2784          20.053
v  Velocity[Z]                  -29.81          29.347          0.3152       -0.010684
v  ǁVelocityǁ                0.0093201          31.134           10.44          20.296
v  Pressure                    -534.27          370.89         -18.493          31.925
v  k                        4.8866e-08          79.259          2.6866        0.050127
v  omega                        6.5227      6.1959e+07          9059.3          17.422
v  turbulent_viscosity      2.0613e-14        0.059345        0.004151       0.0041777
v  CourantNb                   0.07268          2349.7          43.565          1.3895
v  FourierNb                2.0924e-05           13446          59.054        0.069019
v  total_pressure           1.0079e+05       1.017e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1604        0.010788        0.045854


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.19653           13687          102.62          1.4585


 TIME FOR THE TIME STEP               60:        0.43221E+02

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


 INSTANT    0.610000000E+01   TIME STEP NUMBER              61
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.373990709E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29450E+02 0.14129E+02
   Friction velocity        uet   :  0.10475E-02 0.26422E+01
   Friction velocity        uk    :  0.13203E-01 0.29688E+01
   Dimensionless distance   yplus :  0.11849E+00 0.30606E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        805
   Nb of faces within the viscous sub-layer     :        930
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29285E+04    1619   0.43835E-02   0.83753E+00 
c  VelocityY    0.29285E+04    1619   0.43835E-02   0.00000E+00 
c  VelocityZ    0.29285E+04    1619   0.43835E-02   0.00000E+00 
c  Pressure     0.38437E+00    6950   0.42186E-01   0.17630E+00 
c  k            0.36104E+03    1489   0.40517E-03   0.78481E+00 
c  omega        0.21637E+08     229   0.54259E-04   0.94245E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018745                             1
a  omega          
a  Local Time Step       1.416e-05                         45710


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.23442         0.39189     -0.00014407      2.7267e-07
v  Velocity[Y]                 -26.615          30.451          6.2014          20.052
v  Velocity[Z]                 -27.387          28.221          0.3379       -0.011151
v  ǁVelocityǁ                0.0085117          31.461          10.398          20.297
v  Pressure                    -543.76          366.81         -18.456          32.243
v  k                        7.2494e-07          71.909          2.7427        0.051799
v  omega                        6.5226      4.5079e+07          9027.3          17.244
v  turbulent_viscosity      9.5735e-14        0.070387       0.0043896       0.0042254
v  CourantNb                   0.11245          2057.1          43.169           1.389
v  FourierNb                2.0999e-05           13926          61.728        0.071897
v  total_pressure           1.0078e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01           0.158        0.010787        0.045845


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.32375           14110           104.9          1.4609


 TIME FOR THE TIME STEP               61:        0.43428E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.292816229E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30187E+02 0.17136E+02
   Friction velocity        uet   :  0.20960E-02 0.26076E+01
   Friction velocity        uk    :  0.31637E-01 0.28642E+01
   Dimensionless distance   yplus :  0.22415E+00 0.30640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        789
   Nb of faces within the viscous sub-layer     :        921
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29281E+04    1639   0.45192E-02   0.77332E+00 
c  VelocityY    0.29281E+04    1639   0.45192E-02   0.00000E+00 
c  VelocityZ    0.29281E+04    1639   0.45192E-02   0.00000E+00 
c  Pressure     0.36613E+00    7052   0.38177E-01   0.16776E+00 
c  k            0.40678E+03    1603   0.33675E-03   0.77408E+00 
c  omega        0.36137E+08     215   0.28375E-04   0.10304E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2576e-05                             1
a  omega               -2.3411e+05                             1
a  Local Time Step       1.387e-05                         45720


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17533         0.38425     -0.00036786      3.0637e-07
v  Velocity[Y]                 -23.133          30.755          6.0999          20.051
v  Velocity[Z]                 -27.487           27.36         0.33818       -0.011385
v  ǁVelocityǁ                 0.016254          31.511          10.425          20.298
v  Pressure                    -554.64          361.46         -20.579          32.482
v  k                        1.3654e-09          79.033          2.7889        0.053395
v  omega                        6.5227      3.0508e+07          9218.6          17.098
v  turbulent_viscosity      1.3124e-13        0.072449       0.0045925        0.004275
v  CourantNb                  0.021303          2035.2          42.833          1.3888
v  FourierNb                2.1103e-05           13507          64.593        0.074474
v  total_pressure           1.0077e+05      1.0169e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.16029        0.010788        0.045843


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30067           13678          107.43          1.4633


 TIME FOR THE TIME STEP               62:        0.43455E+02

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


 INSTANT    0.630000000E+01   TIME STEP NUMBER              63
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.189139909E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28104E+02 0.15927E+02
   Friction velocity        uet   :  0.57973E-03 0.21838E+01
   Friction velocity        uk    :  0.97275E-02 0.30382E+01
   Dimensionless distance   yplus :  0.10727E+00 0.30375E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        816
   Nb of faces within the viscous sub-layer     :        889
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29278E+04    1615   0.45466E-02   0.74717E+00 
c  VelocityY    0.29278E+04    1615   0.45466E-02   0.00000E+00 
c  VelocityZ    0.29278E+04    1615   0.45466E-02   0.00000E+00 
c  Pressure     0.41471E+00    7033   0.39807E-01   0.19062E+00 
c  k            0.41555E+03    1676   0.37327E-03   0.69380E+00 
c  omega        0.21517E+08     389   0.38360E-04   0.90959E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3482e-05                         45696


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17742         0.36903     -0.00052508      2.9979e-07
v  Velocity[Y]                 -35.179          31.055          6.0692          20.052
v  Velocity[Z]                 -27.585          27.649         0.35348       -0.011711
v  ǁVelocityǁ                0.0050675          35.725          10.449          20.301
v  Pressure                    -566.91          356.79         -24.185           33.06
v  k                        2.8184e-08          88.734           2.847        0.055062
v  omega                         6.523      3.1421e+07          9024.3          16.924
v  turbulent_viscosity      8.4923e-16        0.067669       0.0047654       0.0043261
v  CourantNb                  0.057625          2018.4          43.015          1.3891
v  FourierNb                2.1247e-05           12903          66.762        0.076711
v  total_pressure           1.0076e+05      1.0168e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.16606        0.010787        0.045842


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.2989           13071          109.78          1.4659


 TIME FOR THE TIME STEP               63:        0.45311E+02

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


 INSTANT    0.640000000E+01   TIME STEP NUMBER              64
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.830757397E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40878E+02 0.14343E+02
   Friction velocity        uet   :  0.78220E-03 0.32895E+01
   Friction velocity        uk    :  0.17095E-01 0.36772E+01
   Dimensionless distance   yplus :  0.16962E+00 0.35963E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        733
   Nb of faces within the viscous sub-layer     :        884
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29277E+04    1565   0.44365E-02   0.73888E+00 
c  VelocityY    0.29277E+04    1565   0.44365E-02   0.00000E+00 
c  VelocityZ    0.29277E+04    1565   0.44365E-02   0.00000E+00 
c  Pressure     0.41239E+00    7055   0.44841E-01   0.18869E+00 
c  k            0.40916E+03    1493   0.58448E-03   0.56848E+00 
c  omega        0.16759E+08     417   0.36026E-04   0.45575E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3096e-05                         45625


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17838         0.37283      -0.0006604      2.5056e-07
v  Velocity[Y]                 -25.402          31.267           6.105          20.053
v  Velocity[Z]                 -27.782          28.334          0.3567       -0.012239
v  ǁVelocityǁ                0.0096742          31.637          10.487          20.304
v  Pressure                    -579.35          353.59         -27.963          33.669
v  k                        2.9085e-09          51.656          2.8628        0.056812
v  omega                        6.5233      1.6704e+07          8718.2          16.742
v  turbulent_viscosity      1.4083e-14        0.068689       0.0049258       0.0043794
v  CourantNb                   0.13288          2716.5          43.499          1.3896
v  FourierNb                2.1443e-05           12215          67.885        0.078458
v  total_pressure           1.0075e+05      1.0168e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.16142        0.010786        0.045833


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.27926           12397          111.38          1.4681


 TIME FOR THE TIME STEP               64:        0.44609E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.507879301E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29321E+02 0.14445E+02
   Friction velocity        uet   :  0.73421E-03 0.25896E+01
   Friction velocity        uk    :  0.23779E-01 0.29752E+01
   Dimensionless distance   yplus :  0.13908E+00 0.32240E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        772
   Nb of faces within the viscous sub-layer     :        911
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29276E+04    1591   0.43078E-02   0.71558E+00 
c  VelocityY    0.29276E+04    1591   0.43078E-02   0.00000E+00 
c  VelocityZ    0.29276E+04    1591   0.43078E-02   0.00000E+00 
c  Pressure     0.37795E+00    7030   0.46830E-01   0.17310E+00 
c  k            0.41237E+03    1369   0.36573E-03   0.44008E+00 
c  omega        0.13381E+08     310   0.39539E-04   0.24125E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -44229                             1
a  Local Time Step      1.3013e-05                         45633


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.15351         0.37358     -0.00089297      2.2637e-07
v  Velocity[Y]                 -25.205          31.422           6.196          20.052
v  Velocity[Z]                 -27.795          28.881         0.33398        -0.01247
v  ǁVelocityǁ                0.0069472          32.114          10.518          20.305
v  Pressure                    -590.29          352.31         -30.673          34.107
v  k                        1.4099e-08          53.929          2.8726        0.058643
v  omega                        5.4827      1.1723e+07          8345.2          16.562
v  turbulent_viscosity      2.0716e-15        0.067074       0.0050565       0.0044343
v  CourantNb                  0.040638          2635.9           43.65            1.39
v  FourierNb                2.1708e-05           11423          66.994        0.079173
v  total_pressure           1.0073e+05      1.0168e+05      1.0129e+05      1.0136e+05
v  Local Time Step                0.01          0.1747        0.010785        0.045808


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.23606           11627          110.64          1.4691


 TIME FOR THE TIME STEP               65:        0.44595E+02

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


 INSTANT    0.660000000E+01   TIME STEP NUMBER              66
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.483674863E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32096E+02 0.14371E+02
   Friction velocity        uet   :  0.10154E-02 0.25151E+01
   Friction velocity        uk    :  0.25865E-01 0.27503E+01
   Dimensionless distance   yplus :  0.10709E+00 0.30431E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        820
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29276E+04    1798   0.45740E-02   0.68916E+00 
c  VelocityY    0.29276E+04    1798   0.45740E-02   0.00000E+00 
c  VelocityZ    0.29276E+04    1798   0.45740E-02   0.00000E+00 
c  Pressure     0.37129E+00    7036   0.41875E-01   0.16952E+00 
c  k            0.42555E+03    1488   0.34466E-03   0.38744E+00 
c  omega        0.13667E+08     364   0.20275E-03   0.26950E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2983e-05                         45688


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17369         0.31286      -0.0011766      2.7186e-07
v  Velocity[Y]                 -23.733          31.516          6.3215          20.052
v  Velocity[Z]                 -27.677          29.316         0.28305       -0.012656
v  ǁVelocityǁ                 0.010607           32.14          10.529          20.306
v  Pressure                    -600.31          353.97         -31.242          34.551
v  k                        5.4731e-08          43.827          2.8968        0.060555
v  omega                        3.8446      7.7399e+07          9100.7          16.497
v  turbulent_viscosity      6.8197e-15        0.064711       0.0051815       0.0044908
v  CourantNb                  0.051247            1994          43.677          1.3902
v  FourierNb                2.2109e-05           11586          66.219        0.079725
v  total_pressure           1.0072e+05      1.0168e+05      1.0129e+05      1.0136e+05
v  Local Time Step                0.01         0.15647        0.010783        0.045755


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.20792           11771           109.9          1.4699


 TIME FOR THE TIME STEP               66:        0.47177E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.924530341E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32917E+02 0.15138E+02
   Friction velocity        uet   :  0.84881E-03 0.25527E+01
   Friction velocity        uk    :  0.20602E-01 0.29086E+01
   Dimensionless distance   yplus :  0.17036E+00 0.28667E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        785
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29277E+04    1665   0.46406E-02   0.66642E+00 
c  VelocityY    0.29277E+04    1665   0.46406E-02   0.00000E+00 
c  VelocityZ    0.29277E+04    1665   0.46406E-02   0.00000E+00 
c  Pressure     0.38878E+00    6991   0.36076E-01   0.17731E+00 
c  k            0.44145E+03    1571   0.31662E-03   0.46958E+00 
c  omega        0.41052E+08     331   0.36536E-04   0.11862E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0031846                             1
a  omega                    -75310                             1
a  Local Time Step      1.2419e-05                         45722


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22409         0.29756      -0.0013109      2.7525e-07
v  Velocity[Y]                 -23.514          31.593          6.4425          20.053
v  Velocity[Z]                 -27.299          29.314         0.22676       -0.013041
v  ǁVelocityǁ                 0.024015          32.326          10.518          20.309
v  Pressure                    -611.25          357.92         -30.262          35.187
v  k                        5.3128e-08          39.594          2.9134        0.062537
v  omega                        2.1576      3.9514e+07          8791.1          16.339
v  turbulent_viscosity      1.4291e-14        0.073331       0.0053077       0.0045492
v  CourantNb                   0.07132          1990.8          43.689          1.3901
v  FourierNb                2.2535e-05           11618          66.635        0.080613
v  total_pressure           1.0071e+05      1.0168e+05      1.0129e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010782        0.045725


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43108           11783          110.32          1.4708


 TIME FOR THE TIME STEP               67:        0.45498E+02

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


 INSTANT    0.680000000E+01   TIME STEP NUMBER              68
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.774071647E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32022E+02 0.14941E+02
   Friction velocity        uet   :  0.15531E-02 0.25070E+01
   Friction velocity        uk    :  0.19198E-01 0.30155E+01
   Dimensionless distance   yplus :  0.88771E-01 0.36860E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        692
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29278E+04    1505   0.47984E-02   0.65143E+00 
c  VelocityY    0.29278E+04    1505   0.47984E-02   0.00000E+00 
c  VelocityZ    0.29278E+04    1505   0.47984E-02   0.00000E+00 
c  Pressure     0.39097E+00    6994   0.34938E-01   0.17840E+00 
c  k            0.45643E+03    1539   0.25337E-03   0.47954E+00 
c  omega        0.18444E+08     322   0.35556E-04   0.35092E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9303e+05                             3
a  Local Time Step      1.3444e-05                         45761


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21468         0.29277      -0.0013895      1.8104e-07
v  Velocity[Y]                 -23.664          31.643          6.5134          20.053
v  Velocity[Z]                 -26.637          29.237         0.15938       -0.013365
v  ǁVelocityǁ                 0.017185          32.496          10.513           20.31
v  Pressure                    -620.52          363.43         -28.016          35.599
v  k                        7.1104e-08          35.011          2.9196        0.064607
v  omega                        1.2439       2.132e+07            8395          16.162
v  turbulent_viscosity       2.441e-14        0.087397        0.005463       0.0046103
v  CourantNb                  0.019733          1986.8          43.763          1.3901
v  FourierNb                2.3081e-05           12044          66.701        0.081878
v  total_pressure            1.007e+05      1.0169e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14759        0.010781        0.045693


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.45353           12061          110.46           1.472


 TIME FOR THE TIME STEP               68:        0.44012E+02

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


 INSTANT    0.690000000E+01   TIME STEP NUMBER              69
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.144336590E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30707E+02 0.19086E+02
   Friction velocity        uet   :  0.99184E-03 0.24169E+01
   Friction velocity        uk    :  0.23541E-01 0.29113E+01
   Dimensionless distance   yplus :  0.17206E+00 0.33442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        650
   Nb of faces within the viscous sub-layer     :       1069
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29280E+04    1472   0.47965E-02   0.64046E+00 
c  VelocityY    0.29280E+04    1472   0.47965E-02   0.00000E+00 
c  VelocityZ    0.29280E+04    1472   0.47965E-02   0.00000E+00 
c  Pressure     0.40919E+00    6988   0.34181E-01   0.18810E+00 
c  k            0.47547E+03    1572   0.23310E-03   0.47523E+00 
c  omega        0.10833E+08     247   0.36141E-03   0.51165E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1744e+05                             1
a  Local Time Step      1.3697e-05                         45754


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22465         0.25725      -0.0015546      3.7711e-08
v  Velocity[Y]                 -23.759          31.625          6.5442          20.054
v  Velocity[Z]                 -26.325          29.801        0.096046        -0.01397
v  ǁVelocityǁ                 0.014447          32.242          10.491          20.313
v  Pressure                    -628.71          369.77         -24.914          36.148
v  k                        9.4009e-08          32.298          2.9387        0.066816
v  omega                        1.1695      1.1075e+08          9540.9          16.111
v  turbulent_viscosity      1.5486e-14          0.1001       0.0056249       0.0046735
v  CourantNb                  0.050322          1982.6          43.848          1.3903
v  FourierNb                2.3742e-05           12551          66.445        0.083031
v  total_pressure            1.007e+05      1.0169e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14878         0.01078        0.045679


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.39292           12569          110.29          1.4734


 TIME FOR THE TIME STEP               69:        0.42777E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.683593597E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32583E+02 0.19580E+02
   Friction velocity        uet   :  0.19058E-02 0.26737E+01
   Friction velocity        uk    :  0.32446E-01 0.29591E+01
   Dimensionless distance   yplus :  0.13804E+00 0.28759E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        666
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29283E+04    1507   0.47949E-02   0.64232E+00 
c  VelocityY    0.29283E+04    1507   0.47949E-02   0.00000E+00 
c  VelocityZ    0.29283E+04    1507   0.47949E-02   0.00000E+00 
c  Pressure     0.38940E+00    7004   0.33598E-01   0.17795E+00 
c  k            0.49683E+03    1588   0.25278E-03   0.49472E+00 
c  omega        0.80829E+08     115   0.22546E-04   0.14951E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7111e+05                             3
a  Local Time Step      1.3189e-05                         45752


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25754         0.23843       -0.001751      1.7682e-07
v  Velocity[Y]                 -23.836           31.57          6.5678          20.053
v  Velocity[Z]                 -28.053          30.597        0.021471       -0.014172
v  ǁVelocityǁ                0.0018058          33.829          10.467          20.313
v  Pressure                    -636.37          376.42         -20.624          36.769
v  k                        2.9073e-08          43.554          2.9747        0.069159
v  omega                       0.76829      5.5891e+07            9000          15.968
v  turbulent_viscosity      2.0474e-14         0.10887        0.005802       0.0047398
v  CourantNb                  0.076105          1983.1          44.026          1.3906
v  FourierNb                2.4533e-05           12846          67.456        0.084713
v  total_pressure           1.0069e+05       1.017e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14834        0.010779        0.045679


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.33339           12874          111.48          1.4753


 TIME FOR THE TIME STEP               70:        0.43399E+02

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


 INSTANT    0.710000000E+01   TIME STEP NUMBER              71
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.475705135E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27593E+02 0.16783E+02
   Friction velocity        uet   :  0.53034E-03 0.28176E+01
   Friction velocity        uk    :  0.24150E-01 0.27166E+01
   Dimensionless distance   yplus :  0.15666E+00 0.28824E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        626
   Nb of faces within the viscous sub-layer     :       1060
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29288E+04    1539   0.50425E-02   0.61810E+00 
c  VelocityY    0.29288E+04    1539   0.50425E-02   0.00000E+00 
c  VelocityZ    0.29288E+04    1539   0.50425E-02   0.00000E+00 
c  Pressure     0.40481E+00    7047   0.34648E-01   0.18525E+00 
c  k            0.52048E+03    1484   0.23075E-03   0.56027E+00 
c  omega        0.23126E+08     187   0.34294E-03   0.23904E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00084478                             1
a  omega                    -65836                             1
a  Local Time Step      1.3964e-05                         45739


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.28733         0.21612      -0.0019719     -2.2614e-07
v  Velocity[Y]                 -23.928           31.54          6.5884          20.053
v  Velocity[Z]                 -30.595          30.493       -0.036379       -0.014245
v  ǁVelocityǁ                 0.010157          35.523          10.479          20.314
v  Pressure                    -640.03          380.02           -16.7          37.501
v  k                        2.4034e-08          60.453          3.0291         0.07171
v  omega                       0.47471      3.7998e+08          9799.2          15.878
v  turbulent_viscosity      7.7721e-15         0.11396       0.0059896       0.0048094
v  CourantNb                  0.095463          1990.2           43.94          1.3904
v  FourierNb                2.5467e-05           13301          68.712        0.086611
v  total_pressure           1.0068e+05      1.0171e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14815        0.010777        0.045645


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55423           13337          112.65          1.4771


 TIME FOR THE TIME STEP               71:        0.43351E+02

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


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




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.227870110E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31380E+02 0.16490E+02
   Friction velocity        uet   :  0.11728E-02 0.29965E+01
   Friction velocity        uk    :  0.16353E-01 0.28185E+01
   Dimensionless distance   yplus :  0.16500E+00 0.28743E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        670
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29296E+04    1529   0.50638E-02   0.60452E+00 
c  VelocityY    0.29296E+04    1529   0.50638E-02   0.00000E+00 
c  VelocityZ    0.29296E+04    1529   0.50638E-02   0.00000E+00 
c  Pressure     0.40207E+00    7029   0.36219E-01   0.18413E+00 
c  k            0.54952E+03    1326   0.22456E-03   0.65503E+00 
c  omega        0.66862E+09      72   0.55850E-05   0.60392E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030867                             1
a  omega               -4.0597e+05                             1
a  Local Time Step       1.348e-05                         45715


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.30998         0.19944      -0.0021193     -2.2921e-07
v  Velocity[Y]                 -23.997          31.497          6.6028          20.053
v  Velocity[Z]                 -31.367          30.076       -0.058979       -0.014671
v  ǁVelocityǁ                 0.018153          34.828          10.535          20.316
v  Pressure                    -641.46          380.34         -13.168          38.131
v  k                        9.6608e-09          78.789          3.0978        0.074446
v  omega                       0.28511      1.9005e+08          8976.3          15.716
v  turbulent_viscosity      1.1696e-14          0.1155       0.0061958       0.0048836
v  CourantNb                   0.03753          2001.2          43.531          1.3899
v  FourierNb                2.6572e-05           13528          70.352        0.088805
v  total_pressure           1.0068e+05      1.0171e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14916        0.010776        0.045587


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.57762           13571          113.88          1.4787


 TIME FOR THE TIME STEP               72:        0.43253E+02

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


 INSTANT    0.730000000E+01   TIME STEP NUMBER              73
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.344675176E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26665E+02 0.17360E+02
   Friction velocity        uet   :  0.80480E-03 0.29007E+01
   Friction velocity        uk    :  0.11851E-01 0.31314E+01
   Dimensionless distance   yplus :  0.16882E+00 0.28652E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        687
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29305E+04    1544   0.48859E-02   0.58502E+00 
c  VelocityY    0.29305E+04    1544   0.48859E-02   0.00000E+00 
c  VelocityZ    0.29305E+04    1544   0.48859E-02   0.00000E+00 
c  Pressure     0.39839E+00    7030   0.36219E-01   0.18190E+00 
c  k            0.58648E+03    1582   0.20742E-03   0.72890E+00 
c  omega        0.16684E+09      81   0.14162E-04   0.28313E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2381e+05                             2
a  Local Time Step      1.3998e-05                         45663


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.35601         0.17657      -0.0021242     -4.0996e-07
v  Velocity[Y]                 -24.105          31.382          6.6172          20.053
v  Velocity[Z]                  -30.71          29.219        -0.04305       -0.014598
v  ǁVelocityǁ                 0.025448          32.855          10.566          20.318
v  Pressure                    -643.72          377.68         -10.762          38.241
v  k                        4.3429e-08          90.173          3.1649        0.077313
v  omega                       0.17103      9.5172e+07          8981.9          15.627
v  turbulent_viscosity      5.8801e-15         0.11459       0.0063948       0.0049623
v  CourantNb                  0.081599          2176.7          43.315          1.3893
v  FourierNb                2.7863e-05           13567          71.649        0.090977
v  total_pressure           1.0068e+05       1.017e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14766        0.010776        0.045536


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.5463           13608          114.96          1.4803


 TIME FOR THE TIME STEP               73:        0.43066E+02

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


 INSTANT    0.740000000E+01   TIME STEP NUMBER              74
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.542167261E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26381E+02 0.16161E+02
   Friction velocity        uet   :  0.30602E-02 0.28222E+01
   Friction velocity        uk    :  0.12152E-01 0.32870E+01
   Dimensionless distance   yplus :  0.77000E-01 0.29405E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        608
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29316E+04    1578   0.49285E-02   0.54017E+00 
c  VelocityY    0.29316E+04    1578   0.49285E-02   0.00000E+00 
c  VelocityZ    0.29316E+04    1578   0.49285E-02   0.00000E+00 
c  Pressure     0.38816E+00    6975   0.37078E-01   0.17639E+00 
c  k            0.62441E+03    1714   0.19826E-03   0.78179E+00 
c  omega        0.52542E+08     139   0.65567E-04   0.44558E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00066794                             1
a  omega          
a  Local Time Step       1.388e-05                         45637


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.3619         0.16855      -0.0019122     -4.2538e-07
v  Velocity[Y]                 -24.141          31.314           6.575          20.053
v  Velocity[Z]                 -29.256          28.451      -0.0062245       -0.014536
v  ǁVelocityǁ                 0.034815          31.332          10.534          20.319
v  Pressure                    -644.94          373.32         -9.5069          38.047
v  k                        1.0998e-07          79.177          3.2162        0.080261
v  omega                       0.10574      1.4269e+08          9214.6          15.555
v  turbulent_viscosity      6.1937e-15         0.11592       0.0065904       0.0050455
v  CourantNb                  0.052221            2244          43.284          1.3888
v  FourierNb                2.9063e-05           13431           73.41         0.09326
v  total_pressure           1.0068e+05       1.017e+05      1.0132e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010775        0.045442


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.30582           13464          116.69          1.4821


 TIME FOR THE TIME STEP               74:        0.43891E+02

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


 INSTANT    0.750000000E+01   TIME STEP NUMBER              75
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.616137275E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27200E+02 0.13991E+02
   Friction velocity        uet   :  0.17713E-02 0.25833E+01
   Friction velocity        uk    :  0.28295E-01 0.29435E+01
   Dimensionless distance   yplus :  0.12025E+00 0.33822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        592
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29326E+04    1532   0.49975E-02   0.47273E+00 
c  VelocityY    0.29326E+04    1532   0.49975E-02   0.00000E+00 
c  VelocityZ    0.29326E+04    1532   0.49975E-02   0.00000E+00 
c  Pressure     0.40343E+00    7036   0.38572E-01   0.18312E+00 
c  k            0.65758E+03    1773   0.19623E-03   0.81856E+00 
c  omega        0.10195E+09      93   0.15904E-04   0.13716E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028149                             2
a  omega          
a  Local Time Step       1.344e-05                         45613


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.38432         0.17845      -0.0015145     -3.6938e-07
v  Velocity[Y]                 -29.548          31.283          6.4536          20.053
v  Velocity[Z]                  -26.63          27.508        0.037906        -0.01465
v  ǁVelocityǁ                 0.021815          32.101          10.461          20.321
v  Pressure                    -643.09          368.94          -9.456          37.801
v  k                        2.3539e-07          62.963          3.2879        0.083298
v  omega                      0.071283      7.1552e+07            8840           15.45
v  turbulent_viscosity      6.3211e-14         0.11903       0.0067682       0.0051342
v  CourantNb                  0.024749          2006.3          43.105          1.3885
v  FourierNb                3.0124e-05           13152          74.634        0.095312
v  total_pressure           1.0068e+05      1.0169e+05      1.0132e+05      1.0136e+05
v  Local Time Step                0.01         0.14826        0.010775        0.045365


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.25199           13177          117.74          1.4838


 TIME FOR THE TIME STEP               75:        0.43518E+02

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


 INSTANT    0.760000000E+01   TIME STEP NUMBER              76
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.218779412E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29576E+02 0.20265E+02
   Friction velocity        uet   :  0.41005E-03 0.27196E+01
   Friction velocity        uk    :  0.15912E-01 0.29259E+01
   Dimensionless distance   yplus :  0.17051E+00 0.33619E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        601
   Nb of faces within the viscous sub-layer     :       1068
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    1443   0.49589E-02   0.42612E+00 
c  VelocityY    0.29336E+04    1443   0.49589E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    1443   0.49589E-02   0.00000E+00 
c  Pressure     0.41266E+00    6959   0.37232E-01   0.18776E+00 
c  k            0.67734E+03    1624   0.22770E-03   0.80180E+00 
c  omega        0.31901E+08     201   0.25797E-04   0.42151E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.3227e-06                             1
a  omega          
a  Local Time Step      1.3343e-05                         45640


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.34304         0.17452      -0.0010292     -3.4938e-07
v  Velocity[Y]                 -24.822          31.257          6.2993          20.054
v  Velocity[Z]                 -26.968          28.273        0.066914       -0.014524
v  ǁVelocityǁ                 0.022382          32.112          10.404          20.323
v  Pressure                    -639.86           363.8          -11.42          37.073
v  k                         3.124e-08          73.634          3.3863        0.086493
v  omega                      0.054566      3.6194e+07          8518.3          15.344
v  turbulent_viscosity      3.4071e-14         0.12409       0.0069505       0.0052289
v  CourantNb                  0.039319          1993.2          42.689           1.388
v  FourierNb                3.1497e-05           12332          76.061        0.097737
v  total_pressure           1.0069e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010776        0.045343


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.42992           12349          118.75          1.4857


 TIME FOR THE TIME STEP               76:        0.41723E+02

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


 INSTANT    0.770000000E+01   TIME STEP NUMBER              77
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.222992847E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31298E+02 0.18645E+02
   Friction velocity        uet   :  0.20349E-02 0.22473E+01
   Friction velocity        uk    :  0.11644E-01 0.35007E+01
   Dimensionless distance   yplus :  0.13205E+00 0.32185E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        601
   Nb of faces within the viscous sub-layer     :       1047
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29343E+04    1485   0.50778E-02   0.39619E+00 
c  VelocityY    0.29343E+04    1485   0.50778E-02   0.00000E+00 
c  VelocityZ    0.29343E+04    1485   0.50778E-02   0.00000E+00 
c  Pressure     0.39362E+00    7029   0.34946E-01   0.17902E+00 
c  k            0.68038E+03    1193   0.28077E-03   0.74601E+00 
c  omega        0.16009E+08     353   0.30375E-04   0.20772E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4155e-06                             1
a  omega          
a  Local Time Step      1.3015e-05                         45618


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.32234          0.2281     -0.00052492     -3.0949e-07
v  Velocity[Y]                 -34.379          31.212          6.2083          20.054
v  Velocity[Z]                 -26.711          28.261        0.099021       -0.014097
v  ǁVelocityǁ                 0.018181          35.217          10.339          20.324
v  Pressure                    -634.97           359.7         -14.194          36.563
v  k                        2.2413e-08          81.903          3.4449        0.089886
v  omega                      0.040385      1.8924e+07            8544          15.255
v  turbulent_viscosity       4.513e-15         0.12988       0.0071331       0.0053301
v  CourantNb                  0.038377          1973.8          42.436          1.3876
v  FourierNb                3.3261e-05           11997          77.915         0.10046
v  total_pressure           1.0069e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1481        0.010773        0.045327


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61275           12132          120.35          1.4881


 TIME FOR THE TIME STEP               77:        0.41193E+02

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


 INSTANT    0.780000000E+01   TIME STEP NUMBER              78
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.405372910E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37489E+02 0.12492E+02
   Friction velocity        uet   :  0.98635E-03 0.32586E+01
   Friction velocity        uk    :  0.10533E-01 0.42674E+01
   Dimensionless distance   yplus :  0.13370E+00 0.39236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        578
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29349E+04    1533   0.49904E-02   0.37382E+00 
c  VelocityY    0.29349E+04    1533   0.49904E-02   0.00000E+00 
c  VelocityZ    0.29349E+04    1533   0.49904E-02   0.00000E+00 
c  Pressure     0.40129E+00    7074   0.35587E-01   0.18277E+00 
c  k            0.68113E+03    1435   0.28632E-03   0.67262E+00 
c  omega        0.12405E+08     326   0.47440E-04   0.14213E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.3618e-06                             1
a  omega               -1.4959e+05                             1
a  Local Time Step      1.2342e-05                         45540


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.2814         0.24919     -6.6517e-05     -4.9347e-07
v  Velocity[Y]                 -25.325          31.205           6.176          20.053
v  Velocity[Z]                 -28.016          27.104         0.11996       -0.013448
v  ǁVelocityǁ                 0.006009          31.988          10.284          20.325
v  Pressure                    -627.68          357.59         -16.896          35.966
v  k                        2.7994e-08          34.079          3.4222        0.093424
v  omega                      0.027209      5.5379e+07          8560.1          15.171
v  turbulent_viscosity      7.8043e-15         0.13455       0.0072869       0.0054384
v  CourantNb                  0.027337          2745.4          42.535          1.3875
v  FourierNb                3.5511e-05           12359          78.688         0.10266
v  total_pressure            1.007e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14824        0.010772        0.045314


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.55637           12472          121.22          1.4901


 TIME FOR THE TIME STEP               78:        0.42916E+02

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


 INSTANT    0.790000000E+01   TIME STEP NUMBER              79
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.441652797E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30541E+02 0.13205E+02
   Friction velocity        uet   :  0.11513E-02 0.23762E+01
   Friction velocity        uk    :  0.15858E-01 0.29723E+01
   Dimensionless distance   yplus :  0.70827E-01 0.29587E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        569
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29355E+04    1555   0.49071E-02   0.35477E+00 
c  VelocityY    0.29355E+04    1555   0.49071E-02   0.00000E+00 
c  VelocityZ    0.29355E+04    1555   0.49071E-02   0.00000E+00 
c  Pressure     0.43511E+00    7050   0.36510E-01   0.19814E+00 
c  k            0.68641E+03    1487   0.18672E-03   0.52939E+00 
c  omega        0.38673E+08     169   0.15611E-04   0.97192E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.7736e-05                             1
a  omega                -2.434e+05                             1
a  Local Time Step       1.277e-05                         45481


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.27006         0.25267      0.00029423     -2.5595e-07
v  Velocity[Y]                  -25.61          31.125          6.1887          20.053
v  Velocity[Z]                   -27.4          27.529         0.12533       -0.013021
v  ǁVelocityǁ                0.0060682          32.249          10.237          20.326
v  Pressure                    -623.15          357.43         -18.481          35.488
v  k                        3.4401e-09          35.823          3.4196        0.097214
v  omega                      0.017657      2.7683e+07          8615.4          15.106
v  turbulent_viscosity      1.1064e-14          0.1394       0.0074022       0.0055549
v  CourantNb                   0.03202          2210.9          42.503          1.3874
v  FourierNb                 3.836e-05           12009          78.069         0.10407
v  total_pressure            1.007e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14822        0.010771        0.045299


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.43027           12028          120.57          1.4914


 TIME FOR THE TIME STEP               79:        0.42606E+02

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


 INSTANT    0.800000000E+01   TIME STEP NUMBER              80
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.188605319E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29176E+02 0.14393E+02
   Friction velocity        uet   :  0.12810E-03 0.26174E+01
   Friction velocity        uk    :  0.15782E-01 0.28411E+01
   Dimensionless distance   yplus :  0.10411E+00 0.29730E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1004
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29360E+04    1550   0.49760E-02   0.35181E+00 
c  VelocityY    0.29360E+04    1550   0.49760E-02   0.00000E+00 
c  VelocityZ    0.29360E+04    1550   0.49760E-02   0.00000E+00 
c  Pressure     0.38390E+00    7009   0.35399E-01   0.17453E+00 
c  k            0.69385E+03    1491   0.18253E-03   0.48755E+00 
c  omega        0.15577E+08     258   0.16487E-03   0.21378E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4614e-05                             1
a  omega          
a  Local Time Step      1.2776e-05                         45472


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.26358          0.2622      0.00063797      6.2315e-08
v  Velocity[Y]                 -25.874          31.047           6.222          20.054
v  Velocity[Z]                 -27.502          27.662        0.099452       -0.012646
v  ǁVelocityǁ                0.0093521          32.253          10.206          20.327
v  Pressure                    -618.63          358.64         -18.875          34.949
v  k                        3.5025e-08          42.675          3.4228         0.10131
v  omega                      0.011588      6.5166e+07          8958.3           15.03
v  turbulent_viscosity      8.5788e-15         0.14318       0.0074996       0.0056807
v  CourantNb                  0.032333          1982.6          42.192          1.3872
v  FourierNb                4.1947e-05           12229          77.689         0.10509
v  total_pressure           1.0071e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14796         0.01077         0.04527


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.24924           12252          119.88          1.4922


 TIME FOR THE TIME STEP               80:        0.43607E+02

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


 INSTANT    0.810000000E+01   TIME STEP NUMBER              81
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.141497383E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27194E+02 0.15059E+02
   Friction velocity        uet   :  0.13201E-02 0.26379E+01
   Friction velocity        uk    :  0.19831E-01 0.28144E+01
   Dimensionless distance   yplus :  0.12962E+00 0.29662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        527
   Nb of faces within the viscous sub-layer     :       1059
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29363E+04    1563   0.51669E-02   0.36562E+00 
c  VelocityY    0.29363E+04    1563   0.51669E-02   0.00000E+00 
c  VelocityZ    0.29363E+04    1563   0.51669E-02   0.00000E+00 
c  Pressure     0.40222E+00    6948   0.31542E-01   0.18380E+00 
c  k            0.70259E+03    1360   0.18079E-03   0.50929E+00 
c  omega        0.30892E+08     236   0.34498E-04   0.11196E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2484e-05                         45477


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25193         0.25854      0.00097703      4.2892e-07
v  Velocity[Y]                 -26.108          30.955          6.2616          20.054
v  Velocity[Z]                 -27.461          27.704        0.054304        -0.01234
v  ǁVelocityǁ                 0.011164           32.16          10.194          20.328
v  Pressure                    -612.75          359.02         -19.178            34.2
v  k                        6.2993e-08          45.858          3.4057         0.10572
v  omega                     0.0074815      3.2701e+07          9030.6          14.921
v  turbulent_viscosity      6.9723e-14         0.14782       0.0075914       0.0058169
v  CourantNb                  0.011854          2014.3          41.881          1.3869
v  FourierNb                 4.643e-05           12411          78.256         0.10632
v  total_pressure           1.0071e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14865         0.01077        0.045291


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.34216           12438          120.14          1.4932


 TIME FOR THE TIME STEP               81:        0.43392E+02

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


 INSTANT    0.820000000E+01   TIME STEP NUMBER              82
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.595388061E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29304E+02 0.14311E+02
   Friction velocity        uet   :  0.14705E-02 0.25466E+01
   Friction velocity        uk    :  0.18212E-01 0.30653E+01
   Dimensionless distance   yplus :  0.64865E-01 0.38527E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        486
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29366E+04    1545   0.51128E-02   0.38623E+00 
c  VelocityY    0.29366E+04    1545   0.51128E-02   0.00000E+00 
c  VelocityZ    0.29366E+04    1545   0.51128E-02   0.00000E+00 
c  Pressure     0.43792E+00    6875   0.29817E-01   0.19980E+00 
c  k            0.71100E+03    1289   0.18173E-03   0.48644E+00 
c  omega        0.13346E+08     269   0.50062E-04   0.42003E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -30780                             2
a  Local Time Step      1.2149e-05                         45524


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.2314          0.2457       0.0013444      4.0862e-07
v  Velocity[Y]                 -26.431          30.917          6.2778          20.054
v  Velocity[Z]                  -28.06           27.62       0.0076857       -0.011585
v  ǁVelocityǁ                0.0069834           32.04          10.186          20.329
v  Pressure                    -604.71          358.92         -18.873          33.367
v  k                        7.3438e-09          57.615           3.361         0.11052
v  omega                     0.0046002      1.6642e+07          8596.6          14.773
v  turbulent_viscosity       5.054e-14         0.15395       0.0076667       0.0059648
v  CourantNb                  0.031339          2040.2           41.86          1.3868
v  FourierNb                   5.2e-05           12603          77.803         0.10716
v  total_pressure           1.0072e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14886        0.010769        0.045297


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.47116           12635          119.66          1.4939


 TIME FOR THE TIME STEP               82:        0.41592E+02

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


 INSTANT    0.830000000E+01   TIME STEP NUMBER              83
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.357680523E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28316E+02 0.17626E+02
   Friction velocity        uet   :  0.22645E-03 0.25082E+01
   Friction velocity        uk    :  0.20067E-01 0.30009E+01
   Dimensionless distance   yplus :  0.11368E+00 0.31186E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29368E+04    1573   0.52173E-02   0.40837E+00 
c  VelocityY    0.29368E+04    1573   0.52173E-02   0.00000E+00 
c  VelocityZ    0.29368E+04    1573   0.52173E-02   0.00000E+00 
c  Pressure     0.44294E+00    6957   0.28938E-01   0.20385E+00 
c  k            0.71898E+03    1556   0.15323E-03   0.48685E+00 
c  omega        0.10462E+08     316   0.69935E-04   0.35643E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2814e-05                         45521


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20588         0.24022       0.0016928      7.6956e-07
v  Velocity[Y]                 -26.683          35.221          6.2952          20.054
v  Velocity[Z]                 -28.829           27.15       -0.022617       -0.010378
v  ǁVelocityǁ                  0.01185          35.496          10.167           20.33
v  Pressure                    -594.81          358.98         -17.633          33.127
v  k                        5.3761e-09          76.842          3.3248         0.11578
v  omega                     0.0028145      2.2282e+07          8412.7          14.685
v  turbulent_viscosity      4.8015e-15         0.16116       0.0077321       0.0061258
v  CourantNb                  0.013572          2073.6          41.947          1.3867
v  FourierNb                5.5846e-05           12734          76.998         0.10782
v  total_pressure           1.0073e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010769        0.045274


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.648           12770          118.94          1.4946


 TIME FOR THE TIME STEP               83:        0.42646E+02

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


 INSTANT    0.840000000E+01   TIME STEP NUMBER              84
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.197418478E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28881E+02 0.22990E+02
   Friction velocity        uet   :  0.35936E-03 0.32517E+01
   Friction velocity        uk    :  0.19814E-01 0.28527E+01
   Dimensionless distance   yplus :  0.17444E+00 0.27183E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        511
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    1621   0.53060E-02   0.43114E+00 
c  VelocityY    0.29372E+04    1621   0.53060E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    1621   0.53060E-02   0.00000E+00 
c  Pressure     0.42287E+00    6985   0.29375E-01   0.19424E+00 
c  k            0.72832E+03    1707   0.14077E-03   0.53566E+00 
c  omega        0.10857E+08     313   0.72276E-03   0.10548E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -72633                             1
a  Local Time Step      1.2955e-05                         45539


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.18031         0.23009        0.002027      9.8164e-07
v  Velocity[Y]                 -26.812          32.656          6.3309          20.054
v  Velocity[Z]                 -29.317          27.113       -0.054082      -0.0096854
v  ǁVelocityǁ                 0.014799          33.455          10.148           20.33
v  Pressure                    -583.46          359.07         -15.699          32.867
v  k                        1.9545e-08          82.215          3.3145         0.12154
v  omega                     0.0017305      2.7694e+08            9097          14.616
v  turbulent_viscosity      1.1376e-14         0.16644       0.0078199       0.0063025
v  CourantNb                  0.016937          2110.2          42.018          1.3867
v  FourierNb                5.6381e-05           12716          76.858         0.10907
v  total_pressure           1.0074e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14688        0.010769        0.045231


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.58207           12755          118.88          1.4958


 TIME FOR THE TIME STEP               84:        0.44682E+02

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


 INSTANT    0.850000000E+01   TIME STEP NUMBER              85
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.401203789E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28269E+02 0.19946E+02
   Friction velocity        uet   :  0.12533E-02 0.30845E+01
   Friction velocity        uk    :  0.18935E-01 0.28648E+01
   Dimensionless distance   yplus :  0.13457E+00 0.29775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :        994
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29374E+04    1619   0.51022E-02   0.44243E+00 
c  VelocityY    0.29374E+04    1619   0.51022E-02   0.00000E+00 
c  VelocityZ    0.29374E+04    1619   0.51022E-02   0.00000E+00 
c  Pressure     0.42796E+00    6985   0.32341E-01   0.19707E+00 
c  k            0.74116E+03    1747   0.15606E-03   0.63157E+00 
c  omega        0.29806E+09     132   0.96096E-05   0.32667E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -98607                             2
a  Local Time Step      1.3094e-05                         45517


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17186         0.24694       0.0022358      1.3663e-06
v  Velocity[Y]                  -26.93          30.816          6.3793          20.054
v  Velocity[Z]                 -29.953          26.771       -0.068374      -0.0085379
v  ǁVelocityǁ                 0.010286          33.807          10.162          20.331
v  Pressure                    -576.14          359.71         -13.615          32.746
v  k                        4.0399e-09          58.155          3.3116          0.1278
v  omega                     0.0011029      1.3864e+08          8898.9          14.561
v  turbulent_viscosity      5.7268e-14         0.17133       0.0079414       0.0064965
v  CourantNb                  0.018687          2139.5          41.915          1.3865
v  FourierNb                5.7057e-05           12467          76.655          0.1107
v  total_pressure           1.0075e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14776        0.010769         0.04522


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.38539           12506          118.57          1.4972


 TIME FOR THE TIME STEP               85:        0.43176E+02

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


 INSTANT    0.860000000E+01   TIME STEP NUMBER              86
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.351032192E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29286E+02 0.16397E+02
   Friction velocity        uet   :  0.17104E-02 0.29651E+01
   Friction velocity        uk    :  0.14970E-01 0.31207E+01
   Dimensionless distance   yplus :  0.16740E+00 0.34943E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1488   0.50578E-02   0.45759E+00 
c  VelocityY    0.29376E+04    1488   0.50578E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1488   0.50578E-02   0.00000E+00 
c  Pressure     0.44350E+00    7058   0.35304E-01   0.20389E+00 
c  k            0.76084E+03    1577   0.16557E-03   0.72731E+00 
c  omega        0.76131E+08     104   0.28581E-04   0.18521E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.716e+05                             1
a  Local Time Step      1.2618e-05                         45540


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.18963         0.26401       0.0023067      2.0845e-06
v  Velocity[Y]                 -26.967          30.887          6.4277          20.055
v  Velocity[Z]                 -30.617          26.921       -0.058261      -0.0074045
v  ǁVelocityǁ                 0.021935          33.052          10.213          20.333
v  Pressure                    -569.52           360.7         -11.819          32.614
v  k                        2.0114e-09          48.026          3.3001         0.13452
v  omega                    0.00072516      7.6067e+07          8737.9          14.444
v  turbulent_viscosity      1.7126e-14         0.17542       0.0080503       0.0067103
v  CourantNb                  0.048156          2234.7          41.864          1.3862
v  FourierNb                5.7903e-05           11844          75.648         0.11194
v  total_pressure           1.0076e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01           0.149        0.010769        0.045237


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40743           11885          117.51          1.4981


 TIME FOR THE TIME STEP               86:        0.42341E+02

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


 INSTANT    0.870000000E+01   TIME STEP NUMBER              87
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.598141183E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31351E+02 0.15489E+02
   Friction velocity        uet   :  0.78397E-03 0.28820E+01
   Friction velocity        uk    :  0.28366E-01 0.28070E+01
   Dimensionless distance   yplus :  0.14473E+00 0.32301E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1337   0.50851E-02   0.46425E+00 
c  VelocityY    0.29379E+04    1337   0.50851E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1337   0.50851E-02   0.00000E+00 
c  Pressure     0.44204E+00    7073   0.35788E-01   0.20207E+00 
c  k            0.78525E+03    1250   0.16825E-03   0.76347E+00 
c  omega        0.33607E+08     150   0.33165E-04   0.10913E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.4986e-06                             1
a  omega          
a  Local Time Step      1.2694e-05                         45549


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20336         0.27614       0.0021939      2.3394e-06
v  Velocity[Y]                 -26.946           30.94          6.4618          20.054
v  Velocity[Z]                 -29.258          27.066       -0.019097      -0.0057925
v  ǁVelocityǁ                  0.02217           31.44          10.252          20.333
v  Pressure                    -571.63          362.38          -10.67          32.477
v  k                        3.2701e-08          46.186          3.3076         0.14171
v  omega                    0.00048031      3.8818e+07          8602.3          14.381
v  turbulent_viscosity      2.1423e-15         0.17884       0.0081597       0.0069462
v  CourantNb                  0.031289          2328.3          42.097           1.386
v  FourierNb                5.8962e-05           11303          75.254         0.11354
v  total_pressure           1.0075e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14796         0.01077        0.045247


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.44214           11344          117.35          1.4996


 TIME FOR THE TIME STEP               87:        0.40627E+02

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


 INSTANT    0.880000000E+01   TIME STEP NUMBER              88
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.522746259E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30086E+02 0.14646E+02
   Friction velocity        uet   :  0.87264E-03 0.26611E+01
   Friction velocity        uk    :  0.20821E-01 0.28008E+01
   Dimensionless distance   yplus :  0.99902E-01 0.34299E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1235   0.50029E-02   0.44731E+00 
c  VelocityY    0.29382E+04    1235   0.50029E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1235   0.50029E-02   0.00000E+00 
c  Pressure     0.39187E+00    6959   0.33826E-01   0.17939E+00 
c  k            0.80705E+03    1183   0.16227E-03   0.78665E+00 
c  omega        0.17470E+08     173   0.37554E-04   0.61763E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.6866e-05                             1
a  omega          
a  Local Time Step      1.3227e-05                         45659


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21131         0.28687       0.0019322      2.2026e-06
v  Velocity[Y]                 -26.728          30.967          6.4465          20.054
v  Velocity[Z]                 -29.623          27.288        0.027244      -0.0042003
v  ǁVelocityǁ                 0.010658           31.01          10.249          20.333
v  Pressure                    -582.38          364.19         -10.511          32.473
v  k                        4.4111e-09          37.904          3.3274          0.1494
v  omega                    0.00032129      2.0992e+07          8532.8          14.306
v  turbulent_viscosity       1.994e-15         0.18051       0.0082523       0.0072059
v  CourantNb                  0.063085          2241.1          42.354           1.386
v  FourierNb                6.0282e-05           11173          75.134         0.11526
v  total_pressure           1.0074e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.15921         0.01077        0.045266


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52991           11216          117.49          1.5012


 TIME FOR THE TIME STEP               88:        0.38128E+02

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


 INSTANT    0.890000000E+01   TIME STEP NUMBER              89
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.146713642E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30498E+02 0.14432E+02
   Friction velocity        uet   :  0.18904E-02 0.25567E+01
   Friction velocity        uk    :  0.11036E-01 0.29807E+01
   Dimensionless distance   yplus :  0.98027E-01 0.32809E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :       1023
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    1252   0.49794E-02   0.42160E+00 
c  VelocityY    0.29385E+04    1252   0.49794E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    1252   0.49794E-02   0.00000E+00 
c  Pressure     0.43245E+00    6985   0.31530E-01   0.19792E+00 
c  k            0.82237E+03    1366   0.18078E-03   0.81567E+00 
c  omega        0.11390E+08     223   0.15028E-03   0.14910E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.5128e-05                             1
a  omega          
a  Local Time Step       1.258e-05                         45699


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21374         0.29468       0.0014525      2.0446e-06
v  Velocity[Y]                 -29.898          30.974          6.3781          20.054
v  Velocity[Z]                 -28.136          27.316        0.068745      -0.0021987
v  ǁVelocityǁ                0.0088936          31.878           10.26          20.334
v  Pressure                    -592.15          365.85         -11.514          32.316
v  k                        1.7516e-11          64.275          3.3911         0.15765
v  omega                    0.00021962      6.0405e+07          8720.4          14.247
v  turbulent_viscosity      3.3333e-15         0.18097       0.0083457       0.0074928
v  CourantNb                  0.014992          2071.4          42.354           1.386
v  FourierNb                6.1946e-05           11327          76.116         0.11751
v  total_pressure           1.0073e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.16134         0.01077        0.045276


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.64066           11371          118.47          1.5035


 TIME FOR THE TIME STEP               89:        0.38740E+02

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


 INSTANT    0.900000000E+01   TIME STEP NUMBER              90
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.665319995E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29041E+02 0.20095E+02
   Friction velocity        uet   :  0.80316E-03 0.25771E+01
   Friction velocity        uk    :  0.80441E-02 0.30078E+01
   Dimensionless distance   yplus :  0.11249E+00 0.26877E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        531
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1309   0.48780E-02   0.40192E+00 
c  VelocityY    0.29390E+04    1309   0.48780E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1309   0.48780E-02   0.00000E+00 
c  Pressure     0.41070E+00    6948   0.32466E-01   0.18730E+00 
c  k            0.82317E+03    1442   0.23146E-03   0.79629E+00 
c  omega        0.28332E+08     252   0.32893E-04   0.49691E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5674e+05                             1
a  Local Time Step      1.3332e-05                         45743


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.21166         0.30285      0.00085884      1.3023e-06
v  Velocity[Y]                  -34.73          30.988          6.3126          20.053
v  Velocity[Z]                 -27.375          27.387        0.099485     -0.00021268
v  ǁVelocityǁ                 0.012052          37.996          10.294          20.335
v  Pressure                     -600.4          366.99         -13.554          32.087
v  k                        6.1176e-11          95.977          3.4765         0.16656
v  omega                    0.00014626      3.1172e+07          8592.2          14.179
v  turbulent_viscosity      1.2288e-17         0.17919       0.0084497       0.0078095
v  CourantNb                   0.12646          2017.9          42.466          1.3861
v  FourierNb                6.4032e-05           11543          77.967         0.12041
v  total_pressure           1.0072e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1583         0.01077        0.045247


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78984           11586          120.43          1.5065


 TIME FOR THE TIME STEP               90:        0.38995E+02

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


 INSTANT    0.910000000E+01   TIME STEP NUMBER              91
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.351713689E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53116E+02 0.14848E+02
   Friction velocity        uet   :  0.72386E-03 0.33401E+01
   Friction velocity        uk    :  0.12018E-01 0.41214E+01
   Dimensionless distance   yplus :  0.16724E+00 0.37295E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        538
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1490   0.49918E-02   0.38983E+00 
c  VelocityY    0.29393E+04    1490   0.49918E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1490   0.49918E-02   0.00000E+00 
c  Pressure     0.38097E+00    7076   0.37655E-01   0.17243E+00 
c  k            0.81424E+03    1463   0.29733E-03   0.74176E+00 
c  omega        0.12346E+08     463   0.54167E-04   0.36664E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3411e-05                         45735


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25865          0.3188      0.00022669      1.0621e-06
v  Velocity[Y]                  -30.73          31.038          6.2916          20.054
v  Velocity[Z]                 -27.471          28.423         0.11668       0.0019234
v  ǁVelocityǁ                0.0070498           32.14          10.297          20.336
v  Pressure                    -608.39          368.17         -15.921          32.151
v  k                        1.4449e-08          60.988          3.4957         0.17621
v  omega                    9.2118e-05      2.3634e+07          8686.7          14.142
v  turbulent_viscosity       2.578e-17         0.17669       0.0085496       0.0081583
v  CourantNb                 0.0061923          1999.6          42.686          1.3863
v  FourierNb                6.6636e-05           11776          79.554         0.12348
v  total_pressure           1.0072e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.17043        0.010772        0.045277


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74061           11817          122.24          1.5098


 TIME FOR THE TIME STEP               91:        0.42943E+02

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


 INSTANT    0.920000000E+01   TIME STEP NUMBER              92
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.373131248E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26660E+02 0.14340E+02
   Friction velocity        uet   :  0.88786E-04 0.30211E+01
   Friction velocity        uk    :  0.86394E-02 0.29613E+01
   Dimensionless distance   yplus :  0.78008E-01 0.26649E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1438   0.49761E-02   0.38954E+00 
c  VelocityY    0.29397E+04    1438   0.49761E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1438   0.49761E-02   0.00000E+00 
c  Pressure     0.38987E+00    7088   0.41760E-01   0.17674E+00 
c  k            0.80598E+03    1393   0.19293E-03   0.68125E+00 
c  omega        0.10646E+08     357   0.91381E-04   0.48551E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3442e-05                         45626


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.23126         0.32923     -0.00031012      3.4141e-08
v  Velocity[Y]                 -26.343           31.03          6.2909          20.053
v  Velocity[Z]                 -27.617          26.984         0.10279       0.0040472
v  ǁVelocityǁ                 0.010276          32.445          10.262          20.337
v  Pressure                    -614.88          369.33          -17.42          32.354
v  k                        4.2649e-08          46.724          3.4977         0.18657
v  omega                    5.6739e-05      3.4891e+07          8652.1          14.062
v  turbulent_viscosity       7.673e-15         0.17367       0.0086259       0.0085426
v  CourantNb                   0.02235          2998.5          43.016          1.3866
v  FourierNb                6.9879e-05           11892          79.681         0.12583
v  total_pressure           1.0071e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.18748        0.010773        0.045292


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.63693           11931           122.7          1.5124


 TIME FOR THE TIME STEP               92:        0.42149E+02

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


 INSTANT    0.930000000E+01   TIME STEP NUMBER              93
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.411721573E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27729E+02 0.13085E+02
   Friction velocity        uet   :  0.27498E-02 0.26193E+01
   Friction velocity        uk    :  0.26146E-01 0.28521E+01
   Dimensionless distance   yplus :  0.12159E+00 0.25888E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        566
   Nb of faces within the viscous sub-layer     :       1049
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1513   0.48266E-02   0.39990E+00 
c  VelocityY    0.29401E+04    1513   0.48266E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1513   0.48266E-02   0.00000E+00 
c  Pressure     0.42218E+00    7040   0.40190E-01   0.19299E+00 
c  k            0.80093E+03    1228   0.15488E-03   0.62010E+00 
c  omega        0.11787E+08     289   0.68034E-04   0.12405E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2716e-05                         45617


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.25737          0.3328     -0.00072892     -9.8171e-07
v  Velocity[Y]                 -26.106          31.061          6.3022          20.054
v  Velocity[Z]                 -27.684          26.764        0.058552       0.0062939
v  ǁVelocityǁ                 0.013984          32.656          10.211          20.339
v  Pressure                    -619.83          369.93         -17.554            32.5
v  k                        3.8393e-11          72.077          3.5169         0.19762
v  omega                    3.4703e-05      4.0449e+07          8670.4          14.004
v  turbulent_viscosity      3.2509e-14          0.1751       0.0087015       0.0089637
v  CourantNb                  0.041895          2303.1          43.012          1.3866
v  FourierNb                  7.39e-05           12100          80.594         0.12814
v  total_pressure           1.0071e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.20622        0.010772          0.0453


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.72142           12133          123.61          1.5148


 TIME FOR THE TIME STEP               93:        0.42331E+02

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


 INSTANT    0.940000000E+01   TIME STEP NUMBER              94
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.400789521E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27532E+02 0.12266E+02
   Friction velocity        uet   :  0.74349E-03 0.26821E+01
   Friction velocity        uk    :  0.17377E-01 0.28570E+01
   Dimensionless distance   yplus :  0.10791E+00 0.27336E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        555
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1509   0.49253E-02   0.40830E+00 
c  VelocityY    0.29406E+04    1509   0.49253E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1509   0.49253E-02   0.00000E+00 
c  Pressure     0.42065E+00    6947   0.34470E-01   0.19144E+00 
c  k            0.79761E+03    1221   0.18353E-03   0.72052E+00 
c  omega        0.24329E+08     330   0.19517E-04   0.37781E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2594e-05                         45586


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.32678          0.3309      -0.0009696     -2.6954e-06
v  Velocity[Y]                   -25.9          31.129          6.3114          20.054
v  Velocity[Z]                 -27.665          26.623      -0.0082888       0.0088396
v  ǁVelocityǁ                0.0072213          32.427          10.158           20.34
v  Pressure                    -624.21          368.77         -17.352          32.221
v  k                        1.6282e-08           96.29          3.5096         0.20932
v  omega                    2.0441e-05      2.0233e+07          8361.2          13.892
v  turbulent_viscosity      1.4668e-16         0.18839       0.0087946       0.0094216
v  CourantNb                 0.0074671          2036.5           42.78          1.3867
v  FourierNb                7.8899e-05           12295          83.017         0.13111
v  total_pressure            1.007e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1873        0.010772        0.045315


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7109           12330           125.8          1.5178


 TIME FOR THE TIME STEP               94:        0.40395E+02

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


 INSTANT    0.950000000E+01   TIME STEP NUMBER              95
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.141997265E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27749E+02 0.13135E+02
   Friction velocity        uet   :  0.10470E-02 0.26513E+01
   Friction velocity        uk    :  0.28995E-01 0.30599E+01
   Dimensionless distance   yplus :  0.14583E+00 0.31119E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        608
   Nb of faces within the viscous sub-layer     :       1060
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1448   0.48951E-02   0.41655E+00 
c  VelocityY    0.29410E+04    1448   0.48951E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1448   0.48951E-02   0.00000E+00 
c  Pressure     0.40178E+00    7000   0.30715E-01   0.18284E+00 
c  k            0.79303E+03    1440   0.15557E-03   0.70473E+00 
c  omega        0.11789E+08     371   0.57213E-04   0.51650E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.782e+05                             1
a  Local Time Step       1.328e-05                         45594


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39516          0.3212     -0.00097229      -2.751e-06
v  Velocity[Y]                 -25.686          31.199          6.3065          20.054
v  Velocity[Z]                 -27.517          26.499       -0.082376        0.011662
v  ǁVelocityǁ                0.0094261          32.127          10.139          20.341
v  Pressure                    -628.01          366.63         -17.039          31.707
v  k                        5.4189e-10          105.03          3.4688         0.22172
v  omega                    1.1738e-05      1.5937e+07          8788.6          13.881
v  turbulent_viscosity      2.2836e-14         0.20044       0.0088763       0.0099165
v  CourantNb                   0.02117          2083.8           42.71          1.3869
v  FourierNb                8.5073e-05           12359          84.468         0.13395
v  total_pressure            1.007e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.16632        0.010772        0.045315


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82699           12398          127.18          1.5209


 TIME FOR THE TIME STEP               95:        0.42487E+02

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


 INSTANT    0.960000000E+01   TIME STEP NUMBER              96
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.353386960E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27563E+02 0.20595E+02
   Friction velocity        uet   :  0.59027E-03 0.26122E+01
   Friction velocity        uk    :  0.92808E-02 0.29465E+01
   Dimensionless distance   yplus :  0.81711E-01 0.37035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        585
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1428   0.49131E-02   0.42204E+00 
c  VelocityY    0.29414E+04    1428   0.49131E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1428   0.49131E-02   0.00000E+00 
c  Pressure     0.37975E+00    6948   0.27933E-01   0.17236E+00 
c  k            0.78865E+03    1498   0.13565E-03   0.70006E+00 
c  omega        0.15997E+08     287   0.73987E-03   0.10431E+12 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.9464e-06                             2
a  omega          
a  Local Time Step      1.3549e-05                         45608


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.46164         0.30306       -0.000819     -1.5994e-06
v  Velocity[Y]                  -25.41          31.293          6.3028          20.054
v  Velocity[Z]                  -27.41          26.598        -0.14477        0.014328
v  ǁVelocityǁ                0.0080784          31.681          10.117          20.341
v  Pressure                    -632.29          364.56         -16.205          31.389
v  k                        6.6639e-09          102.67          3.4266         0.23482
v  omega                    6.8382e-06      1.6238e+09           13068          14.493
v  turbulent_viscosity      2.8636e-16          0.2124       0.0089397        0.010449
v  CourantNb                  0.020399          2150.1          42.822          1.3872
v  FourierNb                9.2677e-05           12275          83.426         0.13625
v  total_pressure           1.0069e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.18295        0.010771        0.045323


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82967           12319          126.25          1.5235


 TIME FOR THE TIME STEP               96:        0.41256E+02

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


 INSTANT    0.970000000E+01   TIME STEP NUMBER              97
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.147901614E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28006E+02 0.19089E+02
   Friction velocity        uet   :  0.12539E-02 0.26133E+01
   Friction velocity        uk    :  0.21927E-01 0.31242E+01
   Dimensionless distance   yplus :  0.83282E-01 0.35898E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1450   0.49927E-02   0.43803E+00 
c  VelocityY    0.29419E+04    1450   0.49927E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1450   0.49927E-02   0.00000E+00 
c  Pressure     0.39390E+00    6925   0.25986E-01   0.17892E+00 
c  k            0.78695E+03    1388   0.13810E-03   0.78112E+00 
c  omega        0.31177E+11      12   0.17129E-06   0.26139E+11 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012486                             2
a  omega                   -920.75                             1
a  Local Time Step      1.3338e-05                         45570


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.51254         0.28403     -0.00058145     -4.3218e-07
v  Velocity[Y]                  -25.16          31.446          6.3356          20.053
v  Velocity[Z]                 -27.343          26.773        -0.19237        0.016868
v  ǁVelocityǁ                 0.018963            32.2          10.115          20.342
v  Pressure                    -636.78          363.38          -14.48          31.355
v  k                         2.073e-08           84.96          3.3879         0.24867
v  omega                    4.0807e-06      8.1191e+08           10756          14.097
v  turbulent_viscosity      2.8864e-15         0.22646        0.008996        0.011018
v  CourantNb                  0.036126          2219.4          42.681          1.3873
v  FourierNb                0.00010198           12051          82.376         0.13847
v  total_pressure           1.0069e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.17918        0.010772        0.045327


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97244           12100          125.06          1.5258


 TIME FOR THE TIME STEP               97:        0.40293E+02

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


 INSTANT    0.980000000E+01   TIME STEP NUMBER              98
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.512087797E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28649E+02 0.18105E+02
   Friction velocity        uet   :  0.50267E-03 0.27056E+01
   Friction velocity        uk    :  0.24026E-01 0.32643E+01
   Dimensionless distance   yplus :  0.11322E+00 0.37507E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        552
   Nb of faces within the viscous sub-layer     :       1079
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1396   0.51516E-02   0.44678E+00 
c  VelocityY    0.29426E+04    1396   0.51516E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1396   0.51516E-02   0.00000E+00 
c  Pressure     0.41170E+00    6910   0.27199E-01   0.18708E+00 
c  k            0.79072E+03    1035   0.14689E-03   0.92289E+00 
c  omega        0.77941E+10      28   0.33961E-06   0.65618E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2729e-05                         45559


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.54581         0.25049     -0.00029614      8.5331e-07
v  Velocity[Y]                  -24.92          31.568          6.3837          20.054
v  Velocity[Z]                  -28.67          27.217         -0.2311        0.019561
v  ǁVelocityǁ                  0.01564          33.654          10.138          20.343
v  Pressure                    -640.26          363.11          -12.13          31.615
v  k                        5.5275e-09          51.245          3.3795         0.26334
v  omega                     2.508e-06      4.0595e+08          9661.7          13.864
v  turbulent_viscosity      7.1035e-15         0.23842       0.0090782        0.011624
v  CourantNb                  0.024756          2287.4          42.536          1.3872
v  FourierNb                0.00011331           11779          81.133         0.14095
v  total_pressure           1.0068e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.15999         0.01077        0.045286


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0001           11820          123.67          1.5282


 TIME FOR THE TIME STEP               98:        0.38986E+02

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


 INSTANT    0.990000000E+01   TIME STEP NUMBER              99
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.554624865E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28606E+02 0.14166E+02
   Friction velocity        uet   :  0.12824E-02 0.28452E+01
   Friction velocity        uk    :  0.17849E-01 0.31041E+01
   Dimensionless distance   yplus :  0.12718E+00 0.34049E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        559
   Nb of faces within the viscous sub-layer     :       1104
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29433E+04    1314   0.49650E-02   0.45485E+00 
c  VelocityY    0.29433E+04    1314   0.49650E-02   0.00000E+00 
c  VelocityZ    0.29433E+04    1314   0.49650E-02   0.00000E+00 
c  Pressure     0.37428E+00    6963   0.31563E-01   0.17091E+00 
c  k            0.80546E+03    1362   0.15555E-03   0.10508E+01 
c  omega        0.19484E+10      61   0.12123E-05   0.17512E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9419e+05                             1
a  Local Time Step      1.2953e-05                         45529


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.56014         0.23431     -1.4887e-05      3.9477e-07
v  Velocity[Y]                 -24.693          31.699          6.4362          20.054
v  Velocity[Z]                 -29.519          27.395        -0.23865        0.022333
v  ǁVelocityǁ                0.0099865          33.385          10.201          20.344
v  Pressure                    -645.28          362.36         -10.741          31.624
v  k                        3.7975e-07          57.698          3.3886         0.27874
v  omega                    1.5685e-06      2.0297e+08          9395.4          13.712
v  turbulent_viscosity      2.0327e-14         0.24921       0.0091987        0.012266
v  CourantNb                  0.025411          2335.9          42.269          1.3868
v  FourierNb                 0.0001271           11774          80.082         0.14404
v  total_pressure           1.0068e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010771        0.045289


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96498           11812          122.35          1.5309


 TIME FOR THE TIME STEP               99:        0.39577E+02

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


 INSTANT    0.100000000E+02   TIME STEP NUMBER             100
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.110603114E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28745E+02 0.13419E+02
   Friction velocity        uet   :  0.20661E-03 0.27983E+01
   Friction velocity        uk    :  0.20145E-01 0.31084E+01
   Dimensionless distance   yplus :  0.83101E-01 0.29976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        572
   Nb of faces within the viscous sub-layer     :       1063
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29441E+04    1313   0.49578E-02   0.46913E+00 
c  VelocityY    0.29441E+04    1313   0.49578E-02   0.00000E+00 
c  VelocityZ    0.29441E+04    1313   0.49578E-02   0.00000E+00 
c  Pressure     0.36201E+00    6963   0.35641E-01   0.16550E+00 
c  k            0.83149E+03    1462   0.15196E-03   0.11588E+01 
c  omega        0.48747E+09      61   0.28942E-05   0.46996E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3124e-05                         45505


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.5439         0.24451      0.00017699     -1.7755e-06
v  Velocity[Y]                 -24.529          31.816          6.4829          20.054
v  Velocity[Z]                 -30.054          27.632        -0.20831        0.025216
v  ǁVelocityǁ                0.0076665          31.855          10.266          20.345
v  Pressure                    -649.68          361.38          -10.13          31.674
v  k                        9.2261e-08          58.208          3.4009         0.29479
v  omega                    9.8958e-07      1.0148e+08          8851.8          13.575
v  turbulent_viscosity      8.2933e-14         0.26259       0.0093345        0.012943
v  CourantNb                  0.025246          2354.4          42.247          1.3866
v  FourierNb                 0.0001438           11989          80.239         0.14766
v  total_pressure           1.0068e+05      1.0169e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14883        0.010771        0.045277


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.975           12023          122.49          1.5343


 TIME FOR THE TIME STEP              100:        0.40781E+02

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


 INSTANT    0.101000000E+02   TIME STEP NUMBER             101
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.188967790E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27805E+02 0.12604E+02
   Friction velocity        uet   :  0.81695E-03 0.27346E+01
   Friction velocity        uk    :  0.17915E-01 0.27752E+01
   Dimensionless distance   yplus :  0.11727E+00 0.27564E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        575
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29450E+04    1332   0.49813E-02   0.46486E+00 
c  VelocityY    0.29450E+04    1332   0.49813E-02   0.00000E+00 
c  VelocityZ    0.29450E+04    1332   0.49813E-02   0.00000E+00 
c  Pressure     0.37854E+00    6863   0.35753E-01   0.17291E+00 
c  k            0.86213E+03    1508   0.14761E-03   0.12577E+01 
c  omega        0.12237E+09     117   0.62215E-05   0.12307E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00090075                             1
a  omega          
a  Local Time Step      1.3091e-05                         45531


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.51277         0.25727      0.00020703     -3.1052e-06
v  Velocity[Y]                 -24.411          31.958          6.4911          20.053
v  Velocity[Z]                 -29.186          27.604        -0.16699        0.027782
v  ǁVelocityǁ                0.0069257          32.006           10.29          20.345
v  Pressure                    -654.01          360.44         -9.9372          31.626
v  k                        7.8332e-09          50.933          3.4051         0.31145
v  omega                    6.2096e-07      5.0736e+07          8383.6          13.463
v  turbulent_viscosity      9.3083e-15         0.27459       0.0094822        0.013653
v  CourantNb                  0.014531          2349.1          42.383          1.3866
v  FourierNb                0.00016388           12305          81.428         0.15178
v  total_pressure           1.0067e+05      1.0169e+05      1.0132e+05      1.0136e+05
v  Local Time Step                0.01          0.1473        0.010771        0.045243


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98716           12337          123.81          1.5384


 TIME FOR THE TIME STEP              101:        0.39327E+02

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


 INSTANT    0.102000000E+02   TIME STEP NUMBER             102
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.372575912E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25660E+02 0.12077E+02
   Friction velocity        uet   :  0.33390E-02 0.25580E+01
   Friction velocity        uk    :  0.23191E-01 0.28610E+01
   Dimensionless distance   yplus :  0.10778E+00 0.27539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29460E+04    1331   0.50241E-02   0.44618E+00 
c  VelocityY    0.29460E+04    1331   0.50241E-02   0.00000E+00 
c  VelocityZ    0.29460E+04    1331   0.50241E-02   0.00000E+00 
c  Pressure     0.37800E+00    6880   0.33418E-01   0.17337E+00 
c  k            0.89087E+03    1533   0.15341E-03   0.13520E+01 
c  omega        0.32138E+08     157   0.16534E-04   0.53530E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -34068                             1
a  Local Time Step      1.2541e-05                         45511


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.46631         0.26706      0.00015827     -3.0141e-06
v  Velocity[Y]                 -24.294          32.035          6.4313          20.053
v  Velocity[Z]                 -28.103          27.564        -0.12765         0.03028
v  ǁVelocityǁ                0.0083514          32.082          10.269          20.346
v  Pressure                    -656.86          359.09         -10.318          31.469
v  k                        8.0602e-08          49.115          3.4157         0.32874
v  omega                    3.8475e-07      2.5363e+07          8313.5          13.413
v  turbulent_viscosity       3.847e-14         0.28739       0.0096012        0.014395
v  CourantNb                  0.034577          2311.7          42.391          1.3867
v  FourierNb                0.00018792           12523          82.298         0.15593
v  total_pressure           1.0067e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14804        0.010772        0.045226


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88111           12555          124.69          1.5426


 TIME FOR THE TIME STEP              102:        0.39443E+02

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


 INSTANT    0.103000000E+02   TIME STEP NUMBER             103
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.696400611E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25217E+02 0.16558E+02
   Friction velocity        uet   :  0.74013E-03 0.24329E+01
   Friction velocity        uk    :  0.17634E-01 0.30544E+01
   Dimensionless distance   yplus :  0.10518E+00 0.27690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        470
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29472E+04    1355   0.51513E-02   0.43705E+00 
c  VelocityY    0.29472E+04    1355   0.51513E-02   0.00000E+00 
c  VelocityZ    0.29472E+04    1355   0.51513E-02   0.00000E+00 
c  Pressure     0.38955E+00    6930   0.32518E-01   0.17842E+00 
c  k            0.90796E+03    1517   0.18867E-03   0.13946E+01 
c  omega        0.12817E+08     242   0.42245E-04   0.34263E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4389e+05                             1
a  Local Time Step      1.2947e-05                         45468


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.40889         0.27474      3.8299e-05      -2.809e-06
v  Velocity[Y]                 -24.166          32.111          6.3366          20.054
v  Velocity[Z]                 -26.338          27.436        -0.10433        0.032427
v  ǁVelocityǁ                0.0094486          32.196          10.283          20.347
v  Pressure                    -659.63          356.77         -11.605          31.284
v  k                        1.2784e-07          78.147          3.4551         0.34676
v  omega                    2.3492e-07      1.4036e+07          8231.4           13.35
v  turbulent_viscosity      1.7116e-14         0.30155        0.009699        0.015169
v  CourantNb                   0.04603          2259.4          42.099          1.3866
v  FourierNb                0.00021658           12636          83.366         0.16037
v  total_pressure           1.0067e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14903        0.010771        0.045213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0002           12670          125.46           1.547


 TIME FOR THE TIME STEP              103:        0.39977E+02

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


 INSTANT    0.104000000E+02   TIME STEP NUMBER             104
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.103700192E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26956E+02 0.15826E+02
   Friction velocity        uet   :  0.66451E-03 0.22352E+01
   Friction velocity        uk    :  0.26571E-01 0.28676E+01
   Dimensionless distance   yplus :  0.88528E-01 0.27701E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        511
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29484E+04    1595   0.51098E-02   0.44814E+00 
c  VelocityY    0.29484E+04    1595   0.51098E-02   0.00000E+00 
c  VelocityZ    0.29484E+04    1595   0.51098E-02   0.00000E+00 
c  Pressure     0.41660E+00    7015   0.33556E-01   0.19020E+00 
c  k            0.91190E+03    1415   0.22613E-03   0.14172E+01 
c  omega        0.14856E+08     366   0.22684E-04   0.36106E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -12330                             1
a  Local Time Step      1.3122e-05                         45455


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.33362         0.28404     -0.00017158     -2.6849e-06
v  Velocity[Y]                 -36.486          32.162           6.295          20.053
v  Velocity[Z]                 -26.734          27.212       -0.071896        0.034033
v  ǁVelocityǁ                 0.020239          37.167          10.295          20.347
v  Pressure                    -662.07          353.67         -13.821          31.112
v  k                        3.4739e-08           77.67          3.4939         0.36569
v  omega                    1.4119e-07      1.1836e+07          8224.2          13.341
v  turbulent_viscosity      3.1519e-14         0.31463       0.0097872        0.015975
v  CourantNb                  0.017406          2191.5          42.101          1.3867
v  FourierNb                 0.0002507           12650           83.53         0.16503
v  total_pressure           1.0066e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1494         0.01077        0.045199


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0003           12686          125.63          1.5517


 TIME FOR THE TIME STEP              104:        0.43129E+02

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


 INSTANT    0.105000000E+02   TIME STEP NUMBER             105
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.311571507E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46618E+02 0.11930E+02
   Friction velocity        uet   :  0.20880E-02 0.33473E+01
   Friction velocity        uk    :  0.30215E-01 0.34794E+01
   Dimensionless distance   yplus :  0.15070E+00 0.36456E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        512
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29497E+04    1537   0.52072E-02   0.46398E+00 
c  VelocityY    0.29497E+04    1537   0.52072E-02   0.00000E+00 
c  VelocityZ    0.29497E+04    1537   0.52072E-02   0.00000E+00 
c  Pressure     0.40505E+00    7017   0.35280E-01   0.18526E+00 
c  k            0.91667E+03    1249   0.21302E-03   0.15211E+01 
c  omega        0.11733E+08     414   0.31873E-04   0.17221E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2931e-05                         45443


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.26192         0.29205     -0.00039237      -2.185e-06
v  Velocity[Y]                  -27.22          32.204          6.2936          20.053
v  Velocity[Z]                 -26.461          27.632       -0.044622        0.035951
v  ǁVelocityǁ                 0.012818          32.384          10.286          20.347
v  Pressure                    -662.45          350.25         -16.395          31.159
v  k                        2.0494e-08          47.781          3.4727         0.38549
v  omega                    8.3953e-08      1.1733e+07          8055.2           13.26
v  turbulent_viscosity      4.9795e-15         0.33012       0.0098729         0.01681
v  CourantNb                  0.025095          2996.2          42.462          1.3868
v  FourierNb                0.00029099           12693              83         0.16932
v  total_pressure           1.0066e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14932         0.01077        0.045153


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0003           12730          125.46          1.5561


 TIME FOR THE TIME STEP              105:        0.43400E+02

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


 INSTANT    0.106000000E+02   TIME STEP NUMBER             106
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.567433269E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26792E+02 0.11872E+02
   Friction velocity        uet   :  0.83982E-03 0.30067E+01
   Friction velocity        uk    :  0.30841E-01 0.28801E+01
   Dimensionless distance   yplus :  0.13858E+00 0.27719E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        562
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29509E+04    1639   0.51778E-02   0.48473E+00 
c  VelocityY    0.29509E+04    1639   0.51778E-02   0.00000E+00 
c  VelocityZ    0.29509E+04    1639   0.51778E-02   0.00000E+00 
c  Pressure     0.39346E+00    7004   0.34993E-01   0.17970E+00 
c  k            0.92768E+03    1023   0.12326E-03   0.15870E+01 
c  omega        0.10381E+08     300   0.21916E-03   0.20568E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66197                             1
a  Local Time Step      1.2646e-05                         45388


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22097          0.3004     -0.00050339     -2.9442e-06
v  Velocity[Y]                 -23.805          32.204          6.3113          20.053
v  Velocity[Z]                 -27.421          27.103       -0.035986        0.037718
v  ǁVelocityǁ                 0.015156          32.285          10.235          20.348
v  Pressure                     -660.4           346.8         -18.427          31.237
v  k                        4.1169e-10          55.422           3.479         0.40617
v  omega                    4.9837e-08      8.4838e+07          8581.6          13.215
v  turbulent_viscosity      8.7959e-15         0.34524       0.0099566        0.017676
v  CourantNb                  0.060195          2995.2          42.577          1.3867
v  FourierNb                0.00033832           12798          82.223         0.17343
v  total_pressure           1.0066e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010769        0.045168


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0003           12837           124.8          1.5601


 TIME FOR THE TIME STEP              106:        0.42143E+02

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


 INSTANT    0.107000000E+02   TIME STEP NUMBER             107
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.484688362E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27407E+02 0.11962E+02
   Friction velocity        uet   :  0.39541E-03 0.28708E+01
   Friction velocity        uk    :  0.22344E-01 0.28068E+01
   Dimensionless distance   yplus :  0.86986E-01 0.28411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        571
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29521E+04    1767   0.52687E-02   0.51482E+00 
c  VelocityY    0.29521E+04    1767   0.52687E-02   0.00000E+00 
c  VelocityZ    0.29521E+04    1767   0.52687E-02   0.00000E+00 
c  Pressure     0.41907E+00    6969   0.32856E-01   0.19002E+00 
c  k            0.94284E+03    1125   0.12655E-03   0.17798E+01 
c  omega        0.38927E+08     142   0.12260E-03   0.73936E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -75126                             2
a  Local Time Step      1.2745e-05                         45389


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.2066         0.31141     -0.00053269     -3.7017e-06
v  Velocity[Y]                 -23.693          32.182          6.3357          20.053
v  Velocity[Z]                 -27.655          27.165        -0.04349        0.038729
v  ǁVelocityǁ                0.0042125          32.736           10.16          20.347
v  Pressure                    -656.79          344.83         -19.506          30.932
v  k                        3.9923e-10          53.103          3.4872         0.42776
v  omega                    2.9356e-08      1.4046e+08          9590.4          13.225
v  turbulent_viscosity      6.8845e-16          0.3628        0.010053        0.018571
v  CourantNb                  0.041348            2068          42.359          1.3865
v  FourierNb                0.00039369           12892          82.632           0.178
v  total_pressure           1.0067e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14944         0.01077        0.045213


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0004           12931          124.99          1.5645


 TIME FOR THE TIME STEP              107:        0.43797E+02

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


 INSTANT    0.108000000E+02   TIME STEP NUMBER             108
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.173067807E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27971E+02 0.15136E+02
   Friction velocity        uet   :  0.87052E-03 0.28145E+01
   Friction velocity        uk    :  0.15213E-01 0.28728E+01
   Dimensionless distance   yplus :  0.10052E+00 0.31315E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29534E+04    1779   0.53952E-02   0.53298E+00 
c  VelocityY    0.29534E+04    1779   0.53952E-02   0.00000E+00 
c  VelocityZ    0.29534E+04    1779   0.53952E-02   0.00000E+00 
c  Pressure     0.43491E+00    7032   0.34680E-01   0.19873E+00 
c  k            0.95874E+03    1220   0.12846E-03   0.20358E+01 
c  omega        0.11832E+09     245   0.32442E-04   0.43091E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -99396                             2
a  Local Time Step       1.291e-05                         45369


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20143         0.32643      -0.0004813     -4.1552e-06
v  Velocity[Y]                 -23.573           32.21          6.3465          20.054
v  Velocity[Z]                 -26.941          27.373       -0.069032        0.039376
v  ǁVelocityǁ                0.0025642          32.601          10.086          20.348
v  Pressure                    -655.13          343.26         -20.423          30.477
v  k                        3.5925e-08          42.393          3.4582         0.45023
v  omega                    1.7064e-08      7.0447e+07          9877.2          13.187
v  turbulent_viscosity      3.7416e-16         0.38247        0.010161        0.019497
v  CourantNb                  0.030742          2064.5          42.006          1.3863
v  FourierNb                0.00045841           12914           84.73         0.18324
v  total_pressure           1.0067e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14911         0.01077        0.045209


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0005           12953          126.74          1.5695


 TIME FOR THE TIME STEP              108:        0.44295E+02

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


 INSTANT    0.109000000E+02   TIME STEP NUMBER             109
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.311164055E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28594E+02 0.13969E+02
   Friction velocity        uet   :  0.86336E-03 0.26718E+01
   Friction velocity        uk    :  0.17780E-01 0.30899E+01
   Dimensionless distance   yplus :  0.16054E+00 0.34222E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29547E+04    1776   0.53065E-02   0.54177E+00 
c  VelocityY    0.29547E+04    1776   0.53065E-02   0.00000E+00 
c  VelocityZ    0.29547E+04    1776   0.53065E-02   0.00000E+00 
c  Pressure     0.46114E+00    6990   0.36401E-01   0.21076E+00 
c  k            0.97417E+03    1073   0.12405E-03   0.21633E+01 
c  omega        0.43759E+08     248   0.34203E-04   0.13315E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0008e+05                             1
a  Local Time Step      1.2488e-05                         45330


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.20624          0.3375     -0.00042008     -4.2191e-06
v  Velocity[Y]                 -23.451           32.18          6.3352          20.054
v  Velocity[Z]                 -26.747          27.564        -0.10855        0.039484
v  ǁVelocityǁ                 0.016409          32.194          10.043          20.348
v  Pressure                    -650.86          343.44         -20.404          30.006
v  k                        2.8246e-07          42.932          3.4232         0.47363
v  omega                    9.8952e-09      3.5637e+07          9136.1          13.076
v  turbulent_viscosity      3.8156e-14         0.41437        0.010258        0.020455
v  CourantNb                  0.023374          2069.4          41.848          1.3862
v  FourierNb                0.00053345           12974          85.024         0.18821
v  total_pressure           1.0067e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14824        0.010771        0.045197


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0005           13012          126.87          1.5744


 TIME FOR THE TIME STEP              109:        0.44294E+02

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


 INSTANT    0.110000000E+02   TIME STEP NUMBER             110
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.809477376E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28630E+02 0.18712E+02
   Friction velocity        uet   :  0.11662E-02 0.24655E+01
   Friction velocity        uk    :  0.27563E-01 0.30413E+01
   Dimensionless distance   yplus :  0.70829E-01 0.28661E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29561E+04    1794   0.51734E-02   0.54776E+00 
c  VelocityY    0.29561E+04    1794   0.51734E-02   0.00000E+00 
c  VelocityZ    0.29561E+04    1794   0.51734E-02   0.00000E+00 
c  Pressure     0.42267E+00    6950   0.34800E-01   0.19266E+00 
c  k            0.99207E+03    1126   0.12343E-03   0.23540E+01 
c  omega        0.18338E+08     224   0.41153E-04   0.50263E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62981                             1
a  Local Time Step       1.395e-05                         45309


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22123         0.35316     -0.00040209     -3.5316e-06
v  Velocity[Y]                 -23.306          32.074          6.3329          20.054
v  Velocity[Z]                 -27.658          27.805         -0.1281         0.03942
v  ǁVelocityǁ                 0.020216          32.288          10.015          20.347
v  Pressure                    -644.32          344.79         -19.918          29.632
v  k                        1.7289e-08          46.968          3.4296         0.49802
v  omega                    5.8086e-09       1.865e+07          8752.6          13.009
v  turbulent_viscosity      3.1427e-14         0.46997        0.010355        0.021445
v  CourantNb                  0.027229          2085.7          41.862          1.3863
v  FourierNb                0.00062006           13018          83.473         0.19299
v  total_pressure           1.0068e+05      1.0167e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14868         0.01077         0.04517


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0006           13059          125.34          1.5793


 TIME FOR THE TIME STEP              110:        0.43920E+02

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


 INSTANT    0.111000000E+02   TIME STEP NUMBER             111
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.486549337E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28654E+02 0.18786E+02
   Friction velocity        uet   :  0.53940E-03 0.27043E+01
   Friction velocity        uk    :  0.25242E-01 0.30273E+01
   Dimensionless distance   yplus :  0.11974E+00 0.26158E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29576E+04    1806   0.52633E-02   0.56255E+00 
c  VelocityY    0.29576E+04    1806   0.52633E-02   0.00000E+00 
c  VelocityZ    0.29576E+04    1806   0.52633E-02   0.00000E+00 
c  Pressure     0.40011E+00    6914   0.32389E-01   0.18379E+00 
c  k            0.10153E+04    1222   0.12999E-03   0.25582E+01 
c  omega        0.12379E+08     269   0.32168E-04   0.29691E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1491e+05                             2
a  Local Time Step      1.3965e-05                         45360


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.23364         0.35177     -0.00024096     -3.6856e-06
v  Velocity[Y]                 -23.143          32.021          6.3583          20.054
v  Velocity[Z]                  -28.98          27.712        -0.13937        0.038589
v  ǁVelocityǁ                 0.012619          34.759          10.023          20.346
v  Pressure                    -635.07          347.02          -18.85          29.403
v  k                        1.4736e-09          50.065          3.4473         0.52329
v  omega                    3.4902e-09      1.2526e+07          8535.4          12.946
v  turbulent_viscosity       1.192e-15         0.52314        0.010483         0.02247
v  CourantNb                  0.049892          2118.6          41.718           1.386
v  FourierNb                0.00072003           13050          83.342         0.19841
v  total_pressure           1.0069e+05      1.0167e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14909         0.01077        0.045142


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98164           13093          125.06          1.5844


 TIME FOR THE TIME STEP              111:        0.44845E+02

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


 INSTANT    0.112000000E+02   TIME STEP NUMBER             112
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.683565018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26364E+02 0.14947E+02
   Friction velocity        uet   :  0.10251E-02 0.29190E+01
   Friction velocity        uk    :  0.28390E-01 0.28066E+01
   Dimensionless distance   yplus :  0.11056E+00 0.25397E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :        990
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29590E+04    1831   0.52064E-02   0.57212E+00 
c  VelocityY    0.29590E+04    1831   0.52064E-02   0.00000E+00 
c  VelocityZ    0.29590E+04    1831   0.52064E-02   0.00000E+00 
c  Pressure     0.43070E+00    6929   0.30980E-01   0.19895E+00 
c  k            0.10476E+04    1231   0.14435E-03   0.27451E+01 
c  omega        0.11764E+08     274   0.22066E-04   0.15543E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3553e-05                         45391


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.24267         0.32643      1.1875e-05     -3.0894e-06
v  Velocity[Y]                 -22.915          31.923          6.4084          20.054
v  Velocity[Z]                  -30.67          27.612          -0.146        0.037464
v  ǁVelocityǁ                  0.01834           34.34          10.075          20.346
v  Pressure                    -623.04          349.31         -17.681          29.621
v  k                        1.5448e-08          57.643          3.4702         0.54937
v  omega                    2.1449e-09      1.1729e+07          8300.4          12.879
v  turbulent_viscosity      1.5453e-16         0.57032        0.010645        0.023529
v  CourantNb                  0.020851          2167.1          41.699          1.3858
v  FourierNb                0.00083437           13105          82.815         0.20427
v  total_pressure            1.007e+05      1.0167e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14681         0.01077        0.045128


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0008           13152          124.51          1.5901


 TIME FOR THE TIME STEP              112:        0.45582E+02

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


 INSTANT    0.113000000E+02   TIME STEP NUMBER             113
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.161171990E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.25049E+02 0.14545E+02
   Friction velocity        uet   :  0.18333E-02 0.28825E+01
   Friction velocity        uk    :  0.21854E-01 0.30028E+01
   Dimensionless distance   yplus :  0.14729E+00 0.24940E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29603E+04    1835   0.52327E-02   0.58454E+00 
c  VelocityY    0.29603E+04    1835   0.52327E-02   0.00000E+00 
c  VelocityZ    0.29603E+04    1835   0.52327E-02   0.00000E+00 
c  Pressure     0.42668E+00    6978   0.33050E-01   0.19573E+00 
c  k            0.10918E+04    1181   0.14906E-03   0.28756E+01 
c  omega        0.10894E+08     250   0.25420E-04   0.15323E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.6729e-07                             1
a  omega          
a  Local Time Step      1.3473e-05                         45447


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.24597         0.29287      0.00026368     -3.1655e-06
v  Velocity[Y]                 -22.741          31.882          6.4788          20.053
v  Velocity[Z]                 -29.992          27.747        -0.11195        0.036177
v  ǁVelocityǁ                 0.016388          32.356          10.158          20.344
v  Pressure                    -609.67          350.18         -17.672           29.39
v  k                         1.472e-08          62.139          3.4785         0.57611
v  omega                    1.3361e-09      1.1671e+07          8457.8          12.864
v  turbulent_viscosity      1.7217e-15         0.61773        0.010814        0.024624
v  CourantNb                  0.022379            2220          41.882          1.3857
v  FourierNb                0.00096473           13149          81.909         0.21008
v  total_pressure           1.0072e+05      1.0168e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14796        0.010769        0.045151


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.001           13200          123.79          1.5957


 TIME FOR THE TIME STEP              113:        0.45418E+02

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


 INSTANT    0.114000000E+02   TIME STEP NUMBER             114
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.744352371E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26888E+02 0.14468E+02
   Friction velocity        uet   :  0.20646E-03 0.27791E+01
   Friction velocity        uk    :  0.14447E-01 0.30752E+01
   Dimensionless distance   yplus :  0.11676E+00 0.24401E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29618E+04    1820   0.53502E-02   0.58993E+00 
c  VelocityY    0.29618E+04    1820   0.53502E-02   0.00000E+00 
c  VelocityZ    0.29618E+04    1820   0.53502E-02   0.00000E+00 
c  Pressure     0.41903E+00    7074   0.35482E-01   0.19173E+00 
c  k            0.11456E+04    1399   0.14800E-03   0.29129E+01 
c  omega        0.11441E+08     221   0.16273E-03   0.13807E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015985                             1
a  omega                    -98473                             2
a  Local Time Step      1.3255e-05                         45484


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.26447          0.2556       0.0004326     -2.3829e-06
v  Velocity[Y]                 -22.451           31.83          6.5436          20.053
v  Velocity[Z]                 -28.146          27.224        -0.04072        0.034785
v  ǁVelocityǁ                 0.005132          31.843          10.218          20.343
v  Pressure                    -599.33          350.06         -18.173          29.339
v  k                         3.437e-08          80.315          3.4737         0.60325
v  omega                    8.3525e-10      6.2999e+07            8949          12.848
v  turbulent_viscosity      3.7925e-15         0.66746        0.010984        0.025756
v  CourantNb                  0.046806          2267.1          42.326          1.3857
v  FourierNb                 0.0011128           13189          81.142         0.21591
v  total_pressure           1.0073e+05      1.0168e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14746        0.010768        0.045113


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94829           13242          123.47          1.6016


 TIME FOR THE TIME STEP              114:        0.45295E+02

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


 INSTANT    0.115000000E+02   TIME STEP NUMBER             115
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.131771857E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26965E+02 0.13544E+02
   Friction velocity        uet   :  0.12704E-02 0.24877E+01
   Friction velocity        uk    :  0.15329E-01 0.30513E+01
   Dimensionless distance   yplus :  0.13518E+00 0.24173E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29633E+04    1827   0.52901E-02   0.58139E+00 
c  VelocityY    0.29633E+04    1827   0.52901E-02   0.00000E+00 
c  VelocityZ    0.29633E+04    1827   0.52901E-02   0.00000E+00 
c  Pressure     0.41475E+00    7060   0.34874E-01   0.19091E+00 
c  k            0.12028E+04    1505   0.14254E-03   0.29123E+01 
c  omega        0.47283E+08     189   0.56691E-04   0.97791E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018544                             2
a  omega               -2.9052e+05                             1
a  Local Time Step      1.2724e-05                         45518


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.33149         0.21935      0.00057975     -1.3886e-06
v  Velocity[Y]                 -23.652          31.781          6.5628          20.054
v  Velocity[Z]                 -27.274          27.092        0.032631        0.032702
v  ǁVelocityǁ                0.0097261          31.808           10.25          20.343
v  Pressure                    -586.83          349.74          -18.87          29.297
v  k                        2.3609e-09          98.374          3.4647         0.63067
v  omega                    5.1843e-10      3.5645e+07          9035.4          12.841
v  turbulent_viscosity      7.4938e-15         0.71662        0.011155        0.026921
v  CourantNb                  0.021259          2301.5          42.625          1.3859
v  FourierNb                 0.0012803           13133          80.509         0.22197
v  total_pressure           1.0074e+05      1.0167e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14919        0.010769        0.045084


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0013           13188          123.13          1.6079


 TIME FOR THE TIME STEP              115:        0.45992E+02

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


 INSTANT    0.116000000E+02   TIME STEP NUMBER             116
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.739220708E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27728E+02 0.13443E+02
   Friction velocity        uet   :  0.51947E-03 0.22797E+01
   Friction velocity        uk    :  0.69710E-02 0.31537E+01
   Dimensionless distance   yplus :  0.56837E-01 0.23873E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        474
   Nb of faces within the viscous sub-layer     :       1101
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29649E+04    1836   0.52457E-02   0.55997E+00 
c  VelocityY    0.29649E+04    1836   0.52457E-02   0.00000E+00 
c  VelocityZ    0.29649E+04    1836   0.52457E-02   0.00000E+00 
c  Pressure     0.40825E+00    6952   0.31881E-01   0.18830E+00 
c  k            0.12586E+04    1529   0.13337E-03   0.28747E+01 
c  omega        0.50247E+08     127   0.29617E-04   0.26862E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010786                             2
a  omega                    -42543                             1
a  Local Time Step      1.2713e-05                         45501


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39453         0.25732      0.00071554     -6.4924e-07
v  Velocity[Y]                 -30.488          31.694          6.5305          20.054
v  Velocity[Z]                 -27.319           26.84         0.08135        0.030502
v  ǁVelocityǁ                0.0076766          31.739           10.28          20.342
v  Pressure                    -570.87          349.71         -19.377          29.574
v  k                        1.1879e-09          92.934          3.4754         0.65834
v  omega                    3.1775e-10      6.5624e+07          9186.7          12.834
v  turbulent_viscosity      4.9808e-15         0.76427        0.011313        0.028121
v  CourantNb                  0.024514          2313.4          42.757          1.3862
v  FourierNb                 0.0014693           12970          80.252         0.22794
v  total_pressure           1.0075e+05      1.0167e+05      1.0131e+05      1.0135e+05
v  Local Time Step                0.01         0.14898        0.010769        0.045046


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9483           13028          123.01          1.6141


 TIME FOR THE TIME STEP              116:        0.44633E+02

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


 INSTANT    0.117000000E+02   TIME STEP NUMBER             117
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.151416437E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28190E+02 0.21305E+02
   Friction velocity        uet   :  0.16961E-02 0.27569E+01
   Friction velocity        uk    :  0.82662E-02 0.30309E+01
   Dimensionless distance   yplus :  0.81819E-01 0.29398E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        509
   Nb of faces within the viscous sub-layer     :       1111
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29662E+04    1791   0.52959E-02   0.54614E+00 
c  VelocityY    0.29662E+04    1791   0.52959E-02   0.00000E+00 
c  VelocityZ    0.29662E+04    1791   0.52959E-02   0.00000E+00 
c  Pressure     0.41933E+00    6674   0.31415E-01   0.19367E+00 
c  k            0.13066E+04    1499   0.14928E-03   0.27904E+01 
c  omega        0.51481E+08     190   0.17225E-04   0.95408E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014355                             2
a  omega               -2.6336e+05                             1
a  Local Time Step      1.2606e-05                         45471


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.44501         0.30887      0.00075078      3.1972e-07
v  Velocity[Y]                  -26.69          31.606          6.4835          20.054
v  Velocity[Z]                 -27.457          26.912          0.1183        0.028054
v  ǁVelocityǁ                0.0051537          33.362          10.329          20.341
v  Pressure                    -552.49          349.36         -20.326          29.859
v  k                        4.6347e-10          95.373          3.5318          0.6864
v  omega                    1.9307e-10      3.2936e+07          8857.7          12.758
v  turbulent_viscosity      5.0349e-15          0.8032        0.011479        0.029353
v  CourantNb                  0.023558          2299.7          42.857          1.3865
v  FourierNb                 0.0016814           12667          80.555         0.23455
v  total_pressure           1.0077e+05      1.0167e+05       1.013e+05      1.0135e+05
v  Local Time Step                0.01         0.14909        0.010771        0.045056


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96599           12726          123.41           1.621


 TIME FOR THE TIME STEP              117:        0.43323E+02

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


 INSTANT    0.118000000E+02   TIME STEP NUMBER             118
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.730748558E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51740E+02 0.15304E+02
   Friction velocity        uet   :  0.15926E-02 0.28652E+01
   Friction velocity        uk    :  0.13038E-01 0.36258E+01
   Dimensionless distance   yplus :  0.61227E-01 0.33400E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :       1083
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29676E+04    1768   0.53890E-02   0.55014E+00 
c  VelocityY    0.29676E+04    1768   0.53890E-02   0.00000E+00 
c  VelocityZ    0.29676E+04    1768   0.53890E-02   0.00000E+00 
c  Pressure     0.39071E+00    6987   0.34485E-01   0.18061E+00 
c  k            0.13515E+04    1449   0.18507E-03   0.27279E+01 
c  omega        0.21235E+08     434   0.32232E-04   0.10371E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2695e-05                         45434


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.46963         0.35211       0.0007736      3.8293e-07
v  Velocity[Y]                 -33.416          31.466          6.4876          20.054
v  Velocity[Z]                 -27.358          26.958          0.1488         0.02508
v  ǁVelocityǁ                0.0034353          34.127          10.366           20.34
v  Pressure                    -532.37          349.03         -21.691          30.167
v  k                        7.6897e-09          92.546          3.5841         0.71499
v  omega                    1.1686e-10      4.9703e+07          8630.5          12.675
v  turbulent_viscosity      2.2439e-15         0.84308        0.011652        0.030619
v  CourantNb                  0.027686          2264.2          43.145          1.3867
v  FourierNb                 0.0019183           12433          79.907         0.24136
v  total_pressure           1.0079e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01          0.1492        0.010773        0.045053


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.74429           12492          123.05           1.628


 TIME FOR THE TIME STEP              118:        0.44499E+02

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


 INSTANT    0.119000000E+02   TIME STEP NUMBER             119
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.180206260E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37199E+02 0.13417E+02
   Friction velocity        uet   :  0.22094E-02 0.31232E+01
   Friction velocity        uk    :  0.15333E-01 0.33202E+01
   Dimensionless distance   yplus :  0.10018E+00 0.33216E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        520
   Nb of faces within the viscous sub-layer     :       1084
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29689E+04    1749   0.54602E-02   0.55271E+00 
c  VelocityY    0.29689E+04    1749   0.54602E-02   0.00000E+00 
c  VelocityZ    0.29689E+04    1749   0.54602E-02   0.00000E+00 
c  Pressure     0.41101E+00    7096   0.36607E-01   0.18913E+00 
c  k            0.14005E+04    1278   0.18186E-03   0.27819E+01 
c  omega        0.24993E+08     373   0.41670E-04   0.21579E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -96374                             2
a  Local Time Step      1.1762e-05                         45426


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.45405         0.36373      0.00079641     -1.4852e-07
v  Velocity[Y]                 -20.598          31.433          6.5266          20.054
v  Velocity[Z]                 -27.251          27.104         0.16372        0.021771
v  ǁVelocityǁ                0.0082586          31.516          10.373           20.34
v  Pressure                     -518.3          349.23         -22.766          30.751
v  k                        4.8826e-10          62.243          3.5893          0.7441
v  omega                    7.0448e-11      5.9877e+07          8597.8           12.65
v  turbulent_viscosity      7.3365e-15         0.87515        0.011854        0.031917
v  CourantNb                  0.037242            2779          43.533          1.3867
v  FourierNb                 0.0021823           12384           79.67         0.24832
v  total_pressure           1.0081e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01            0.15        0.010772        0.045051


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.6194           12440           123.2           1.635


 TIME FOR THE TIME STEP              119:        0.44138E+02

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


 INSTANT    0.120000000E+02   TIME STEP NUMBER             120
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.419230388E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29487E+02 0.13569E+02
   Friction velocity        uet   :  0.97809E-03 0.23343E+01
   Friction velocity        uk    :  0.30441E-01 0.30819E+01
   Dimensionless distance   yplus :  0.14692E+00 0.27690E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        511
   Nb of faces within the viscous sub-layer     :       1053
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29702E+04    1796   0.53464E-02   0.56471E+00 
c  VelocityY    0.29702E+04    1796   0.53464E-02   0.00000E+00 
c  VelocityZ    0.29702E+04    1796   0.53464E-02   0.00000E+00 
c  Pressure     0.42409E+00    7105   0.34952E-01   0.19539E+00 
c  k            0.14546E+04    1085   0.11226E-03   0.28003E+01 
c  omega        0.56175E+08     145   0.71253E-05   0.77019E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7346e+05                             2
a  Local Time Step      1.2854e-05                         45409


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.40783         0.36313       0.0006534      5.6596e-07
v  Velocity[Y]                 -20.228           31.37          6.5734          20.054
v  Velocity[Z]                  -27.01          27.365         0.14534        0.018679
v  ǁVelocityǁ                0.0097903          32.039          10.356          20.339
v  Pressure                    -502.84          350.19         -22.811              31
v  k                        1.0283e-08          61.948          3.6123         0.77376
v  omega                      4.24e-11      2.9936e+07          8392.4          12.604
v  turbulent_viscosity      1.7546e-15         0.90593        0.012063        0.033248
v  CourantNb                  0.040963          2463.6          43.599          1.3864
v  FourierNb                  0.002475           12266          80.236         0.25513
v  total_pressure           1.0082e+05      1.0168e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01          0.1491         0.01077        0.045075


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8734           12320          123.83          1.6416


 TIME FOR THE TIME STEP              120:        0.43829E+02

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


 INSTANT    0.121000000E+02   TIME STEP NUMBER             121
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.159826188E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29316E+02 0.16558E+02
   Friction velocity        uet   :  0.13872E-02 0.26342E+01
   Friction velocity        uk    :  0.16400E-01 0.30586E+01
   Dimensionless distance   yplus :  0.15531E+00 0.30539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        572
   Nb of faces within the viscous sub-layer     :       1102
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29714E+04    1974   0.51589E-02   0.59414E+00 
c  VelocityY    0.29714E+04    1974   0.51589E-02   0.00000E+00 
c  VelocityZ    0.29714E+04    1974   0.51589E-02   0.00000E+00 
c  Pressure     0.46422E+00    6918   0.30950E-01   0.21383E+00 
c  k            0.15121E+04    1157   0.11679E-03   0.30210E+01 
c  omega        0.17502E+08     380   0.26242E-04   0.56096E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.861e-05                             1
a  omega               -1.9824e+05                             2
a  Local Time Step      1.3197e-05                         45378


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.32399         0.37443      0.00058636      7.7882e-07
v  Velocity[Y]                  -19.88          31.262           6.615          20.054
v  Velocity[Z]                 -27.855          27.857        0.098355        0.015101
v  ǁVelocityǁ                0.0034121          31.915          10.323          20.338
v  Pressure                    -484.05          352.08         -21.672           31.09
v  k                         3.779e-08          61.691          3.6295         0.80404
v  omega                    2.5299e-11      1.4959e+07            8530           12.61
v  turbulent_viscosity       2.668e-15         0.93419         0.01229        0.034611
v  CourantNb                  0.043449          2198.2          43.464          1.3861
v  FourierNb                 0.0027986           12200          81.923         0.26238
v  total_pressure           1.0084e+05      1.0168e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14836        0.010769        0.045108


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0028           12247          125.39          1.6485


 TIME FOR THE TIME STEP              121:        0.45304E+02

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


 INSTANT    0.122000000E+02   TIME STEP NUMBER             122
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.232396939E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30186E+02 0.13501E+02
   Friction velocity        uet   :  0.25667E-02 0.26794E+01
   Friction velocity        uk    :  0.16628E-01 0.27855E+01
   Dimensionless distance   yplus :  0.10994E+00 0.29547E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        590
   Nb of faces within the viscous sub-layer     :       1144
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29726E+04    1730   0.51708E-02   0.63026E+00 
c  VelocityY    0.29726E+04    1730   0.51708E-02   0.00000E+00 
c  VelocityZ    0.29726E+04    1730   0.51708E-02   0.00000E+00 
c  Pressure     0.44715E+00    7008   0.29676E-01   0.20573E+00 
c  k            0.15712E+04    1316   0.11673E-03   0.33039E+01 
c  omega        0.11485E+08     474   0.97058E-04   0.66358E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4167e+05                             3
a  Local Time Step      1.3143e-05                         45318


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.29704         0.37472      0.00068808      8.5308e-07
v  Velocity[Y]                 -19.454          31.203          6.6307          20.054
v  Velocity[Z]                 -27.022            28.1        0.030737        0.011184
v  ǁVelocityǁ                 0.013838          31.887          10.302          20.337
v  Pressure                    -463.49          352.58         -20.845          30.747
v  k                        9.7151e-09          61.002          3.6142         0.83499
v  omega                    1.4991e-11      4.8611e+07          8782.1          12.571
v  turbulent_viscosity      9.7342e-15         0.95872        0.012531        0.036007
v  CourantNb                  0.026411          2190.1          43.253          1.3858
v  FourierNb                 0.0031552           12200          83.779          0.2698
v  total_pressure           1.0086e+05      1.0168e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14799         0.01077        0.045139


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0032           12246          127.03          1.6557


 TIME FOR THE TIME STEP              122:        0.43551E+02

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


 INSTANT    0.123000000E+02   TIME STEP NUMBER             123
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.185745193E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26912E+02 0.19863E+02
   Friction velocity        uet   :  0.60355E-03 0.26093E+01
   Friction velocity        uk    :  0.14471E-01 0.30282E+01
   Dimensionless distance   yplus :  0.11731E+00 0.34775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        609
   Nb of faces within the viscous sub-layer     :       1152
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29738E+04    1778   0.53717E-02   0.65484E+00 
c  VelocityY    0.29738E+04    1778   0.53717E-02   0.00000E+00 
c  VelocityZ    0.29738E+04    1778   0.53717E-02   0.00000E+00 
c  Pressure     0.44597E+00    6922   0.30000E-01   0.20619E+00 
c  k            0.16315E+04    1367   0.12036E-03   0.35840E+01 
c  omega        0.14333E+08     317   0.48203E-03   0.18544E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019745                             2
a  omega               -3.0529e+05                             2
a  Local Time Step      1.2596e-05                         45217


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -0.253         0.38063       0.0011239      2.0441e-06
v  Velocity[Y]                 -19.034           31.11           6.602          20.055
v  Velocity[Z]                 -27.055          27.898       -0.028174       0.0076161
v  ǁVelocityǁ                0.0033288          31.766          10.275          20.337
v  Pressure                    -442.22          352.45         -19.881          30.462
v  k                        7.8718e-10          60.407          3.5983         0.86677
v  omega                    8.9861e-12      3.2377e+08           10338          12.662
v  turbulent_viscosity      4.6606e-15         0.98101        0.012778        0.037436
v  CourantNb                  0.042285          2178.5          43.183          1.3857
v  FourierNb                 0.0035466           12190          83.522         0.27688
v  total_pressure           1.0088e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14812         0.01077        0.045125


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90384           12236           126.7          1.6626


 TIME FOR THE TIME STEP              123:        0.43795E+02

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


 INSTANT    0.124000000E+02   TIME STEP NUMBER             124
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.102023865E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.26967E+02 0.19257E+02
   Friction velocity        uet   :  0.88320E-03 0.24471E+01
   Friction velocity        uk    :  0.12323E-01 0.31310E+01
   Dimensionless distance   yplus :  0.83118E-01 0.29424E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        602
   Nb of faces within the viscous sub-layer     :       1164
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29748E+04    1841   0.52525E-02   0.69156E+00 
c  VelocityY    0.29748E+04    1841   0.52525E-02   0.00000E+00 
c  VelocityZ    0.29748E+04    1841   0.52525E-02   0.00000E+00 
c  Pressure     0.43218E+00    7001   0.29646E-01   0.20022E+00 
c  k            0.16944E+04    1412   0.12975E-03   0.39646E+01 
c  omega        0.41983E+09      64   0.70434E-05   0.47432E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019685                             7
a  omega               -3.5835e+05                             2
a  Local Time Step      1.3765e-05                         45204


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.17943          0.3966       0.0014886      3.2058e-06
v  Velocity[Y]                 -18.543          30.947          6.5675          20.054
v  Velocity[Z]                 -28.946          27.838       -0.084337       0.0035092
v  ǁVelocityǁ                0.0028809          35.096          10.248          20.335
v  Pressure                    -426.12          352.18         -18.476          30.451
v  k                        7.6702e-09          59.643          3.5909          0.8994
v  omega                    5.4549e-12      1.6206e+08          9359.9          12.563
v  turbulent_viscosity      7.2548e-16          1.0024        0.013024        0.038901
v  CourantNb                  0.042301          2169.6          43.067          1.3855
v  FourierNb                 0.0039748           12282          82.603         0.28365
v  total_pressure            1.009e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010769        0.045129


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.004           12331          125.67          1.6691


 TIME FOR THE TIME STEP              124:        0.43926E+02

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


 INSTANT    0.125000000E+02   TIME STEP NUMBER             125
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.177359832E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28109E+02 0.17145E+02
   Friction velocity        uet   :  0.61288E-03 0.28770E+01
   Friction velocity        uk    :  0.18499E-01 0.29299E+01
   Dimensionless distance   yplus :  0.12907E+00 0.25041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        618
   Nb of faces within the viscous sub-layer     :       1151
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29759E+04    1868   0.51882E-02   0.73227E+00 
c  VelocityY    0.29759E+04    1868   0.51882E-02   0.00000E+00 
c  VelocityZ    0.29759E+04    1868   0.51882E-02   0.00000E+00 
c  Pressure     0.44680E+00    6965   0.30746E-01   0.20626E+00 
c  k            0.17611E+04    1430   0.14489E-03   0.44620E+01 
c  omega        0.10625E+09     207   0.33673E-04   0.49310E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0023457                            10
a  omega               -2.8101e+05                             2
a  Local Time Step      1.3686e-05                         45239


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.22142         0.41877       0.0016587      4.3505e-06
v  Velocity[Y]                 -18.039          30.878          6.5508          20.054
v  Velocity[Z]                 -31.114          27.698        -0.14123     -0.00045584
v  ǁVelocityǁ                0.0072654          36.261           10.25          20.334
v  Pressure                    -408.89          351.49         -17.259          30.622
v  k                        2.0929e-08          58.687          3.5896         0.93295
v  omega                    3.3915e-12      1.5048e+08          9232.6          12.533
v  turbulent_viscosity      7.1324e-15          1.0216        0.013291        0.040402
v  CourantNb                  0.028488          2167.3          42.925           1.385
v  FourierNb                 0.0044416           12682          82.471         0.29097
v  total_pressure           1.0092e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01          0.1492        0.010767        0.045133


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0044           12729           125.4           1.676


 TIME FOR THE TIME STEP              125:        0.44621E+02

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


 INSTANT    0.126000000E+02   TIME STEP NUMBER             126
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.371037456E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27504E+02 0.12741E+02
   Friction velocity        uet   :  0.16272E-02 0.30765E+01
   Friction velocity        uk    :  0.16077E-01 0.30668E+01
   Dimensionless distance   yplus :  0.39199E-01 0.25193E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        608
   Nb of faces within the viscous sub-layer     :       1102
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29770E+04    1899   0.50127E-02   0.76341E+00 
c  VelocityY    0.29770E+04    1899   0.50127E-02   0.00000E+00 
c  VelocityZ    0.29770E+04    1899   0.50127E-02   0.00000E+00 
c  Pressure     0.42694E+00    6983   0.33542E-01   0.19787E+00 
c  k            0.18343E+04    1352   0.15981E-03   0.50100E+01 
c  omega        0.10902E+09      93   0.33467E-04   0.51984E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0015322                             4
a  omega          
a  Local Time Step      1.3698e-05                         45461


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.24874         0.44336       0.0015775      4.4763e-06
v  Velocity[Y]                 -17.561          30.783          6.5556          20.054
v  Velocity[Z]                 -32.383          27.199        -0.17762      -0.0048651
v  ǁVelocityǁ                0.0093403            35.6           10.27          20.332
v  Pressure                    -389.03           350.5         -16.292          31.084
v  k                        4.4377e-09          62.647          3.5867         0.96749
v  omega                    2.1379e-12      1.5306e+08          9220.7          12.486
v  turbulent_viscosity      1.7801e-15          1.0421        0.013552        0.041941
v  CourantNb                  0.048557          2172.9          42.629          1.3842
v  FourierNb                 0.0049485           12900          82.725         0.29826
v  total_pressure           1.0094e+05      1.0168e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01           0.149        0.010764        0.045114


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0049           12949          125.35          1.6824


 TIME FOR THE TIME STEP              126:        0.45822E+02

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


 INSTANT    0.127000000E+02   TIME STEP NUMBER             127
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.238005207E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27630E+02 0.12444E+02
   Friction velocity        uet   :  0.16325E-02 0.29824E+01
   Friction velocity        uk    :  0.15480E-01 0.29351E+01
   Dimensionless distance   yplus :  0.11575E+00 0.25550E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        563
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29782E+04    1907   0.51543E-02   0.78652E+00 
c  VelocityY    0.29782E+04    1907   0.51543E-02   0.00000E+00 
c  VelocityZ    0.29782E+04    1907   0.51543E-02   0.00000E+00 
c  Pressure     0.41670E+00    6995   0.34538E-01   0.19194E+00 
c  k            0.19165E+04    1242   0.17815E-03   0.55729E+01 
c  omega        0.11423E+09      96   0.15739E-04   0.15779E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00054887                             6
a  omega          
a  Local Time Step      1.3659e-05                         45566


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.27132         0.50899       0.0012318      4.7134e-06
v  Velocity[Y]                 -17.167          30.617          6.5694          20.053
v  Velocity[Z]                 -32.535          27.224        -0.17566       -0.008693
v  ǁVelocityǁ                0.0048335          34.839          10.277           20.33
v  Pressure                    -385.98          349.02           -15.6          31.308
v  k                        3.5379e-08           74.62          3.5779          1.0029
v  omega                    1.3552e-12      7.6712e+07          8625.8          12.402
v  turbulent_viscosity      1.2615e-16          1.0618         0.01381        0.043522
v  CourantNb                  0.016708          2483.5          42.561          1.3834
v  FourierNb                 0.0054974           13194          82.647         0.30551
v  total_pressure           1.0094e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14908        0.010764        0.045107


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81402           13242          125.21          1.6889


 TIME FOR THE TIME STEP              127:        0.45233E+02

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


 INSTANT    0.128000000E+02   TIME STEP NUMBER             128
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.187318499E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27391E+02 0.12689E+02
   Friction velocity        uet   :  0.47693E-03 0.29914E+01
   Friction velocity        uk    :  0.18783E-01 0.29212E+01
   Dimensionless distance   yplus :  0.11486E+00 0.27638E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        584
   Nb of faces within the viscous sub-layer     :       1056
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29795E+04    1842   0.50472E-02   0.77429E+00 
c  VelocityY    0.29795E+04    1842   0.50472E-02   0.00000E+00 
c  VelocityZ    0.29795E+04    1842   0.50472E-02   0.00000E+00 
c  Pressure     0.43649E+00    6969   0.33228E-01   0.20212E+00 
c  k            0.20066E+04    1130   0.19230E-03   0.60930E+01 
c  omega        0.32171E+08     127   0.30019E-04   0.55639E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000754                             2
a  omega          
a  Local Time Step      1.2691e-05                         45559


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.26493         0.55898      0.00093347      5.0334e-06
v  Velocity[Y]                 -23.717          30.547          6.5575          20.054
v  Velocity[Z]                 -30.863          27.373        -0.14688       -0.012871
v  ǁVelocityǁ                 0.018444          32.141           10.25           20.33
v  Pressure                    -390.89          346.83         -15.497          31.485
v  k                        3.0921e-09          60.841          3.5638          1.0392
v  omega                    8.5251e-13      3.8735e+07          8366.8          12.372
v  turbulent_viscosity      7.4244e-15          1.0798        0.014052        0.045148
v  CourantNb                  0.021388          2509.1          42.654          1.3827
v  FourierNb                 0.0060894           13377          82.671         0.31292
v  total_pressure           1.0093e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14941        0.010763        0.045067


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82454           13425          125.33          1.6957


 TIME FOR THE TIME STEP              128:        0.44297E+02

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


 INSTANT    0.129000000E+02   TIME STEP NUMBER             129
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.212220664E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28546E+02 0.12723E+02
   Friction velocity        uet   :  0.11308E-02 0.27081E+01
   Friction velocity        uk    :  0.36344E-01 0.29537E+01
   Dimensionless distance   yplus :  0.13323E+00 0.33468E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        515
   Nb of faces within the viscous sub-layer     :       1108
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29808E+04    1777   0.49033E-02   0.73663E+00 
c  VelocityY    0.29808E+04    1777   0.49033E-02   0.00000E+00 
c  VelocityZ    0.29808E+04    1777   0.49033E-02   0.00000E+00 
c  Pressure     0.40674E+00    6946   0.30180E-01   0.18676E+00 
c  k            0.21038E+04    1162   0.20871E-03   0.65862E+01 
c  omega        0.14386E+08     189   0.39471E-04   0.34308E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2551e-05                         45535


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.28991         0.57727      0.00070879      4.5876e-06
v  Velocity[Y]                 -21.569          30.375          6.5016          20.053
v  Velocity[Z]                 -27.687          27.385        -0.10649        -0.01643
v  ǁVelocityǁ                 0.015725          31.032           10.22          20.328
v  Pressure                    -376.75          344.62         -16.212          31.108
v  k                        2.7694e-09          62.827          3.5582          1.0764
v  omega                    5.3004e-13      2.0137e+07          8322.1          12.329
v  turbulent_viscosity      3.9678e-15          1.0961        0.014276        0.046821
v  CourantNb                    0.0145          2221.9          42.503          1.3823
v  FourierNb                  0.006726           13418          83.122         0.32056
v  total_pressure           1.0095e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010762        0.045072


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0067           13466          125.63          1.7028


 TIME FOR THE TIME STEP              129:        0.43731E+02

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


 INSTANT    0.130000000E+02   TIME STEP NUMBER             130
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.347987940E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28980E+02 0.12188E+02
   Friction velocity        uet   :  0.12522E-02 0.23699E+01
   Friction velocity        uk    :  0.91529E-02 0.28413E+01
   Dimensionless distance   yplus :  0.73565E-01 0.28940E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        513
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29820E+04    1724   0.50562E-02   0.70637E+00 
c  VelocityY    0.29820E+04    1724   0.50562E-02   0.00000E+00 
c  VelocityZ    0.29820E+04    1724   0.50562E-02   0.00000E+00 
c  Pressure     0.44846E+00    6942   0.29287E-01   0.20673E+00 
c  k            0.22072E+04    1331   0.22082E-03   0.69847E+01 
c  omega        0.11420E+08     237   0.28803E-04   0.20110E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00051717                             2
a  omega          
a  Local Time Step      1.2476e-05                         45558


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.27302           0.561      0.00062204      3.1411e-06
v  Velocity[Y]                 -25.722          30.198          6.4305          20.053
v  Velocity[Z]                  -27.05          27.372       -0.076005       -0.020329
v  ǁVelocityǁ                  0.01728          31.497          10.241          20.325
v  Pressure                    -347.95          343.14         -17.338          31.265
v  k                         3.121e-09          73.081          3.5968          1.1146
v  omega                    3.2756e-13      1.1738e+07          8118.8           12.26
v  turbulent_viscosity      2.4907e-15          1.1105        0.014499        0.048545
v  CourantNb                  0.059849          2241.8          42.287          1.3818
v  FourierNb                 0.0074074           13432          83.128         0.32829
v  total_pressure           1.0098e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14915        0.010762        0.045057


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0074           13481          125.42          1.7101


 TIME FOR THE TIME STEP              130:        0.43964E+02

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


 INSTANT    0.131000000E+02   TIME STEP NUMBER             131
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.823842773E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29467E+02 0.17075E+02
   Friction velocity        uet   :  0.42539E-03 0.23137E+01
   Friction velocity        uk    :  0.94980E-02 0.30954E+01
   Dimensionless distance   yplus :  0.10883E+00 0.25944E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :       1090
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29833E+04    1687   0.48457E-02   0.70417E+00 
c  VelocityY    0.29833E+04    1687   0.48457E-02   0.00000E+00 
c  VelocityZ    0.29833E+04    1687   0.48457E-02   0.00000E+00 
c  Pressure     0.43724E+00    7008   0.32770E-01   0.20385E+00 
c  k            0.23173E+04    1437   0.24093E-03   0.73666E+01 
c  omega        0.23708E+08     312   0.83373E-04   0.12443E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014523                             2
a  omega               -2.5306e+05                             2
a  Local Time Step      1.2708e-05                         45535


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.29585         0.50963      0.00056224       1.413e-06
v  Velocity[Y]                 -34.041          30.063          6.4257          20.053
v  Velocity[Z]                 -26.961          27.728       -0.037289       -0.023404
v  ǁVelocityǁ                 0.017365          34.472          10.284          20.324
v  Pressure                    -347.96          342.15         -19.667          31.281
v  k                        4.7391e-09          103.42          3.6729          1.1537
v  omega                    2.0324e-13      4.5412e+07          8714.5          12.292
v  turbulent_viscosity      3.4025e-15          1.1935        0.014728        0.050322
v  CourantNb                  0.010753          2254.7          42.256          1.3815
v  FourierNb                 0.0081341           13542           82.66         0.33657
v  total_pressure           1.0098e+05      1.0167e+05      1.0131e+05      1.0136e+05
v  Local Time Step                0.01         0.14815        0.010762        0.045044


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0081           13590          124.92           1.718


 TIME FOR THE TIME STEP              131:        0.43662E+02

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


 INSTANT    0.132000000E+02   TIME STEP NUMBER             132
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.257084492E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42624E+02 0.12329E+02
   Friction velocity        uet   :  0.12256E-02 0.31127E+01
   Friction velocity        uk    :  0.14330E-01 0.36421E+01
   Dimensionless distance   yplus :  0.15180E+00 0.34383E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1083
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29846E+04    1715   0.48362E-02   0.71088E+00 
c  VelocityY    0.29846E+04    1715   0.48362E-02   0.00000E+00 
c  VelocityZ    0.29846E+04    1715   0.48362E-02   0.00000E+00 
c  Pressure     0.41558E+00    7093   0.36309E-01   0.19390E+00 
c  k            0.24373E+04    1485   0.26331E-03   0.76910E+01 
c  omega        0.20430E+08     436   0.30956E-03   0.10738E+10 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00062379                             1
a  omega          
a  Local Time Step      1.2726e-05                         45524


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.31506         0.42085      0.00050922     -5.0385e-07
v  Velocity[Y]                  -24.79          29.936          6.4826          20.053
v  Velocity[Z]                 -26.838          27.727       -0.003604       -0.026557
v  ǁVelocityǁ                0.0063216          31.656          10.325          20.321
v  Pressure                    -344.69          342.31         -22.158          31.552
v  k                        1.5153e-08          77.397          3.7208          1.1937
v  omega                    1.2614e-13       1.704e+08           10563          12.381
v  turbulent_viscosity      9.2953e-15          1.2742        0.014977        0.052154
v  CourantNb                   0.03263          2267.6          42.495          1.3813
v  FourierNb                 0.0089063           13759          82.361         0.34535
v  total_pressure           1.0098e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01          0.1487        0.010763        0.045053


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0089           13803          124.86          1.7266


 TIME FOR THE TIME STEP              132:        0.44982E+02

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


 INSTANT    0.133000000E+02   TIME STEP NUMBER             133
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.477446003E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29342E+02 0.12747E+02
   Friction velocity        uet   :  0.13611E-02 0.25263E+01
   Friction velocity        uk    :  0.22037E-01 0.28582E+01
   Dimensionless distance   yplus :  0.11416E+00 0.25844E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        490
   Nb of faces within the viscous sub-layer     :       1140
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29859E+04    1829   0.48187E-02   0.71771E+00 
c  VelocityY    0.29859E+04    1829   0.48187E-02   0.00000E+00 
c  VelocityZ    0.29859E+04    1829   0.48187E-02   0.00000E+00 
c  Pressure     0.40797E+00    7085   0.35383E-01   0.19021E+00 
c  k            0.25695E+04    1483   0.25536E-03   0.78994E+01 
c  omega        0.16128E+09     109   0.18172E-04   0.30601E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2426e-05                         45526


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.40914         0.29578      0.00037256     -9.3276e-07
v  Velocity[Y]                 -17.258          29.799          6.5681          20.053
v  Velocity[Z]                 -27.293           27.86        0.025051       -0.029285
v  ǁVelocityǁ                 0.014781           31.97          10.343          20.319
v  Pressure                    -342.63          343.05          -24.59          31.545
v  k                        4.8452e-08          82.014          3.7404          1.2344
v  omega                    7.8244e-14      8.5489e+07          9449.6          12.328
v  turbulent_viscosity      8.4391e-15          1.3582        0.015217        0.054044
v  CourantNb                  0.013051          2505.9          42.712          1.3811
v  FourierNb                 0.0094079           13989          82.208         0.35376
v  total_pressure           1.0098e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14758        0.010762        0.045041


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0097           14033          124.92          1.7348


 TIME FOR THE TIME STEP              133:        0.44621E+02

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


 INSTANT    0.134000000E+02   TIME STEP NUMBER             134
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.377926183E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27164E+02 0.12848E+02
   Friction velocity        uet   :  0.77083E-03 0.26005E+01
   Friction velocity        uk    :  0.28731E-01 0.31108E+01
   Dimensionless distance   yplus :  0.14757E+00 0.26024E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        566
   Nb of faces within the viscous sub-layer     :       1133
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29873E+04    1748   0.47796E-02   0.72649E+00 
c  VelocityY    0.29873E+04    1748   0.47796E-02   0.00000E+00 
c  VelocityZ    0.29873E+04    1748   0.47796E-02   0.00000E+00 
c  Pressure     0.38693E+00    6949   0.30730E-01   0.18062E+00 
c  k            0.27119E+04    1419   0.26379E-03   0.82313E+01 
c  omega        0.43103E+08     319   0.33775E-04   0.98318E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.1246e-05                             2
a  omega          
a  Local Time Step      1.1269e-05                         45498


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.51581         0.34714      0.00010355     -1.3529e-06
v  Velocity[Y]                 -15.895           30.46          6.6543          20.053
v  Velocity[Z]                 -27.028          27.932        0.055626       -0.031993
v  ǁVelocityǁ                  0.01745          31.897          10.322          20.316
v  Pressure                    -340.72          344.98         -25.244          31.685
v  k                        2.7493e-08           86.26          3.7321          1.2759
v  omega                    4.7854e-14      4.3324e+07          8729.3          12.236
v  turbulent_viscosity      2.6133e-14          1.4453        0.015451        0.055993
v  CourantNb                  0.065321          2308.6          42.922           1.381
v  FourierNb                 0.0095776           14338           83.54         0.36254
v  total_pressure           1.0098e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01          0.1481        0.010763        0.045007


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0102           14385          126.46          1.7436


 TIME FOR THE TIME STEP              134:        0.44343E+02

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


 INSTANT    0.135000000E+02   TIME STEP NUMBER             135
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.447820529E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27333E+02 0.14321E+02
   Friction velocity        uet   :  0.29832E-02 0.27027E+01
   Friction velocity        uk    :  0.10069E-01 0.30821E+01
   Dimensionless distance   yplus :  0.12752E+00 0.28313E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        537
   Nb of faces within the viscous sub-layer     :       1136
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29888E+04    1632   0.50084E-02   0.73080E+00 
c  VelocityY    0.29888E+04    1632   0.50084E-02   0.00000E+00 
c  VelocityZ    0.29888E+04    1632   0.50084E-02   0.00000E+00 
c  Pressure     0.38437E+00    6942   0.29171E-01   0.17834E+00 
c  k            0.28621E+04    1153   0.25590E-03   0.85427E+01 
c  omega        0.16127E+08     319   0.44358E-04   0.32459E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00027632                             1
a  omega          
a  Local Time Step      1.2023e-05                         45507


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.63215         0.43462     -0.00016092     -2.5854e-06
v  Velocity[Y]                  -14.45          30.511          6.7058          20.053
v  Velocity[Z]                 -27.205          28.077        0.087742       -0.034234
v  ǁVelocityǁ                 0.024103          31.808          10.301          20.313
v  Pressure                    -333.56          346.11         -25.647          31.325
v  k                        2.3003e-09          90.046          3.6941          1.3181
v  omega                     2.859e-14      2.2821e+07          8375.7          12.163
v  turbulent_viscosity      3.1189e-15          1.5321        0.015672        0.058008
v  CourantNb                  0.032486          2320.9            43.1           1.381
v  FourierNb                 0.0097359           14517          84.632         0.37175
v  total_pressure           1.0099e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14854        0.010764        0.044983


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93316           14567          127.73          1.7528


 TIME FOR THE TIME STEP              135:        0.42252E+02

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


 INSTANT    0.136000000E+02   TIME STEP NUMBER             136
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.274510855E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28675E+02 0.13073E+02
   Friction velocity        uet   :  0.13638E-02 0.26127E+01
   Friction velocity        uk    :  0.27146E-01 0.31561E+01
   Dimensionless distance   yplus :  0.94854E-01 0.34437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1058
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29903E+04    1514   0.50214E-02   0.73575E+00 
c  VelocityY    0.29903E+04    1514   0.50214E-02   0.00000E+00 
c  VelocityZ    0.29903E+04    1514   0.50214E-02   0.00000E+00 
c  Pressure     0.42184E+00    6938   0.31117E-01   0.19404E+00 
c  k            0.30202E+04    1092   0.24579E-03   0.85707E+01 
c  omega        0.11003E+08     234   0.43125E-04   0.21002E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028601                             2
a  omega                    -46740                             2
a  Local Time Step      1.2757e-05                         45534


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.74645         0.51773     -0.00031143     -1.9527e-06
v  Velocity[Y]                 -14.434          31.178          6.7101          20.054
v  Velocity[Z]                  -27.47          27.955         0.10799       -0.036133
v  ǁVelocityǁ                 0.011484          31.887            10.3          20.311
v  Pressure                    -312.85          346.26         -25.927          31.042
v  k                        2.6351e-08          93.613          3.6569          1.3609
v  omega                    1.6843e-14      1.3624e+07          8363.1          12.141
v  turbulent_viscosity      2.1731e-16          1.6173        0.015863        0.060092
v  CourantNb                  0.034402          2313.5          43.125          1.3809
v  FourierNb                 0.0098841           14644          83.741         0.38027
v  total_pressure           1.0101e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14937        0.010764        0.044956


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0104           14701          126.87          1.7612


 TIME FOR THE TIME STEP              136:        0.40575E+02

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


 INSTANT    0.137000000E+02   TIME STEP NUMBER             137
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.257487461E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28275E+02 0.20081E+02
   Friction velocity        uet   :  0.37456E-03 0.26368E+01
   Friction velocity        uk    :  0.14452E-01 0.30621E+01
   Dimensionless distance   yplus :  0.66176E-01 0.35144E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        479
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29918E+04    1355   0.49360E-02   0.73745E+00 
c  VelocityY    0.29918E+04    1355   0.49360E-02   0.00000E+00 
c  VelocityZ    0.29918E+04    1355   0.49360E-02   0.00000E+00 
c  Pressure     0.40140E+00    6937   0.29671E-01   0.18560E+00 
c  k            0.31860E+04    1387   0.25025E-03   0.87817E+01 
c  omega        0.13144E+08     255   0.21618E-04   0.30714E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00022441                             2
a  omega                   -8036.8                             1
a  Local Time Step      1.2813e-05                         45557


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.83499         0.58745     -0.00048363     -1.6249e-06
v  Velocity[Y]                 -14.498          29.596          6.7039          20.053
v  Velocity[Z]                 -28.159          28.024         0.12624       -0.037814
v  ǁVelocityǁ                0.0027975          31.451          10.297          20.307
v  Pressure                    -304.87           346.4         -26.031          30.783
v  k                        5.0026e-07          96.748          3.6053          1.4042
v  omega                    9.9363e-15      1.8807e+07          8181.1          12.111
v  turbulent_viscosity      3.8168e-15          1.6975        0.016052        0.062248
v  CourantNb                  0.036955            2287          43.163          1.3809
v  FourierNb                  0.010021           14662          83.801         0.38949
v  total_pressure           1.0102e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010764        0.044943


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14725          126.96          1.7704


 TIME FOR THE TIME STEP              137:        0.39513E+02

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


 INSTANT    0.138000000E+02   TIME STEP NUMBER             138
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.918864650E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28579E+02 0.18835E+02
   Friction velocity        uet   :  0.12342E-02 0.24375E+01
   Friction velocity        uk    :  0.17404E-01 0.28962E+01
   Dimensionless distance   yplus :  0.86241E-01 0.28175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1076
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29932E+04    1648   0.47656E-02   0.73654E+00 
c  VelocityY    0.29932E+04    1648   0.47656E-02   0.00000E+00 
c  VelocityZ    0.29932E+04    1648   0.47656E-02   0.00000E+00 
c  Pressure     0.40625E+00    6668   0.27707E-01   0.18904E+00 
c  k            0.33547E+04    1458   0.24412E-03   0.89634E+01 
c  omega        0.12633E+08     237   0.31262E-03   0.40317E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2749e-05                         45578


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86693         0.62123     -0.00064368     -1.7173e-06
v  Velocity[Y]                 -14.498          29.605          6.7142          20.053
v  Velocity[Z]                 -28.783          27.809         0.13744       -0.039225
v  ǁVelocityǁ                 0.011841          34.329          10.311          20.304
v  Pressure                    -298.79          346.33         -25.824          30.855
v  k                         1.219e-06          99.227          3.5888          1.4482
v  omega                    5.9526e-15      1.3927e+08          9116.7          12.151
v  turbulent_viscosity      7.2464e-14          1.7784        0.016239        0.064479
v  CourantNb                  0.016738            2258          43.262          1.3808
v  FourierNb                  0.010146           14616          83.929         0.39894
v  total_pressure           1.0103e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010762        0.044937


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14679          127.19          1.7797


 TIME FOR THE TIME STEP              138:        0.42014E+02

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


 INSTANT    0.139000000E+02   TIME STEP NUMBER             139
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.473369801E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27802E+02 0.16421E+02
   Friction velocity        uet   :  0.78656E-03 0.28613E+01
   Friction velocity        uk    :  0.18189E-01 0.31589E+01
   Dimensionless distance   yplus :  0.10396E+00 0.25178E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1088
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29948E+04    1705   0.47527E-02   0.72972E+00 
c  VelocityY    0.29948E+04    1705   0.47527E-02   0.00000E+00 
c  VelocityZ    0.29948E+04    1705   0.47527E-02   0.00000E+00 
c  Pressure     0.38787E+00    6937   0.29616E-01   0.18019E+00 
c  k            0.35244E+04    1472   0.23219E-03   0.91126E+01 
c  omega        0.82810E+08      95   0.21720E-04   0.15887E+09 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.258e+05                             1
a  Local Time Step      1.3192e-05                         45550


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8301         0.63574     -0.00080791     -1.1845e-06
v  Velocity[Y]                 -14.551          29.544          6.7407          20.053
v  Velocity[Z]                 -30.514          27.947         0.16101       -0.039689
v  ǁVelocityǁ                 0.016433           35.46           10.37            20.3
v  Pressure                     -317.5          345.52         -25.578          30.931
v  k                        2.2111e-07          100.92          3.5908          1.4925
v  omega                    3.6412e-15      6.9975e+07            8970          12.136
v  turbulent_viscosity      1.7649e-13          1.8542        0.016433        0.066788
v  CourantNb                  0.040415          2228.8          43.248          1.3803
v  FourierNb                  0.010262           14454          82.857         0.40836
v  total_pressure           1.0101e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010762        0.044898


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94213           14522           126.1          1.7886


 TIME FOR THE TIME STEP              139:        0.43176E+02

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


 INSTANT    0.140000000E+02   TIME STEP NUMBER             140
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.186504644E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.27911E+02 0.13239E+02
   Friction velocity        uet   :  0.13463E-02 0.29740E+01
   Friction velocity        uk    :  0.25038E-01 0.27824E+01
   Dimensionless distance   yplus :  0.12191E+00 0.24431E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        565
   Nb of faces within the viscous sub-layer     :       1124
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29964E+04    1622   0.47671E-02   0.72524E+00 
c  VelocityY    0.29964E+04    1622   0.47671E-02   0.00000E+00 
c  VelocityZ    0.29964E+04    1622   0.47671E-02   0.00000E+00 
c  Pressure     0.38961E+00    6956   0.31661E-01   0.18052E+00 
c  k            0.36935E+04    1451   0.22674E-03   0.92954E+01 
c  omega        0.24800E+08     173   0.42420E-04   0.90173E+08 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.3506e-05                         45524


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.76737         0.66099      -0.0010127     -8.7103e-07
v  Velocity[Y]                 -14.488          29.473          6.7816          20.054
v  Velocity[Z]                 -30.402          28.072         0.20702       -0.039529
v  ǁVelocityǁ                 0.010773           33.99          10.435          20.297
v  Pressure                    -353.19          343.99          -25.77          31.006
v  k                        1.0328e-07          102.12          3.5985           1.537
v  omega                    2.2498e-15      3.5683e+07          8704.8          12.129
v  turbulent_viscosity      1.2129e-13          1.9227        0.016633        0.069177
v  CourantNb                  0.018479            2198          43.425          1.3797
v  FourierNb                  0.010371           14010          81.483         0.41864
v  total_pressure           1.0097e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14905        0.010762        0.044857


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

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9341           14080          124.91          1.7983


 TIME FOR THE TIME STEP              140:        0.42882E+02

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


 INSTANT    0.141000000E+02   TIME STEP NUMBER             141
 ============================================================= 




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

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.324694755E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29301E+02 0.13535E+02
   Friction velocity        uet   :  0.58905E-03 0.27988E+01
   Friction velocity        uk    :  0.20257E-01 0.29002E+01
   Dimensionless distance   yplus :  0.11939E+00 0.24001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        515
   Nb of faces within the viscous sub-layer     :       1132
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29980E+04    1512   0.49307E-02   0.72130E+00 
c  VelocityY    0.29980E+04    1512   0.49307E-02   0.00000E+00 
c  VelocityZ    0.29980E+04    1512   0.49307E-02   0.00000E+00 
c  Pressure     0.39475E+00    6949   0.32074E-01   0.18233E+00 
c  k            0.38569E+04    1347   0.21839E-03   0.94488E+01 
c  omega        0.15490E+08     227   0.81259E-03   0.10200E+12 
---------------------------------------------------------------
  
  

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

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00056772                             2
a  omega                    -24980                             1
a  Local Time Step      1.3403e-05                         45533


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

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.5844         0.67774      -0.0012422     -6.5194e-08
v  Velocity[Y]                 -17.267          29.436          6.8068          20.054
v  Velocity[Z]                 -30.781          28.155         0.27652       -0.038944
v  ǁVelocityǁ                 0.011694          32.253          10.467          20.293
v  Pressure                    -366.72          342.39         -26.585          30.916
v  k                        2.2886e-08          103.24          3.5874          1.5816
v  omega                     1.388e-15      1.6063e+09           13141          12.848
v  turbulent_viscosity      7.0665e-15          1.9807        0.016824        0.071647
v  CourantNb                  0.055993          2366.9          43.652          1.3792
v  FourierNb                  0.010473           13645          80.703         0.42926
v  total_pressure           1.0096e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14751        0.010761        0.044842


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9506           13715          124.36          1.8085


 TIME FOR THE TIME STEP              141:        0.41224E+02

===============================================================


 INSTANT    0.142000000E+02   TIME STEP NUMBER             142
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.553146627E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29814E+02 0.13814E+02
   Friction velocity        uet   :  0.17797E-02 0.27754E+01
   Friction velocity        uk    :  0.16859E-01 0.28126E+01
   Dimensionless distance   yplus :  0.13136E+00 0.23688E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29997E+04    1330   0.47876E-02   0.69240E+00 
c  VelocityY    0.29997E+04    1330   0.47876E-02   0.00000E+00 
c  VelocityZ    0.29997E+04    1330   0.47876E-02   0.00000E+00 
c  Pressure     0.39940E+00    6950   0.33294E-01   0.18542E+00 
c  k            0.40123E+04    1169   0.20915E-03   0.96329E+01 
c  omega        0.30506E+11       8   0.17187E-06   0.25522E+11 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018938                             2
a  omega                    -34966                             1
a  Local Time Step      1.2893e-05                         45506


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.34995         0.68832      -0.0013882      8.6531e-07
v  Velocity[Y]                 -21.811          29.402          6.7619          20.055
v  Velocity[Z]                 -30.405          28.366         0.35848        -0.03796
v  ǁVelocityǁ                0.0054577          31.169          10.427          20.289
v  Pressure                    -362.82          341.01          -28.02          30.907
v  k                        4.4361e-08          103.48          3.5698           1.626
v  omega                    8.5013e-16      8.0313e+08           10766          12.477
v  turbulent_viscosity       4.102e-15          2.0413        0.016981          0.0742
v  CourantNb                   0.05805          2140.9           43.83          1.3789
v  FourierNb                  0.010568           13416          80.672         0.44043
v  total_pressure           1.0096e+05      1.0167e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14754         0.01076        0.044828


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           13480           124.5          1.8193


 TIME FOR THE TIME STEP              142:        0.38529E+02

===============================================================


 INSTANT    0.143000000E+02   TIME STEP NUMBER             143
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.445433832E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30300E+02 0.15031E+02
   Friction velocity        uet   :  0.12746E-02 0.26627E+01
   Friction velocity        uk    :  0.10263E-01 0.28201E+01
   Dimensionless distance   yplus :  0.62106E-01 0.23698E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1154
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30013E+04    1296   0.48250E-02   0.65483E+00 
c  VelocityY    0.30013E+04    1296   0.48250E-02   0.00000E+00 
c  VelocityZ    0.30013E+04    1296   0.48250E-02   0.00000E+00 
c  Pressure     0.42274E+00    6968   0.33456E-01   0.19773E+00 
c  k            0.41452E+04     875   0.20497E-03   0.99199E+01 
c  omega        0.76263E+10      21   0.34162E-06   0.64103E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -70091                             1
a  Local Time Step      1.2413e-05                         45487


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.29822         0.69847      -0.0014804      9.9881e-07
v  Velocity[Y]                  -31.27          29.307          6.6556          20.054
v  Velocity[Z]                 -27.298          28.423         0.40365       -0.036262
v  ǁVelocityǁ                 0.013567           31.76          10.382          20.284
v  Pressure                    -346.04          339.47         -29.973          30.362
v  k                        9.1724e-09          103.43          3.5901          1.6701
v  omega                    5.1369e-16      4.0156e+08          9512.2          12.286
v  turbulent_viscosity      1.0367e-14          2.0897        0.017093        0.076772
v  CourantNb                  0.043317          2125.7          43.658          1.3784
v  FourierNb                  0.010656           13043          80.067         0.45141
v  total_pressure           1.0098e+05      1.0166e+05       1.013e+05      1.0136e+05
v  Local Time Step                0.01         0.14706        0.010759        0.044835


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99951           13101          123.72          1.8298


 TIME FOR THE TIME STEP              143:        0.37659E+02

===============================================================


 INSTANT    0.144000000E+02   TIME STEP NUMBER             144
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.310164407E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29674E+02 0.20429E+02
   Friction velocity        uet   :  0.11306E-02 0.27507E+01
   Friction velocity        uk    :  0.15109E-01 0.30037E+01
   Dimensionless distance   yplus :  0.10134E+00 0.23972E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        401
   Nb of faces within the viscous sub-layer     :       1123
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30027E+04    1346   0.48874E-02   0.63362E+00 
c  VelocityY    0.30027E+04    1346   0.48874E-02   0.00000E+00 
c  VelocityZ    0.30027E+04    1346   0.48874E-02   0.00000E+00 
c  Pressure     0.40992E+00    6709   0.33258E-01   0.19171E+00 
c  k            0.42682E+04     915   0.19670E-03   0.10147E+02 
c  omega        0.19065E+10      44   0.70861E-06   0.16620E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0778e+05                             2
a  Local Time Step      1.2164e-05                         45441


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39786         0.70056      -0.0014155      7.4699e-07
v  Velocity[Y]                 -29.487          29.267            6.57          20.054
v  Velocity[Z]                 -27.115           28.47         0.41833       -0.034248
v  ǁVelocityǁ                0.0068628          34.926          10.339           20.28
v  Pressure                    -348.76          337.17         -32.687          29.979
v  k                        4.2501e-07          102.38          3.6501          1.7142
v  omega                    3.0652e-16      2.0077e+08            8927          12.207
v  turbulent_viscosity      2.7156e-14          2.1301        0.017202        0.079483
v  CourantNb                  0.052569          2120.2          43.602          1.3778
v  FourierNb                  0.010738           12886          79.873          0.4635
v  total_pressure           1.0098e+05      1.0166e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14683        0.010758        0.044808


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0008           12935          123.47          1.8413


 TIME FOR THE TIME STEP              144:        0.37202E+02

===============================================================


 INSTANT    0.145000000E+02   TIME STEP NUMBER             145
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.317570850E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44485E+02 0.13748E+02
   Friction velocity        uet   :  0.75813E-03 0.30428E+01
   Friction velocity        uk    :  0.20436E-01 0.39303E+01
   Dimensionless distance   yplus :  0.11024E+00 0.31080E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :       1080
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30041E+04    1590   0.46280E-02   0.63134E+00 
c  VelocityY    0.30041E+04    1590   0.46280E-02   0.00000E+00 
c  VelocityZ    0.30041E+04    1590   0.46280E-02   0.00000E+00 
c  Pressure     0.36584E+00    7072   0.34342E-01   0.17017E+00 
c  k            0.43777E+04    1148   0.18503E-03   0.10288E+02 
c  omega        0.47678E+09     107   0.19243E-05   0.53379E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -2.828e-05                             2
a  omega               -2.3838e+05                             1
a  Local Time Step       1.236e-05                         45353


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39855         0.69639      -0.0011951      -5.069e-07
v  Velocity[Y]                 -32.514          29.217          6.5402          20.054
v  Velocity[Z]                 -27.238          28.573         0.41238       -0.031707
v  ǁVelocityǁ                 0.003825           33.19          10.304          20.275
v  Pressure                    -353.59          335.65          -35.35          29.761
v  k                        5.0799e-09          101.42          3.6772          1.7586
v  omega                       1.8e-16      1.0038e+08            8739          12.183
v  turbulent_viscosity      1.4771e-13          2.1635         0.01731        0.082288
v  CourantNb                  0.043173          2131.6          43.603          1.3774
v  FourierNb                  0.010811           12932          81.078         0.47645
v  total_pressure           1.0097e+05      1.0166e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14844        0.010757        0.044792


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           12979          124.68          1.8539


 TIME FOR THE TIME STEP              145:        0.41536E+02

===============================================================


 INSTANT    0.146000000E+02   TIME STEP NUMBER             146
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.449442589E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29270E+02 0.12849E+02
   Friction velocity        uet   :  0.20000E-02 0.32569E+01
   Friction velocity        uk    :  0.15252E-01 0.29248E+01
   Dimensionless distance   yplus :  0.88959E-01 0.24585E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        417
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30053E+04    1651   0.45992E-02   0.62531E+00 
c  VelocityY    0.30053E+04    1651   0.45992E-02   0.00000E+00 
c  VelocityZ    0.30053E+04    1651   0.45992E-02   0.00000E+00 
c  Pressure     0.39863E+00    7073   0.34450E-01   0.18483E+00 
c  k            0.44741E+04    1251   0.17214E-03   0.10495E+02 
c  omega        0.12146E+09     164   0.10499E-04   0.23962E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.3012e-05                             2
a  omega          
a  Local Time Step      1.2146e-05                         45224


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39836         0.69556     -0.00070428     -1.9804e-06
v  Velocity[Y]                 -17.391           29.16          6.5588          20.054
v  Velocity[Z]                 -27.301          28.759         0.38594       -0.029001
v  ǁVelocityǁ                 0.011001          31.794          10.278          20.271
v  Pressure                     -356.5          333.52         -37.901          29.689
v  k                        6.3298e-10          99.877          3.6834          1.8032
v  omega                    1.0522e-16      5.0465e+07          8845.8          12.186
v  turbulent_viscosity       2.586e-15          2.2012        0.017407        0.085182
v  CourantNb                  0.040012          2787.6          43.802          1.3771
v  FourierNb                  0.010877           13138           81.45         0.48959
v  total_pressure           1.0097e+05      1.0166e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14853        0.010757        0.044746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           13185          125.25          1.8667


 TIME FOR THE TIME STEP              146:        0.42575E+02

===============================================================


 INSTANT    0.147000000E+02   TIME STEP NUMBER             147
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.127199091E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28937E+02 0.12944E+02
   Friction velocity        uet   :  0.57438E-03 0.24461E+01
   Friction velocity        uk    :  0.21721E-01 0.28643E+01
   Dimensionless distance   yplus :  0.11919E+00 0.24901E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :       1102
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30064E+04    1670   0.45781E-02   0.62165E+00 
c  VelocityY    0.30064E+04    1670   0.45781E-02   0.00000E+00 
c  VelocityZ    0.30064E+04    1670   0.45781E-02   0.00000E+00 
c  Pressure     0.40559E+00    7095   0.33504E-01   0.18761E+00 
c  k            0.45594E+04    1273   0.15906E-03   0.10708E+02 
c  omega        0.34747E+08     199   0.58593E-04   0.25004E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012038                             2
a  omega          
a  Local Time Step      1.1631e-05                         45169


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.38673         0.77766      -0.0001281     -3.2934e-06
v  Velocity[Y]                 -16.962          29.551          6.6091          20.054
v  Velocity[Z]                 -27.341          28.759         0.34259       -0.025862
v  ǁVelocityǁ                0.0079608          32.158          10.271          20.267
v  Pressure                    -357.12          332.53         -39.664          29.401
v  k                        2.4048e-09          97.369          3.7016          1.8481
v  omega                    6.1571e-17      4.7331e+07            9247          12.206
v  turbulent_viscosity      9.9436e-16          2.2232          0.0175        0.088169
v  CourantNb                  0.017433          2204.6          43.601          1.3766
v  FourierNb                  0.010936           13442          81.122           0.503
v  total_pressure           1.0097e+05      1.0166e+05      1.0129e+05      1.0135e+05
v  Local Time Step                0.01         0.14885        0.010757        0.044711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           13493          124.72          1.8796


 TIME FOR THE TIME STEP              147:        0.43075E+02

===============================================================


 INSTANT    0.148000000E+02   TIME STEP NUMBER             148
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.621034333E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29422E+02 0.13139E+02
   Friction velocity        uet   :  0.81811E-03 0.25735E+01
   Friction velocity        uk    :  0.16650E-01 0.28006E+01
   Dimensionless distance   yplus :  0.14942E+00 0.26568E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        546
   Nb of faces within the viscous sub-layer     :       1121
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30074E+04    1764   0.48201E-02   0.63385E+00 
c  VelocityY    0.30074E+04    1764   0.48201E-02   0.00000E+00 
c  VelocityZ    0.30074E+04    1764   0.48201E-02   0.00000E+00 
c  Pressure     0.40366E+00    7010   0.33231E-01   0.18620E+00 
c  k            0.46347E+04    1285   0.15039E-03   0.11085E+02 
c  omega        0.23947E+08     193   0.12401E-03   0.33033E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017038                             2
a  omega          
a  Local Time Step      1.1932e-05                         45111


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.37634         0.86627      0.00029455     -5.5898e-06
v  Velocity[Y]                 -17.761           30.11          6.6698          20.054
v  Velocity[Z]                 -27.362          31.123         0.28507        -0.02227
v  ǁVelocityǁ                 0.012834          32.081          10.283          20.262
v  Pressure                    -354.37          328.23         -40.899          29.076
v  k                        3.2275e-09          95.493          3.7081          1.8935
v  omega                    3.5753e-17      8.4101e+07          9342.8          12.176
v  turbulent_viscosity      2.6653e-15          2.2411        0.017583        0.091251
v  CourantNb                  0.048108          2241.6          43.255          1.3761
v  FourierNb                  0.010988           13743          81.258         0.51672
v  total_pressure           1.0097e+05      1.0165e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14891        0.010756        0.044674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           13796          124.51          1.8928


 TIME FOR THE TIME STEP              148:        0.43746E+02

===============================================================


 INSTANT    0.149000000E+02   TIME STEP NUMBER             149
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.783808555E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28983E+02 0.17436E+02
   Friction velocity        uet   :  0.72779E-03 0.25790E+01
   Friction velocity        uk    :  0.30297E-01 0.29043E+01
   Dimensionless distance   yplus :  0.12407E+00 0.30848E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :       1171
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30081E+04    1804   0.47385E-02   0.65669E+00 
c  VelocityY    0.30081E+04    1804   0.47385E-02   0.00000E+00 
c  VelocityZ    0.30081E+04    1804   0.47385E-02   0.00000E+00 
c  Pressure     0.45613E+00    6939   0.29694E-01   0.21096E+00 
c  k            0.47011E+04    1277   0.13964E-03   0.11408E+02 
c  omega        0.42922E+09      82   0.30420E-05   0.92160E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015953                             2
a  omega          
a  Local Time Step      1.1752e-05                         45049


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.42321         0.89588      0.00044492     -7.1862e-06
v  Velocity[Y]                  -15.48          29.929          6.7411          20.054
v  Velocity[Z]                 -27.456          28.708         0.22661       -0.018316
v  ǁVelocityǁ                0.0075518          31.968          10.324          20.258
v  Pressure                    -344.57          325.86         -42.167          28.694
v  k                        9.1145e-09          92.857          3.6928          1.9393
v  omega                    2.0813e-17      4.2712e+07          8769.3          12.084
v  turbulent_viscosity      1.7384e-15          2.2605        0.017642        0.094429
v  CourantNb                  0.026042          2269.2          43.092          1.3756
v  FourierNb                  0.011035           14080          81.501         0.53065
v  total_pressure           1.0098e+05      1.0165e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14947        0.010756        0.044637


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           14136          124.59          1.9063


 TIME FOR THE TIME STEP              149:        0.43513E+02

===============================================================


 INSTANT    0.150000000E+02   TIME STEP NUMBER             150
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.293762607E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28825E+02 0.17009E+02
   Friction velocity        uet   :  0.15671E-03 0.24584E+01
   Friction velocity        uk    :  0.18221E-01 0.31373E+01
   Dimensionless distance   yplus :  0.13592E+00 0.39433E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        540
   Nb of faces within the viscous sub-layer     :       1144
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30086E+04    1829   0.47786E-02   0.68132E+00 
c  VelocityY    0.30086E+04    1829   0.47786E-02   0.00000E+00 
c  VelocityZ    0.30086E+04    1829   0.47786E-02   0.00000E+00 
c  Pressure     0.41788E+00    6941   0.27915E-01   0.19351E+00 
c  k            0.47610E+04    1256   0.13010E-03   0.11688E+02 
c  omega        0.15056E+08     308   0.50668E-04   0.32119E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00019948                             2
a  omega               -1.7721e+05                             3
a  Local Time Step      1.1524e-05                         45051


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.39093         0.86711      0.00038254     -8.3674e-06
v  Velocity[Y]                 -14.983          31.806          6.7886          20.054
v  Velocity[Z]                 -27.532           28.64         0.17775       -0.013909
v  ǁVelocityǁ                 0.011766          32.791           10.37          20.253
v  Pressure                    -346.36           324.8         -43.038          28.393
v  k                           7.8e-10          89.756          3.6597          1.9857
v  omega                    1.2251e-17      2.2736e+07          8486.5          12.017
v  turbulent_viscosity      2.7984e-15           2.262        0.017675        0.097702
v  CourantNb                  0.026445          2289.4          43.332          1.3755
v  FourierNb                  0.011077           14547          80.424         0.54454
v  total_pressure           1.0098e+05      1.0165e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14947        0.010756         0.04462


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           14606          123.76          1.9201


 TIME FOR THE TIME STEP              150:        0.43800E+02

===============================================================


 INSTANT    0.151000000E+02   TIME STEP NUMBER             151
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.185729576E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29323E+02 0.20630E+02
   Friction velocity        uet   :  0.15172E-02 0.27849E+01
   Friction velocity        uk    :  0.18981E-01 0.31751E+01
   Dimensionless distance   yplus :  0.90339E-01 0.32786E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :       1149
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30091E+04    1812   0.47604E-02   0.70016E+00 
c  VelocityY    0.30091E+04    1812   0.47604E-02   0.00000E+00 
c  VelocityZ    0.30091E+04    1812   0.47604E-02   0.00000E+00 
c  Pressure     0.39533E+00    6840   0.26591E-01   0.18310E+00 
c  k            0.48154E+04    1204   0.12238E-03   0.11956E+02 
c  omega        0.11297E+08     214   0.36216E-03   0.53984E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6349e-05                             1
a  omega               -1.9361e+05                             2
a  Local Time Step      1.2666e-05                         45056


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.4066         0.78536      0.00016282     -7.3127e-06
v  Velocity[Y]                 -14.677          37.559          6.8405          20.055
v  Velocity[Z]                 -27.587           28.59         0.15184       -0.009119
v  ǁVelocityǁ                0.0084139          38.576          10.412           20.25
v  Pressure                    -346.36          325.39         -43.476          28.308
v  k                        6.2453e-10           87.28          3.6513          2.0328
v  omega                      7.34e-18      1.6532e+08            9515          12.085
v  turbulent_viscosity      3.6564e-16          2.2744        0.017699         0.10107
v  CourantNb                  0.010719          2298.9          43.609          1.3755
v  FourierNb                  0.011113           14816          79.821         0.55828
v  total_pressure           1.0098e+05      1.0165e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14829        0.010756        0.044558


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8115           14878          123.43          1.9338


 TIME FOR THE TIME STEP              151:        0.43426E+02

===============================================================


 INSTANT    0.152000000E+02   TIME STEP NUMBER             152
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.177324801E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29887E+02 0.22461E+02
   Friction velocity        uet   :  0.18845E-02 0.35193E+01
   Friction velocity        uk    :  0.19864E-01 0.30693E+01
   Dimensionless distance   yplus :  0.48212E-01 0.27057E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :       1075
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30092E+04    1782   0.46291E-02   0.71678E+00 
c  VelocityY    0.30092E+04    1782   0.46291E-02   0.00000E+00 
c  VelocityZ    0.30092E+04    1782   0.46291E-02   0.00000E+00 
c  Pressure     0.41183E+00    6876   0.28275E-01   0.19053E+00 
c  k            0.48656E+04    1198   0.11384E-03   0.12241E+02 
c  omega        0.11091E+09     139   0.33239E-04   0.51196E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0004383                             5
a  omega                    -43202                             1
a  Local Time Step      1.2212e-05                         44977


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.4747         0.65941     -0.00012592     -6.4659e-06
v  Velocity[Y]                 -14.869          36.844          6.9038          20.055
v  Velocity[Z]                 -29.389          28.441          0.1307      -0.0043493
v  ǁVelocityǁ                 0.010885          37.396          10.458          20.246
v  Pressure                     -344.9          327.65           -43.1           28.19
v  k                        2.1456e-09          84.054           3.673          2.0805
v  omega                    4.4865e-18       1.537e+08          9280.8          12.037
v  turbulent_viscosity      1.3408e-15          2.2764        0.017742         0.10453
v  CourantNb                  0.025461          2309.6          43.979          1.3754
v  FourierNb                  0.011143           15092          80.363         0.57288
v  total_pressure           1.0098e+05      1.0165e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14805        0.010757        0.044575


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.006           15156          124.34          1.9483


 TIME FOR THE TIME STEP              152:        0.43652E+02

===============================================================


 INSTANT    0.153000000E+02   TIME STEP NUMBER             153
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.383382464E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30799E+02 0.17539E+02
   Friction velocity        uet   :  0.22475E-02 0.34471E+01
   Friction velocity        uk    :  0.19979E-01 0.28863E+01
   Dimensionless distance   yplus :  0.81917E-01 0.25617E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        449
   Nb of faces within the viscous sub-layer     :       1049
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30093E+04    1767   0.47256E-02   0.72938E+00 
c  VelocityY    0.30093E+04    1767   0.47256E-02   0.00000E+00 
c  VelocityZ    0.30093E+04    1767   0.47256E-02   0.00000E+00 
c  Pressure     0.38991E+00    6982   0.32635E-01   0.18057E+00 
c  k            0.49130E+04    1172   0.10746E-03   0.12485E+02 
c  omega        0.11461E+09      92   0.15298E-04   0.13739E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010797                            13
a  omega                    -47547                             1
a  Local Time Step      1.2082e-05                         44925


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.58743         0.49303     -0.00044031     -5.4778e-06
v  Velocity[Y]                 -14.862          36.305            6.97          20.055
v  Velocity[Z]                 -30.998          28.742         0.13484      0.00068167
v  ǁVelocityǁ                0.0044292          36.782          10.534          20.243
v  Pressure                    -346.08          330.75          -42.46          28.474
v  k                         9.738e-10          81.051           3.688          2.1287
v  omega                    2.7784e-18      7.7047e+07          8616.4          11.993
v  turbulent_viscosity      8.6852e-15          2.2704        0.017814         0.10808
v  CourantNb                  0.037571          2473.8          44.111           1.375
v  FourierNb                  0.011168           15321          81.223         0.58785
v  total_pressure           1.0098e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14838        0.010758         0.04457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15385          125.33          1.9629


 TIME FOR THE TIME STEP              153:        0.43329E+02

===============================================================


 INSTANT    0.154000000E+02   TIME STEP NUMBER             154
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.692594356E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30344E+02 0.12992E+02
   Friction velocity        uet   :  0.77790E-03 0.33858E+01
   Friction velocity        uk    :  0.24685E-01 0.30904E+01
   Dimensionless distance   yplus :  0.85242E-01 0.25625E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30093E+04    1829   0.44622E-02   0.73782E+00 
c  VelocityY    0.30093E+04    1829   0.44622E-02   0.00000E+00 
c  VelocityZ    0.30093E+04    1829   0.44622E-02   0.00000E+00 
c  Pressure     0.41714E+00    7063   0.35626E-01   0.19464E+00 
c  k            0.49599E+04    1091   0.10124E-03   0.12644E+02 
c  omega        0.31110E+08     190   0.61843E-04   0.11160E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00033824                             9
a  omega                    -67188                             1
a  Local Time Step      1.2777e-05                         44812


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.72917         0.42129     -0.00073657     -3.8255e-06
v  Velocity[Y]                 -14.797          32.918          7.0263          20.055
v  Velocity[Z]                 -30.211          28.842         0.17417       0.0059959
v  ǁVelocityǁ                0.0049879          34.232          10.612           20.24
v  Pressure                    -372.53          333.76         -42.073          28.597
v  k                        3.0439e-10          78.232           3.694           2.177
v  omega                    1.7312e-18      6.7182e+07          8523.4          11.989
v  turbulent_viscosity       1.713e-16          2.2748        0.017875         0.11172
v  CourantNb                  0.012424          2761.7          44.281          1.3746
v  FourierNb                  0.011189           15494          82.201         0.60313
v  total_pressure           1.0095e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14792        0.010758        0.044558


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15557          126.48          1.9777


 TIME FOR THE TIME STEP              154:        0.44672E+02

===============================================================


 INSTANT    0.155000000E+02   TIME STEP NUMBER             155
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.127840234E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29604E+02 0.13473E+02
   Friction velocity        uet   :  0.87590E-03 0.32121E+01
   Friction velocity        uk    :  0.15635E-01 0.28300E+01
   Dimensionless distance   yplus :  0.82292E-01 0.25956E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30090E+04    1762   0.47439E-02   0.73638E+00 
c  VelocityY    0.30090E+04    1762   0.47439E-02   0.00000E+00 
c  VelocityZ    0.30090E+04    1762   0.47439E-02   0.00000E+00 
c  Pressure     0.36562E+00    7055   0.35127E-01   0.16909E+00 
c  k            0.50031E+04     930   0.96570E-04   0.12725E+02 
c  omega        0.23056E+08     141   0.38671E-04   0.42533E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00060901                            10
a  omega                    -55787                             1
a  Local Time Step      1.2716e-05                         44764


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88145         0.55402     -0.00098743     -2.1326e-06
v  Velocity[Y]                 -21.414          28.567          7.0386          20.054
v  Velocity[Z]                  -30.59           28.86         0.23202        0.011394
v  ǁVelocityǁ                 0.012801          31.961          10.645          20.236
v  Pressure                    -377.68          336.48         -42.287          28.243
v  k                        1.8524e-09          75.083          3.6923          2.2251
v  omega                    1.0781e-18      3.4399e+07          8327.6          11.996
v  turbulent_viscosity      1.0547e-16          2.2611          0.0179         0.11542
v  CourantNb                  0.038875          2719.8          44.529          1.3743
v  FourierNb                  0.011208           15610          82.466         0.61813
v  total_pressure           1.0095e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14916        0.010758        0.044601


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15665          126.99          1.9924


 TIME FOR THE TIME STEP              155:        0.43237E+02

===============================================================


 INSTANT    0.156000000E+02   TIME STEP NUMBER             156
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.434811666E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29367E+02 0.13487E+02
   Friction velocity        uet   :  0.44914E-04 0.27229E+01
   Friction velocity        uk    :  0.16728E-01 0.28058E+01
   Dimensionless distance   yplus :  0.14839E+00 0.26125E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30087E+04    1709   0.46365E-02   0.71773E+00 
c  VelocityY    0.30087E+04    1709   0.46365E-02   0.00000E+00 
c  VelocityZ    0.30087E+04    1709   0.46365E-02   0.00000E+00 
c  Pressure     0.40335E+00    7025   0.34170E-01   0.18663E+00 
c  k            0.50423E+04     745   0.93474E-04   0.12692E+02 
c  omega        0.12028E+08     188   0.64277E-04   0.39860E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -63758                             1
a  Local Time Step      1.2825e-05                         44735


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0281         0.68243      -0.0012432     -4.1831e-07
v  Velocity[Y]                 -27.663          28.438          6.9836          20.054
v  Velocity[Z]                 -30.093          28.725          0.2877        0.016629
v  ǁVelocityǁ                 0.014307          31.334          10.636          20.234
v  Pressure                    -365.94          338.81          -42.66          28.187
v  k                        2.4478e-08           72.16          3.7064          2.2727
v  omega                     6.658e-19      2.3722e+07          8384.3           12.02
v  turbulent_viscosity      1.2117e-15           2.261        0.017898         0.11919
v  CourantNb                   0.03132          2357.9          44.768          1.3741
v  FourierNb                  0.011217           15670          82.788          0.6336
v  total_pressure           1.0096e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14744        0.010758        0.044576


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15725          127.56          2.0077


 TIME FOR THE TIME STEP              156:        0.42133E+02

===============================================================


 INSTANT    0.157000000E+02   TIME STEP NUMBER             157
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.558613199E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29536E+02 0.19127E+02
   Friction velocity        uet   :  0.80482E-03 0.26322E+01
   Friction velocity        uk    :  0.24889E-01 0.30685E+01
   Dimensionless distance   yplus :  0.11561E+00 0.26504E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30083E+04    1814   0.47501E-02   0.69491E+00 
c  VelocityY    0.30083E+04    1814   0.47501E-02   0.00000E+00 
c  VelocityZ    0.30083E+04    1814   0.47501E-02   0.00000E+00 
c  Pressure     0.39476E+00    7039   0.32771E-01   0.18236E+00 
c  k            0.50777E+04     722   0.95387E-04   0.12652E+02 
c  omega        0.11349E+08     219   0.34917E-04   0.26450E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62727                             1
a  Local Time Step      1.1421e-05                         44718


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1437         0.79844      -0.0016128     -3.4507e-07
v  Velocity[Y]                 -26.293          28.706          6.8884          20.054
v  Velocity[Z]                 -27.868          28.757         0.32385        0.021853
v  ǁVelocityǁ                 0.006836          31.848          10.656          20.233
v  Pressure                    -354.07          340.06         -43.772          28.105
v  k                        4.3978e-07          78.577          3.7624          2.3196
v  omega                    4.0793e-19      1.4593e+07          8252.7          12.008
v  turbulent_viscosity      9.5798e-15          2.2515        0.017885         0.12302
v  CourantNb                 0.0085563          2351.6          44.755          1.3739
v  FourierNb                  0.011188           15679          83.312         0.64895
v  total_pressure           1.0097e+05      1.0167e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14825        0.010756        0.044543


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15735          128.07          2.0229


 TIME FOR THE TIME STEP              157:        0.43094E+02

===============================================================


 INSTANT    0.158000000E+02   TIME STEP NUMBER             158
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.158247207E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29271E+02 0.18551E+02
   Friction velocity        uet   :  0.17919E-02 0.23161E+01
   Friction velocity        uk    :  0.12601E-01 0.31170E+01
   Dimensionless distance   yplus :  0.41506E-01 0.31164E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        463
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30078E+04    1751   0.44534E-02   0.69159E+00 
c  VelocityY    0.30078E+04    1751   0.44534E-02   0.00000E+00 
c  VelocityZ    0.30078E+04    1751   0.44534E-02   0.00000E+00 
c  Pressure     0.40421E+00    7028   0.34259E-01   0.18675E+00 
c  k            0.51074E+04    1014   0.10089E-03   0.12504E+02 
c  omega        0.10801E+08     427   0.23199E-03   0.14210E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -92640                             2
a  Local Time Step      1.2625e-05                         44673


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2016         0.89832      -0.0020517     -1.8292e-06
v  Velocity[Y]                 -33.958           29.27          6.8389          20.054
v  Velocity[Z]                 -27.811          28.295         0.35283        0.026536
v  ǁVelocityǁ                 0.011791          34.398          10.664          20.231
v  Pressure                    -360.51          339.92         -46.144          28.024
v  k                        3.4515e-07          87.508          3.8217          2.3653
v  omega                    2.4781e-19       6.035e+07          8778.3          12.038
v  turbulent_viscosity      1.2411e-13          2.2343        0.017883         0.12688
v  CourantNb                  0.024365          2331.8          44.809          1.3739
v  FourierNb                  0.011159           15685          84.306         0.66461
v  total_pressure           1.0096e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14883        0.010754        0.044517


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15743          129.11          2.0385


 TIME FOR THE TIME STEP              158:        0.42978E+02

===============================================================


 INSTANT    0.159000000E+02   TIME STEP NUMBER             159
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.774638100E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39948E+02 0.13031E+02
   Friction velocity        uet   :  0.36268E-03 0.31256E+01
   Friction velocity        uk    :  0.17464E-01 0.39470E+01
   Dimensionless distance   yplus :  0.67031E-01 0.38138E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        452
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30070E+04    1761   0.44913E-02   0.68333E+00 
c  VelocityY    0.30070E+04    1761   0.44913E-02   0.00000E+00 
c  VelocityZ    0.30070E+04    1761   0.44913E-02   0.00000E+00 
c  Pressure     0.37442E+00    6962   0.36944E-01   0.17254E+00 
c  k            0.51304E+04    1105   0.10208E-03   0.12317E+02 
c  omega        0.23722E+08     371   0.44896E-04   0.54518E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -76752                             2
a  Local Time Step      1.2502e-05                         44595


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1738         0.92676      -0.0026411     -2.1768e-06
v  Velocity[Y]                 -25.276          29.539          6.8234          20.054
v  Velocity[Z]                  -27.85          28.463         0.36059        0.031428
v  ǁVelocityǁ                 0.014196          32.405          10.646          20.228
v  Pressure                    -366.86          339.62         -48.489          28.079
v  k                        1.4401e-08          63.684           3.824          2.4095
v  omega                    1.4884e-19      3.1174e+07          8604.7           12.04
v  turbulent_viscosity      2.2975e-13          2.2275        0.017889         0.13078
v  CourantNb                  0.025962          2486.1          45.028          1.3738
v  FourierNb                   0.01113           15671           84.88         0.68034
v  total_pressure           1.0096e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14843        0.010755        0.044521


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           15732          129.91          2.0541


 TIME FOR THE TIME STEP              159:        0.45033E+02

===============================================================


 INSTANT    0.160000000E+02   TIME STEP NUMBER             160
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.114758778E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28873E+02 0.13031E+02
   Friction velocity        uet   :  0.26291E-02 0.26781E+01
   Friction velocity        uk    :  0.16542E-01 0.32047E+01
   Dimensionless distance   yplus :  0.86974E-01 0.26773E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        521
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30064E+04    1893   0.44921E-02   0.68413E+00 
c  VelocityY    0.30064E+04    1893   0.44921E-02   0.00000E+00 
c  VelocityZ    0.30064E+04    1893   0.44921E-02   0.00000E+00 
c  Pressure     0.39097E+00    6939   0.37857E-01   0.18220E+00 
c  k            0.51466E+04    1182   0.96362E-04   0.12000E+02 
c  omega        0.12315E+08     247   0.62658E-04   0.30088E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2026e+05                             2
a  Local Time Step      1.2483e-05                         44556


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0601         0.94461       -0.003218     -4.3757e-06
v  Velocity[Y]                 -17.278          29.952          6.8221          20.055
v  Velocity[Z]                 -28.228          28.307         0.34181        0.036258
v  ǁVelocityǁ                 0.014552          32.609          10.594          20.228
v  Pressure                    -373.06          339.65         -49.947          28.237
v  k                        1.7797e-08          61.032          3.8575          2.4517
v  omega                    8.8414e-20      1.7534e+07          8383.8           12.02
v  turbulent_viscosity      6.2853e-14          2.2078        0.017895         0.13469
v  CourantNb                 0.0058937          2754.1          45.105          1.3737
v  FourierNb                  0.011101           15648          85.514         0.69595
v  total_pressure           1.0095e+05      1.0166e+05      1.0128e+05      1.0135e+05
v  Local Time Step                0.01         0.14813        0.010754        0.044483


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0114           15711          130.62          2.0696


 TIME FOR THE TIME STEP              160:        0.46077E+02

===============================================================


 INSTANT    0.161000000E+02   TIME STEP NUMBER             161
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.523180587E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29633E+02 0.13141E+02
   Friction velocity        uet   :  0.48933E-03 0.27714E+01
   Friction velocity        uk    :  0.11462E-01 0.33879E+01
   Dimensionless distance   yplus :  0.81674E-01 0.27155E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        564
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30055E+04    1988   0.45769E-02   0.68678E+00 
c  VelocityY    0.30055E+04    1988   0.45769E-02   0.00000E+00 
c  VelocityZ    0.30055E+04    1988   0.45769E-02   0.00000E+00 
c  Pressure     0.38238E+00    6927   0.35701E-01   0.17754E+00 
c  k            0.51542E+04    1286   0.10358E-03   0.11907E+02 
c  omega        0.16626E+08     371   0.67880E-04   0.88691E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -31908                             1
a  Local Time Step      1.2583e-05                         44501


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90646         0.97824      -0.0032886     -3.8916e-06
v  Velocity[Y]                 -16.601          31.688          6.8275          20.055
v  Velocity[Z]                 -28.511          28.559         0.30311        0.040303
v  ǁVelocityǁ                 0.013604          32.898          10.537          20.226
v  Pressure                    -377.39           343.9         -50.531          28.052
v  k                        3.1791e-09           58.82          3.8786           2.492
v  omega                    5.1666e-20      5.7234e+07          8468.1          12.028
v  turbulent_viscosity      1.6293e-15          2.1938        0.017899          0.1386
v  CourantNb                  0.032477          2285.5          44.864          1.3735
v  FourierNb                  0.011073           15549          87.183         0.71193
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14871        0.010755        0.044487


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0114           15613          132.05          2.0854


 TIME FOR THE TIME STEP              161:        0.46883E+02

===============================================================


 INSTANT    0.162000000E+02   TIME STEP NUMBER             162
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.204080446E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30324E+02 0.13242E+02
   Friction velocity        uet   :  0.65875E-03 0.28161E+01
   Friction velocity        uk    :  0.29309E-01 0.29188E+01
   Dimensionless distance   yplus :  0.10733E+00 0.29528E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        527
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30045E+04    1881   0.45573E-02   0.68624E+00 
c  VelocityY    0.30045E+04    1881   0.45573E-02   0.00000E+00 
c  VelocityZ    0.30045E+04    1881   0.45573E-02   0.00000E+00 
c  Pressure     0.39410E+00    6913   0.33748E-01   0.18283E+00 
c  k            0.51540E+04    1335   0.10425E-03   0.11700E+02 
c  omega        0.23320E+08     399   0.26761E-04   0.30373E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00050191                             1
a  omega                    -22773                             1
a  Local Time Step      1.2201e-05                         44407


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.63964          1.0025      -0.0026189     -1.8469e-06
v  Velocity[Y]                 -19.016          32.301          6.8172          20.055
v  Velocity[Z]                 -28.422          28.706         0.24638        0.043873
v  ǁVelocityǁ                 0.010681           32.78          10.489          20.225
v  Pressure                     -374.1          339.27         -51.476          27.386
v  k                        1.0888e-07          59.097          3.8411          2.5297
v  omega                    2.9652e-20      2.8766e+07          8169.1          11.983
v  turbulent_viscosity      1.9686e-14          2.1784        0.017887         0.14252
v  CourantNb                  0.027526            2279          44.557          1.3733
v  FourierNb                  0.011046           15409          89.141         0.72805
v  total_pressure           1.0095e+05      1.0166e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14821        0.010756        0.044473


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0114           15475           133.7          2.1013


 TIME FOR THE TIME STEP              162:        0.45217E+02

===============================================================


 INSTANT    0.163000000E+02   TIME STEP NUMBER             163
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.157911426E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30953E+02 0.13067E+02
   Friction velocity        uet   :  0.49548E-03 0.27461E+01
   Friction velocity        uk    :  0.16776E-01 0.31837E+01
   Dimensionless distance   yplus :  0.92967E-01 0.35675E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        494
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30033E+04    1864   0.44296E-02   0.68116E+00 
c  VelocityY    0.30033E+04    1864   0.44296E-02   0.00000E+00 
c  VelocityZ    0.30033E+04    1864   0.44296E-02   0.00000E+00 
c  Pressure     0.40784E+00    6628   0.32900E-01   0.18962E+00 
c  k            0.51448E+04    1299   0.10400E-03   0.11348E+02 
c  omega        0.12381E+08     327   0.16764E-03   0.12527E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -3.586e-06                             2
a  omega               -1.8061e+05                             1
a  Local Time Step      1.2564e-05                         44298


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.3187          1.0203      -0.0014177     -1.1113e-06
v  Velocity[Y]                 -18.353          32.813            6.78          20.055
v  Velocity[Z]                 -28.493          28.707         0.18403        0.047556
v  ǁVelocityǁ                 0.012555          33.793          10.479          20.223
v  Pressure                    -362.33          338.49         -52.692          26.671
v  k                        3.5475e-07          58.867           3.799          2.5651
v  omega                    1.6915e-20      1.7441e+08          9003.5          12.095
v  turbulent_viscosity        2.15e-14          2.1628        0.017842         0.14641
v  CourantNb                  0.025057          2273.6            44.4          1.3731
v  FourierNb                   0.01102           15190          88.243         0.74333
v  total_pressure           1.0096e+05      1.0166e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14845        0.010758        0.044478


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0114           15255          132.64          2.1165


 TIME FOR THE TIME STEP              163:        0.43594E+02

===============================================================


 INSTANT    0.164000000E+02   TIME STEP NUMBER             164
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.274442513E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31354E+02 0.19616E+02
   Friction velocity        uet   :  0.11894E-02 0.26493E+01
   Friction velocity        uk    :  0.19574E-01 0.31063E+01
   Dimensionless distance   yplus :  0.14761E+00 0.31381E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        512
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30019E+04    1836   0.43857E-02   0.67818E+00 
c  VelocityY    0.30019E+04    1836   0.43857E-02   0.00000E+00 
c  VelocityZ    0.30019E+04    1836   0.43857E-02   0.00000E+00 
c  Pressure     0.36717E+00    6930   0.30676E-01   0.17118E+00 
c  k            0.51286E+04    1127   0.10699E-03   0.11075E+02 
c  omega        0.12291E+14       2   0.47535E-09   0.31952E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024617                             4
a  omega          
a  Local Time Step      1.2483e-05                         44152


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.4377           1.058     -0.00011284      -9.817e-07
v  Velocity[Y]                 -17.754          30.785          6.7679          20.054
v  Velocity[Z]                 -28.526          28.821         0.12742        0.050567
v  ǁVelocityǁ                 0.008595          31.817          10.494           20.22
v  Pressure                    -365.29          338.97         -53.376          26.066
v  k                        1.1578e-06          58.239          3.7512          2.5979
v  omega                    9.6913e-21      8.7203e+07          8454.1          12.032
v  turbulent_viscosity      2.0249e-13          2.1511        0.017786         0.15027
v  CourantNb                  0.030592          2269.6          44.391          1.3733
v  FourierNb                  0.010991           14935          86.303         0.75827
v  total_pressure           1.0096e+05      1.0166e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14784         0.01076        0.044469


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0111           14999          130.69          2.1315


 TIME FOR THE TIME STEP              164:        0.43402E+02

===============================================================


 INSTANT    0.165000000E+02   TIME STEP NUMBER             165
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.252719559E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29890E+02 0.19060E+02
   Friction velocity        uet   :  0.21167E-02 0.26425E+01
   Friction velocity        uk    :  0.23824E-01 0.28931E+01
   Dimensionless distance   yplus :  0.11711E+00 0.26567E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        512
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.30004E+04    1867   0.42953E-02   0.66730E+00 
c  VelocityY    0.30004E+04    1867   0.42953E-02   0.00000E+00 
c  VelocityZ    0.30004E+04    1867   0.42953E-02   0.00000E+00 
c  Pressure     0.37476E+00    6979   0.28531E-01   0.17481E+00 
c  k            0.50823E+04     852   0.10742E-03   0.10959E+02 
c  omega        0.45509E+12       3   0.32661E-08   0.97958E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.3456e-05                             5
a  omega          
a  Local Time Step      1.2118e-05                         44065


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.57825          1.1078       0.0010107     -1.5377e-06
v  Velocity[Y]                 -14.941          29.787          6.8025          20.053
v  Velocity[Z]                 -30.678          28.892        0.080147        0.052903
v  ǁVelocityǁ                0.0092987          34.735          10.534          20.219
v  Pressure                    -367.62          340.82          -53.21           26.19
v  k                        4.3131e-07          57.587          3.7337           2.627
v  omega                    5.6674e-21      4.3597e+07          8345.9          12.022
v  turbulent_viscosity      2.0909e-13          2.1281        0.017715         0.15375
v  CourantNb                  0.011875          2274.2          44.491          1.3733
v  FourierNb                  0.010959           14742          85.486         0.77287
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14809        0.010762        0.044456


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0111           14804          129.98          2.1462


 TIME FOR THE TIME STEP              165:        0.42912E+02

===============================================================


 INSTANT    0.166000000E+02   TIME STEP NUMBER             166
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.666944362E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29633E+02 0.14649E+02
   Friction velocity        uet   :  0.12187E-02 0.29328E+01
   Friction velocity        uk    :  0.19840E-01 0.30567E+01
   Dimensionless distance   yplus :  0.12245E+00 0.26372E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29989E+04    1889   0.43911E-02   0.65199E+00 
c  VelocityY    0.29989E+04    1889   0.43911E-02   0.00000E+00 
c  VelocityZ    0.29989E+04    1889   0.43911E-02   0.00000E+00 
c  Pressure     0.39086E+00    7053   0.31079E-01   0.18198E+00 
c  k            0.50320E+04     801   0.10963E-03   0.10861E+02 
c  omega        0.25055E+08     199   0.41127E-04   0.95467E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.3625e-05                             3
a  omega          
a  Local Time Step      1.1691e-05                         44010


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.66219          1.1395        0.001957     -7.9671e-07
v  Velocity[Y]                  -14.94          30.898           6.875          20.053
v  Velocity[Z]                 -30.849          28.888        0.064942        0.054316
v  ǁVelocityǁ                 0.010468           34.54          10.612          20.217
v  Pressure                    -369.98          342.71         -52.631          26.357
v  k                        1.2416e-06          57.732          3.7449          2.6528
v  omega                    3.3759e-21      4.3708e+07          8449.6          12.051
v  turbulent_viscosity      6.2619e-14          2.1043        0.017686         0.15711
v  CourantNb                  0.044487          2287.3          44.474          1.3732
v  FourierNb                  0.010931           14723          83.707         0.78764
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14753        0.010763        0.044418


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9893           14782          128.18          2.1608


 TIME FOR THE TIME STEP              166:        0.44667E+02

===============================================================


 INSTANT    0.167000000E+02   TIME STEP NUMBER             167
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.372995888E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30504E+02 0.13847E+02
   Friction velocity        uet   :  0.21581E-02 0.30433E+01
   Friction velocity        uk    :  0.18294E-01 0.31797E+01
   Dimensionless distance   yplus :  0.13064E+00 0.26492E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29974E+04    1916   0.44055E-02   0.63476E+00 
c  VelocityY    0.29974E+04    1916   0.44055E-02   0.00000E+00 
c  VelocityZ    0.29974E+04    1916   0.44055E-02   0.00000E+00 
c  Pressure     0.38441E+00    7074   0.36271E-01   0.17909E+00 
c  k            0.50030E+04     862   0.10700E-03   0.10557E+02 
c  omega        0.17375E+08     200   0.11155E-03   0.16377E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00062885                             3
a  omega               -2.2719e+05                             1
a  Local Time Step      1.1748e-05                         43997


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.78455          1.2016        0.002613      3.4999e-07
v  Velocity[Y]                  -14.94          32.785          6.9675          20.054
v  Velocity[Z]                 -32.549          28.707        0.097185         0.05554
v  ǁVelocityǁ                 0.014078          34.339          10.708          20.217
v  Pressure                    -398.23          343.75         -52.618          26.376
v  k                        3.1052e-08          64.967          3.7377          2.6762
v  omega                    2.0306e-21      6.4473e+07          8704.2          12.055
v  turbulent_viscosity      1.8032e-13           2.083        0.017669         0.16076
v  CourantNb                  0.042481          2625.8          44.567          1.3731
v  FourierNb                  0.010909           14728          83.019         0.80323
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14872        0.010764        0.044372


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14783          127.59          2.1763


 TIME FOR THE TIME STEP              167:        0.44600E+02

===============================================================


 INSTANT    0.168000000E+02   TIME STEP NUMBER             168
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.265153258E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30191E+02 0.14037E+02
   Friction velocity        uet   :  0.12075E-02 0.32304E+01
   Friction velocity        uk    :  0.13154E-01 0.27825E+01
   Dimensionless distance   yplus :  0.52771E-01 0.26564E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        483
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29957E+04    1907   0.41423E-02   0.61336E+00 
c  VelocityY    0.29957E+04    1907   0.41423E-02   0.00000E+00 
c  VelocityZ    0.29957E+04    1907   0.41423E-02   0.00000E+00 
c  Pressure     0.40127E+00    6974   0.39077E-01   0.18744E+00 
c  k            0.49744E+04    1000   0.10215E-03   0.10175E+02 
c  omega        0.26659E+08     158   0.48091E-04   0.11987E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00084098                             2
a  omega          
a  Local Time Step      1.2203e-05                         44001


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88948           1.352       0.0027908      1.0482e-06
v  Velocity[Y]                 -21.282          29.662          7.0365          20.054
v  Velocity[Z]                 -32.493          28.646         0.16148        0.055919
v  ǁVelocityǁ                 0.017463          33.577          10.762          20.216
v  Pressure                    -404.44          344.15         -52.914          26.242
v  k                         1.001e-07           60.56          3.7318          2.6969
v  omega                    1.2119e-21      3.3189e+07          8599.6          12.077
v  turbulent_viscosity       7.759e-15          2.0761         0.01767         0.16432
v  CourantNb                 0.0021922          2816.5          44.992          1.3733
v  FourierNb                   0.01089           14647          83.051         0.81922
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14936        0.010764        0.044378


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99023           14702          128.04          2.1925


 TIME FOR THE TIME STEP              168:        0.43810E+02

===============================================================


 INSTANT    0.169000000E+02   TIME STEP NUMBER             169
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.531244539E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28875E+02 0.15169E+02
   Friction velocity        uet   :  0.17652E-02 0.28652E+01
   Friction velocity        uk    :  0.13339E-01 0.28455E+01
   Dimensionless distance   yplus :  0.13942E+00 0.26762E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29938E+04    1879   0.40797E-02   0.57154E+00 
c  VelocityY    0.29938E+04    1879   0.40797E-02   0.00000E+00 
c  VelocityZ    0.29938E+04    1879   0.40797E-02   0.00000E+00 
c  Pressure     0.38527E+00    6943   0.36249E-01   0.17903E+00 
c  k            0.49458E+04    1015   0.96818E-04   0.98780E+01 
c  omega        0.18465E+08     255   0.38027E-04   0.42266E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00053716                             2
a  omega          
a  Local Time Step      1.2071e-05                         43947


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94911           1.444       0.0028526     -9.1566e-07
v  Velocity[Y]                 -22.826          29.538          7.0439          20.054
v  Velocity[Z]                 -30.681           28.39         0.23445        0.055811
v  ǁVelocityǁ                 0.016041          31.497          10.762          20.215
v  Pressure                    -391.99          344.73         -53.051           26.19
v  k                        2.2924e-09          71.951          3.7165          2.7147
v  omega                    7.1703e-22      1.8468e+07          8325.9          12.052
v  turbulent_viscosity      1.8882e-14          2.0774        0.017647         0.16778
v  CourantNb                   0.04459          2483.3          45.396          1.3737
v  FourierNb                  0.010872           14583          82.802           0.835
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01           0.148        0.010764        0.044356


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14640           128.2          2.2087


 TIME FOR THE TIME STEP              169:        0.43736E+02

===============================================================


 INSTANT    0.170000000E+02   TIME STEP NUMBER             170
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.835443072E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28695E+02 0.17204E+02
   Friction velocity        uet   :  0.19417E-02 0.26538E+01
   Friction velocity        uk    :  0.17239E-01 0.29036E+01
   Dimensionless distance   yplus :  0.71111E-01 0.26832E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        424
   Nb of faces within the viscous sub-layer     :       1082
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29919E+04    1964   0.42585E-02   0.53175E+00 
c  VelocityY    0.29919E+04    1964   0.42585E-02   0.00000E+00 
c  VelocityZ    0.29919E+04    1964   0.42585E-02   0.00000E+00 
c  Pressure     0.38432E+00    6961   0.33279E-01   0.17832E+00 
c  k            0.49151E+04    1220   0.90967E-04   0.95278E+01 
c  omega        0.12095E+08     236   0.43019E-04   0.28945E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.8783e-06                             1
a  omega                    -39551                             1
a  Local Time Step      1.1511e-05                         43754


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.96434            1.46       0.0026221     -2.3309e-06
v  Velocity[Y]                 -32.567          29.439          6.9877          20.054
v  Velocity[Z]                 -29.842           28.43         0.27773        0.054879
v  ǁVelocityǁ                  0.01428          32.712           10.76          20.214
v  Pressure                    -370.11          345.14         -53.128          26.134
v  k                        4.2802e-10          89.437          3.7131          2.7297
v  omega                    4.2245e-22      1.2597e+07          8309.9          12.064
v  turbulent_viscosity      1.8254e-15          2.0804        0.017599          0.1711
v  CourantNb                  0.043539          2288.7          45.579           1.374
v  FourierNb                  0.010857           14553          83.028         0.85072
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14933        0.010766        0.044336


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14610          128.61          2.2247


 TIME FOR THE TIME STEP              170:        0.44647E+02

===============================================================


 INSTANT    0.171000000E+02   TIME STEP NUMBER             171
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.180826236E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29712E+02 0.22420E+02
   Friction velocity        uet   :  0.26603E-03 0.28955E+01
   Friction velocity        uk    :  0.18816E-01 0.31930E+01
   Dimensionless distance   yplus :  0.80371E-01 0.26887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1093
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29901E+04    1987   0.44857E-02   0.50378E+00 
c  VelocityY    0.29901E+04    1987   0.44857E-02   0.00000E+00 
c  VelocityZ    0.29901E+04    1987   0.44857E-02   0.00000E+00 
c  Pressure     0.42634E+00    6998   0.34518E-01   0.19698E+00 
c  k            0.48814E+04    1134   0.89080E-04   0.91151E+01 
c  omega        0.11304E+08     396   0.49221E-04   0.44731E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1396e+05                             1
a  Local Time Step      1.1687e-05                         43721


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95198          1.3908       0.0022813     -3.6914e-06
v  Velocity[Y]                 -28.756          29.559          6.9372          20.054
v  Velocity[Z]                 -28.616          28.258         0.29919         0.05298
v  ǁVelocityǁ                 0.011439          37.108          10.781          20.214
v  Pressure                    -374.13           345.6         -53.142          26.672
v  k                        1.0123e-10          88.701          3.7495           2.742
v  omega                    2.5043e-22      1.3495e+07          8627.7          12.105
v  turbulent_viscosity      6.6525e-16          2.0916        0.017538         0.17429
v  CourantNb                  0.015685          2274.1          45.629          1.3741
v  FourierNb                  0.010844           14487          82.946         0.86564
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14765        0.010768        0.044286


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14545          128.58          2.2397


 TIME FOR THE TIME STEP              171:        0.44705E+02

===============================================================


 INSTANT    0.172000000E+02   TIME STEP NUMBER             172
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.499578047E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53110E+02 0.18044E+02
   Friction velocity        uet   :  0.19072E-02 0.31699E+01
   Friction velocity        uk    :  0.32249E-01 0.41094E+01
   Dimensionless distance   yplus :  0.13303E+00 0.35515E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29882E+04    1936   0.43667E-02   0.49032E+00 
c  VelocityY    0.29882E+04    1936   0.43667E-02   0.00000E+00 
c  VelocityZ    0.29882E+04    1936   0.43667E-02   0.00000E+00 
c  Pressure     0.41058E+00    7000   0.37159E-01   0.19033E+00 
c  k            0.48449E+04    1089   0.84660E-04   0.87266E+01 
c  omega        0.12922E+08     515   0.35312E-04   0.25582E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1678e-05                         43759


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92977          1.2374       0.0019023     -3.9715e-06
v  Velocity[Y]                 -31.367          30.011          6.9444          20.054
v  Velocity[Z]                  -28.57          28.327         0.30654        0.050304
v  ǁVelocityǁ                0.0053984            32.6          10.787          20.213
v  Pressure                    -374.78           345.3         -54.151          26.958
v  k                        1.4919e-08            60.7           3.771          2.7518
v  omega                    1.4974e-22       1.173e+07          8335.1          12.073
v  turbulent_viscosity       4.616e-17          2.1145        0.017491         0.17732
v  CourantNb                  0.054563          2264.7          45.716          1.3743
v  FourierNb                  0.010833           14408          82.909         0.88028
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14801        0.010769        0.044299


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97569           14467          128.63          2.2545


 TIME FOR THE TIME STEP              172:        0.44327E+02

===============================================================


 INSTANT    0.173000000E+02   TIME STEP NUMBER             173
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.604305730E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30502E+02 0.17960E+02
   Friction velocity        uet   :  0.65174E-03 0.30597E+01
   Friction velocity        uk    :  0.96820E-02 0.32278E+01
   Dimensionless distance   yplus :  0.13892E+00 0.37087E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :       1068
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29864E+04    1903   0.43944E-02   0.47404E+00 
c  VelocityY    0.29864E+04    1903   0.43944E-02   0.00000E+00 
c  VelocityZ    0.29864E+04    1903   0.43944E-02   0.00000E+00 
c  Pressure     0.43674E+00    6991   0.36329E-01   0.20344E+00 
c  k            0.48057E+04     922   0.70410E-04   0.82949E+01 
c  omega        0.11452E+08     391   0.15375E-03   0.17043E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00018769                             1
a  omega          
a  Local Time Step      1.1814e-05                         43825


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0094         0.99536       0.0014445      -5.265e-06
v  Velocity[Y]                 -17.434          30.513          6.9667          20.053
v  Velocity[Z]                  -28.56          28.368          0.2964        0.046616
v  ǁVelocityǁ                0.0079121          33.214          10.775          20.212
v  Pressure                    -375.39          344.99         -55.086          27.401
v  k                         1.503e-08          50.807          3.7936          2.7584
v  omega                    9.0334e-23      4.5703e+07          8905.5          12.062
v  turbulent_viscosity      1.3505e-14          2.1323        0.017482         0.18018
v  CourantNb                  0.026001            2972          45.982          1.3745
v  FourierNb                  0.010823           14389          82.985         0.89456
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14844        0.010771        0.044307


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14448          128.97           2.269


 TIME FOR THE TIME STEP              173:        0.43305E+02

===============================================================


 INSTANT    0.174000000E+02   TIME STEP NUMBER             174
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.629149041E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30856E+02 0.15285E+02
   Friction velocity        uet   :  0.17075E-02 0.26835E+01
   Friction velocity        uk    :  0.33100E-01 0.31072E+01
   Dimensionless distance   yplus :  0.17384E+00 0.26949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        531
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29848E+04    2033   0.40101E-02   0.47470E+00 
c  VelocityY    0.29848E+04    2033   0.40101E-02   0.00000E+00 
c  VelocityZ    0.29848E+04    2033   0.40101E-02   0.00000E+00 
c  Pressure     0.40520E+00    6963   0.32261E-01   0.18775E+00 
c  k            0.47621E+04     825   0.62883E-04   0.79110E+01 
c  omega        0.20285E+08     294   0.97340E-04   0.13883E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0978e-05                         43862


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1957         0.91022      0.00096857     -5.6472e-06
v  Velocity[Y]                 -16.993          31.456          6.9847          20.054
v  Velocity[Z]                 -28.467          28.563         0.26652        0.042337
v  ǁVelocityǁ                 0.020816          33.323          10.745          20.212
v  Pressure                    -376.31          344.93         -55.402          27.737
v  k                         5.776e-11          62.573          3.8286          2.7623
v  omega                    5.4734e-23      5.0214e+07          8799.2          12.042
v  turbulent_viscosity      1.3682e-14           2.147        0.017493         0.18284
v  CourantNb                  0.031923          2303.1          45.861          1.3745
v  FourierNb                  0.010815           14366           84.02         0.90819
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14749        0.010772        0.044328


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14425          129.88          2.2827


 TIME FOR THE TIME STEP              174:        0.45934E+02

===============================================================


 INSTANT    0.175000000E+02   TIME STEP NUMBER             175
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.433329350E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31149E+02 0.13751E+02
   Friction velocity        uet   :  0.77322E-03 0.28956E+01
   Friction velocity        uk    :  0.12483E-01 0.31454E+01
   Dimensionless distance   yplus :  0.11203E+00 0.29271E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        545
   Nb of faces within the viscous sub-layer     :       1099
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29835E+04    1956   0.39422E-02   0.47930E+00 
c  VelocityY    0.29835E+04    1956   0.39422E-02   0.00000E+00 
c  VelocityZ    0.29835E+04    1956   0.39422E-02   0.00000E+00 
c  Pressure     0.39501E+00    6943   0.30467E-01   0.18260E+00 
c  k            0.47154E+04     993   0.57635E-04   0.77044E+01 
c  omega        0.18459E+08     413   0.51396E-04   0.41684E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.148e-05                         43911


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3965          1.0812      0.00032969     -4.0551e-06
v  Velocity[Y]                 -15.063          32.378          6.9862          20.054
v  Velocity[Z]                  -28.72           29.05         0.22821        0.037296
v  ǁVelocityǁ                 0.009044          33.044          10.694          20.212
v  Pressure                    -373.14          345.22         -55.415          27.867
v  k                        1.6935e-09           50.81           3.814          2.7631
v  omega                    3.2984e-23      2.6307e+07          8388.1          12.014
v  turbulent_viscosity      2.7171e-16          2.1467        0.017518         0.18531
v  CourantNb                  0.011596          2259.3          45.514          1.3746
v  FourierNb                  0.010808           14322          86.298         0.92132
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14837        0.010773        0.044341


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14381          131.81          2.2959


 TIME FOR THE TIME STEP              175:        0.45442E+02

===============================================================


 INSTANT    0.176000000E+02   TIME STEP NUMBER             176
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.541432757E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31493E+02 0.14228E+02
   Friction velocity        uet   :  0.19889E-02 0.28430E+01
   Friction velocity        uk    :  0.10723E-01 0.31568E+01
   Dimensionless distance   yplus :  0.95843E-01 0.31366E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        506
   Nb of faces within the viscous sub-layer     :       1033
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29826E+04    1913   0.39748E-02   0.48574E+00 
c  VelocityY    0.29826E+04    1913   0.39748E-02   0.00000E+00 
c  VelocityZ    0.29826E+04    1913   0.39748E-02   0.00000E+00 
c  Pressure     0.37986E+00    6903   0.31333E-01   0.17617E+00 
c  k            0.46611E+04     905   0.51562E-04   0.73488E+01 
c  omega        0.11828E+08     336   0.92997E-04   0.75892E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6456e+05                             1
a  Local Time Step      1.2256e-05                         44014


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5971          1.1689     -0.00071517     -1.9406e-06
v  Velocity[Y]                 -15.017          32.382          6.9271          20.054
v  Velocity[Z]                 -28.325          29.377          0.1745        0.031573
v  ǁVelocityǁ                0.0068716          33.113          10.643          20.211
v  Pressure                    -361.48          345.18         -55.784          27.436
v  k                        2.1868e-07           43.43          3.7928          2.7609
v  omega                    1.9664e-23      5.4585e+07          8426.9          12.021
v  turbulent_viscosity      2.6089e-15          2.1462        0.017523         0.18758
v  CourantNb                  0.063994          2247.6          45.128          1.3746
v  FourierNb                  0.010803           14267          86.179         0.93266
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14829        0.010772        0.044365


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0113           14327          131.31          2.3073


 TIME FOR THE TIME STEP              176:        0.44347E+02

===============================================================


 INSTANT    0.177000000E+02   TIME STEP NUMBER             177
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.449860720E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31316E+02 0.22427E+02
   Friction velocity        uet   :  0.12398E-02 0.26873E+01
   Friction velocity        uk    :  0.24198E-01 0.32613E+01
   Dimensionless distance   yplus :  0.13676E+00 0.34949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29818E+04    2001   0.39303E-02   0.48599E+00 
c  VelocityY    0.29818E+04    2001   0.39303E-02   0.00000E+00 
c  VelocityZ    0.29818E+04    2001   0.39303E-02   0.00000E+00 
c  Pressure     0.34622E+00    6970   0.30821E-01   0.15956E+00 
c  k            0.46004E+04     953   0.46576E-04   0.70491E+01 
c  omega        0.23189E+08     211   0.39644E-04   0.59868E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2307e-05                         44027


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7511          1.1688      -0.0018741     -6.0376e-07
v  Velocity[Y]                 -19.444          31.275          6.8672          20.054
v  Velocity[Z]                 -28.354          29.258         0.13121        0.025468
v  ǁVelocityǁ                 0.016481          34.278          10.616          20.211
v  Pressure                    -353.55          346.68         -55.566          27.582
v  k                        4.0505e-08           41.79          3.7799          2.7562
v  omega                    1.1615e-23      4.0853e+07          8354.6          12.019
v  turbulent_viscosity      4.7707e-14          2.1388        0.017519         0.18962
v  CourantNb                  0.019793          2233.7          44.799          1.3749
v  FourierNb                  0.010799           14181          85.092         0.94272
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01          0.1492        0.010771        0.044361


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0112           14241          129.89          2.3176


 TIME FOR THE TIME STEP              177:        0.45322E+02

===============================================================


 INSTANT    0.178000000E+02   TIME STEP NUMBER             178
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.865353343E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30795E+02 0.21471E+02
   Friction velocity        uet   :  0.11348E-02 0.28160E+01
   Friction velocity        uk    :  0.26986E-01 0.30537E+01
   Dimensionless distance   yplus :  0.11457E+00 0.27426E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        504
   Nb of faces within the viscous sub-layer     :        958
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29812E+04    2062   0.39673E-02   0.48534E+00 
c  VelocityY    0.29812E+04    2062   0.39673E-02   0.00000E+00 
c  VelocityZ    0.29812E+04    2062   0.39673E-02   0.00000E+00 
c  Pressure     0.34697E+00    6973   0.28547E-01   0.15975E+00 
c  k            0.45345E+04     997   0.45414E-04   0.68590E+01 
c  omega        0.16121E+08     201   0.82554E-03   0.41248E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003183                             1
a  omega          
a  Local Time Step      1.2193e-05                         44005


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8376          1.3262      -0.0029037      9.3606e-08
v  Velocity[Y]                 -17.181           29.97          6.8405          20.054
v  Velocity[Z]                 -32.044          29.348        0.081112        0.018508
v  ǁVelocityǁ                 0.016236          36.934          10.595           20.21
v  Pressure                    -350.84          348.79          -54.65          27.907
v  k                         4.672e-07          47.516          3.7797           2.749
v  omega                    6.8225e-24      3.9611e+08           11329          12.204
v  turbulent_viscosity      7.2983e-15          2.1313        0.017524         0.19145
v  CourantNb                  0.029352          2225.4          44.898          1.3752
v  FourierNb                  0.010795           14143          85.088         0.95267
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14923        0.010771         0.04436


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0112           14200          129.99          2.3278


 TIME FOR THE TIME STEP              178:        0.44979E+02

===============================================================


 INSTANT    0.179000000E+02   TIME STEP NUMBER             179
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.474530687E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30346E+02 0.16386E+02
   Friction velocity        uet   :  0.66981E-03 0.31508E+01
   Friction velocity        uk    :  0.18590E-01 0.30740E+01
   Dimensionless distance   yplus :  0.16686E+00 0.27469E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29804E+04    2047   0.41225E-02   0.48181E+00 
c  VelocityY    0.29804E+04    2047   0.41225E-02   0.00000E+00 
c  VelocityZ    0.29804E+04    2047   0.41225E-02   0.00000E+00 
c  Pressure     0.38752E+00    7053   0.28759E-01   0.17994E+00 
c  k            0.44644E+04     869   0.46733E-04   0.67292E+01 
c  omega        0.73596E+09      43   0.61159E-05   0.10490E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.0023e-05                             1
a  omega          
a  Local Time Step      1.1804e-05                         44001


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8216          1.3705      -0.0034722      7.8168e-07
v  Velocity[Y]                 -16.541          31.189          6.8602          20.054
v  Velocity[Z]                 -31.975          29.225        0.048004        0.011184
v  ǁVelocityǁ                 0.019277          36.225          10.615           20.21
v  Pressure                    -381.05          350.22         -53.559          28.391
v  k                        6.6239e-07          60.091          3.7934          2.7395
v  omega                    4.0308e-24      1.9819e+08          9739.3          12.093
v  turbulent_viscosity      3.4712e-13          2.1178        0.017545         0.19307
v  CourantNb                  0.028026          2233.8          44.813          1.3752
v  FourierNb                  0.010793           14177           85.51         0.96213
v  total_pressure           1.0094e+05      1.0168e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14864        0.010772        0.044365


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97187           14233          130.32          2.3373


 TIME FOR THE TIME STEP              179:        0.43927E+02

===============================================================


 INSTANT    0.180000000E+02   TIME STEP NUMBER             180
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.677369601E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30190E+02 0.13610E+02
   Friction velocity        uet   :  0.11662E-02 0.31305E+01
   Friction velocity        uk    :  0.72291E-02 0.31659E+01
   Dimensionless distance   yplus :  0.63647E-01 0.27332E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        436
   Nb of faces within the viscous sub-layer     :        968
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29797E+04    2045   0.38070E-02   0.48297E+00 
c  VelocityY    0.29797E+04    2045   0.38070E-02   0.00000E+00 
c  VelocityZ    0.29797E+04    2045   0.38070E-02   0.00000E+00 
c  Pressure     0.41424E+00    7089   0.30355E-01   0.19212E+00 
c  k            0.43930E+04     924   0.49263E-04   0.65752E+01 
c  omega        0.18409E+09     117   0.13597E-04   0.32363E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.9874e-06                             1
a  omega               -2.5373e+05                             1
a  Local Time Step      1.1272e-05                         44020


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6948          1.4029       -0.003123       1.702e-06
v  Velocity[Y]                 -15.067          31.294          6.9132          20.054
v  Velocity[Z]                 -33.126          29.198        0.051593       0.0037978
v  ǁVelocityǁ                 0.007787          35.356          10.672           20.21
v  Pressure                    -418.32          350.27         -52.573          28.776
v  k                        5.5508e-08          68.972          3.7987          2.7277
v  omega                    2.3838e-24      9.9389e+07            9075          12.075
v  turbulent_viscosity      1.1311e-13          2.1023        0.017569         0.19447
v  CourantNb                 0.0096085          2563.8          44.733          1.3751
v  FourierNb                  0.010791           14202          86.184         0.97112
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14855        0.010773        0.044363


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0111           14262          130.92          2.3462


 TIME FOR THE TIME STEP              180:        0.44744E+02

===============================================================


 INSTANT    0.181000000E+02   TIME STEP NUMBER             181
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.443988731E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30289E+02 0.13758E+02
   Friction velocity        uet   :  0.12272E-02 0.31539E+01
   Friction velocity        uk    :  0.17412E-01 0.30534E+01
   Dimensionless distance   yplus :  0.14244E+00 0.27269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29787E+04    2031   0.40547E-02   0.48770E+00 
c  VelocityY    0.29787E+04    2031   0.40547E-02   0.00000E+00 
c  VelocityZ    0.29787E+04    2031   0.40547E-02   0.00000E+00 
c  Pressure     0.38248E+00    7001   0.33491E-01   0.17702E+00 
c  k            0.43213E+04    1130   0.50879E-04   0.63708E+01 
c  omega        0.49345E+08     128   0.25921E-04   0.99584E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2256e-05                         44023


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4531          1.4911      -0.0017847      1.2509e-07
v  Velocity[Y]                 -21.844          30.098          6.9754          20.054
v  Velocity[Z]                 -32.559          28.887        0.095343      -0.0041568
v  ǁVelocityǁ                  0.01031          33.777          10.729           20.21
v  Pressure                    -429.04          349.02         -52.134          28.756
v  k                        2.6943e-09          66.924          3.7705          2.7136
v  omega                    1.3966e-24      5.0303e+07            8549           12.05
v  turbulent_viscosity      6.5825e-16          2.0899         0.01757         0.19564
v  CourantNb                  0.017243            2762          44.816          1.3751
v  FourierNb                  0.010791           14199          86.327         0.97927
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14859        0.010775        0.044405


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93075           14259          131.14          2.3544


 TIME FOR THE TIME STEP              181:        0.44390E+02

===============================================================


 INSTANT    0.182000000E+02   TIME STEP NUMBER             182
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.264129589E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30214E+02 0.14796E+02
   Friction velocity        uet   :  0.11007E-02 0.28887E+01
   Friction velocity        uk    :  0.21396E-01 0.29390E+01
   Dimensionless distance   yplus :  0.57621E-01 0.27272E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :       1079
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29776E+04    2002   0.42448E-02   0.47127E+00 
c  VelocityY    0.29776E+04    2002   0.42448E-02   0.00000E+00 
c  VelocityZ    0.29776E+04    2002   0.42448E-02   0.00000E+00 
c  Pressure     0.39443E+00    7074   0.34534E-01   0.18203E+00 
c  k            0.42482E+04    1194   0.51830E-04   0.61770E+01 
c  omega        0.16607E+08     225   0.12698E-03   0.26970E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -7.9921e-05                             2
a  omega               -1.9631e+05                             1
a  Local Time Step      1.2192e-05                         44051


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2169          1.5463     -0.00017199      5.9799e-07
v  Velocity[Y]                  -24.42          30.003          6.9983          20.055
v  Velocity[Z]                 -31.873          28.642         0.14168       -0.012094
v  ǁVelocityǁ                0.0057523          33.131          10.744          20.211
v  Pressure                    -419.23          347.24         -52.052          28.896
v  k                        5.5195e-09           54.52           3.726          2.6972
v  omega                         1e-24      7.2112e+07          9024.1          12.107
v  turbulent_viscosity      6.3129e-17          2.0739         0.01753         0.19658
v  CourantNb                  0.026571          2504.4          45.188          1.3754
v  FourierNb                  0.010791           14140          84.954         0.98597
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14892        0.010778         0.04445


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87625           14201          130.14          2.3614


 TIME FOR THE TIME STEP              182:        0.44634E+02

===============================================================


 INSTANT    0.183000000E+02   TIME STEP NUMBER             183
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.689022094E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30470E+02 0.14604E+02
   Friction velocity        uet   :  0.66135E-03 0.27939E+01
   Friction velocity        uk    :  0.17754E-01 0.30491E+01
   Dimensionless distance   yplus :  0.44690E-01 0.26948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :       1111
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29763E+04    1959   0.41163E-02   0.44976E+00 
c  VelocityY    0.29763E+04    1959   0.41163E-02   0.00000E+00 
c  VelocityZ    0.29763E+04    1959   0.41163E-02   0.00000E+00 
c  Pressure     0.39534E+00    6981   0.32455E-01   0.18428E+00 
c  k            0.41716E+04    1157   0.54428E-04   0.59251E+01 
c  omega        0.47067E+08     144   0.47997E-04   0.20690E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00017715                             2
a  omega                   -1009.7                             1
a  Local Time Step      1.0921e-05                         44087


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0588          1.5918       0.0014751      5.7406e-07
v  Velocity[Y]                 -31.054          29.895          6.9677          20.055
v  Velocity[Z]                 -28.848          28.473         0.16798       -0.020095
v  ǁVelocityǁ                0.0090487          32.094          10.751          20.211
v  Pressure                    -395.65          345.85         -52.544          28.622
v  k                        4.6395e-09          61.877          3.7184          2.6787
v  omega                         1e-24      8.2308e+07          9159.5           12.13
v  turbulent_viscosity      2.7806e-15          2.0609         0.01746         0.19729
v  CourantNb                  0.032893          2298.6          45.469          1.3757
v  FourierNb                  0.010791           14044          83.889         0.99183
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14932        0.010781        0.044497


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0071           14106          129.36          2.3675


 TIME FOR THE TIME STEP              183:        0.45260E+02

===============================================================


 INSTANT    0.184000000E+02   TIME STEP NUMBER             184
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.142441362E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30723E+02 0.21837E+02
   Friction velocity        uet   :  0.13879E-02 0.28437E+01
   Friction velocity        uk    :  0.23045E-01 0.30370E+01
   Dimensionless distance   yplus :  0.15321E+00 0.26758E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1147
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29747E+04    1895   0.40712E-02   0.44114E+00 
c  VelocityY    0.29747E+04    1895   0.40712E-02   0.00000E+00 
c  VelocityZ    0.29747E+04    1895   0.40712E-02   0.00000E+00 
c  Pressure     0.35989E+00    6995   0.32222E-01   0.16679E+00 
c  k            0.40898E+04    1010   0.61371E-04   0.55843E+01 
c  omega        0.32567E+08     239   0.33764E-04   0.77896E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028227                             2
a  omega          
a  Local Time Step      1.1582e-05                         44118


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3224          1.6118       0.0031061      1.2345e-06
v  Velocity[Y]                 -20.406            29.8          6.9245          20.054
v  Velocity[Z]                 -28.635          28.564         0.16965       -0.027877
v  ǁVelocityǁ                 0.006259          32.412          10.788           20.21
v  Pressure                    -385.51          344.82         -53.381          28.375
v  k                        1.6114e-09          98.112          3.7754          2.6582
v  omega                         1e-24      4.1809e+07          8764.3           12.12
v  turbulent_viscosity      6.7921e-15          2.0469        0.017383         0.19774
v  CourantNb                   0.05602          2295.2          45.549          1.3759
v  FourierNb                   0.01079           13906          82.896          0.9968
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14894        0.010784        0.044574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           13969          128.45          2.3727


 TIME FOR THE TIME STEP              184:        0.44927E+02

===============================================================


 INSTANT    0.185000000E+02   TIME STEP NUMBER             185
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.538845469E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31716E+02 0.17188E+02
   Friction velocity        uet   :  0.74115E-03 0.24927E+01
   Friction velocity        uk    :  0.13913E-01 0.36077E+01
   Dimensionless distance   yplus :  0.68390E-01 0.32146E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :       1069
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29731E+04    1845   0.40204E-02   0.44904E+00 
c  VelocityY    0.29731E+04    1845   0.40204E-02   0.00000E+00 
c  VelocityZ    0.29731E+04    1845   0.40204E-02   0.00000E+00 
c  Pressure     0.37989E+00    7100   0.34221E-01   0.17600E+00 
c  k            0.40030E+04    1280   0.74515E-04   0.52276E+01 
c  omega        0.13363E+08     536   0.59239E-04   0.42052E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00045703                             2
a  omega               -2.5566e+05                             1
a  Local Time Step      1.1168e-05                         44138


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5488          1.6341       0.0047271      1.2244e-06
v  Velocity[Y]                 -30.521          29.776          6.9436          20.055
v  Velocity[Z]                 -28.646          28.528         0.17628       -0.035329
v  ǁVelocityǁ                0.0074041          32.657          10.823          20.211
v  Pressure                    -382.92          344.63         -54.511          28.667
v  k                        7.3181e-09          92.926          3.8594          2.6361
v  omega                         1e-24      2.2164e+07          8355.6          12.035
v  turbulent_viscosity      2.4902e-15           2.031        0.017317         0.19793
v  CourantNb                  0.058472          2289.6          45.619          1.3762
v  FourierNb                   0.01079           13863           82.46          1.0011
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14912        0.010785         0.04462


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0017           13924          128.08          2.3773


 TIME FOR THE TIME STEP              185:        0.46034E+02

===============================================================


 INSTANT    0.186000000E+02   TIME STEP NUMBER             186
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.338565851E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32149E+02 0.14348E+02
   Friction velocity        uet   :  0.11165E-02 0.29003E+01
   Friction velocity        uk    :  0.18970E-01 0.38990E+01
   Dimensionless distance   yplus :  0.13277E+00 0.35356E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        552
   Nb of faces within the viscous sub-layer     :       1033
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29715E+04    1886   0.39426E-02   0.45509E+00 
c  VelocityY    0.29715E+04    1886   0.39426E-02   0.00000E+00 
c  VelocityZ    0.29715E+04    1886   0.39426E-02   0.00000E+00 
c  Pressure     0.39812E+00    7130   0.33940E-01   0.18471E+00 
c  k            0.39150E+04    1271   0.74177E-04   0.49306E+01 
c  omega        0.16834E+08     462   0.13190E-03   0.12566E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00024594                             1
a  omega               -2.0942e+05                             3
a  Local Time Step       1.114e-05                         44221


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7179          1.6487       0.0059135      4.5015e-08
v  Velocity[Y]                 -19.177          30.399          6.9968          20.054
v  Velocity[Z]                 -28.657          28.857          0.1737       -0.042105
v  ǁVelocityǁ                 0.017308          33.023          10.836           20.21
v  Pressure                    -381.45          344.76         -55.801          28.551
v  k                        1.6498e-08          64.493          3.8962          2.6123
v  omega                         1e-24      5.1289e+07          8724.2           12.02
v  turbulent_viscosity      1.3369e-14          2.0136        0.017294         0.19787
v  CourantNb                  0.030445          2734.7           45.94          1.3765
v  FourierNb                   0.01079           13923          82.913          1.0046
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14816        0.010786        0.044659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9591           13982          128.85          2.3811


 TIME FOR THE TIME STEP              186:        0.44937E+02

===============================================================


 INSTANT    0.187000000E+02   TIME STEP NUMBER             187
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.142172826E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31207E+02 0.14183E+02
   Friction velocity        uet   :  0.93509E-03 0.24253E+01
   Friction velocity        uk    :  0.16462E-01 0.30416E+01
   Dimensionless distance   yplus :  0.13392E+00 0.26500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        537
   Nb of faces within the viscous sub-layer     :       1056
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29696E+04    2206   0.41160E-02   0.46059E+00 
c  VelocityY    0.29696E+04    2206   0.41160E-02   0.00000E+00 
c  VelocityZ    0.29696E+04    2206   0.41160E-02   0.00000E+00 
c  Pressure     0.33857E+00    7008   0.31468E-01   0.15674E+00 
c  k            0.38291E+04    1235   0.60069E-04   0.45434E+01 
c  omega        0.21079E+08     326   0.48361E-04   0.53833E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.6522e-07                             1
a  omega                    -83635                             2
a  Local Time Step       1.138e-05                         44263


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8111           1.672       0.0063575     -5.4282e-10
v  Velocity[Y]                 -16.883          30.732           7.054          20.055
v  Velocity[Z]                  -28.69          28.782         0.15807       -0.048214
v  ǁVelocityǁ                0.0098689          33.345          10.831          20.211
v  Pressure                    -386.75           345.8         -56.129          28.912
v  k                          1.72e-08          68.557          3.9362          2.5871
v  omega                         1e-24      2.6831e+07          8556.5          11.999
v  turbulent_viscosity       1.871e-14          1.9964        0.017275         0.19754
v  CourantNb                  0.013253          2431.6          46.032          1.3768
v  FourierNb                  0.010788           14032          84.075          1.0063
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14895        0.010788        0.044711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8865           14089          130.11          2.3831


 TIME FOR THE TIME STEP              187:        0.49050E+02

===============================================================


 INSTANT    0.188000000E+02   TIME STEP NUMBER             188
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271358767E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31502E+02 0.13701E+02
   Friction velocity        uet   :  0.14748E-02 0.28273E+01
   Friction velocity        uk    :  0.18624E-01 0.29598E+01
   Dimensionless distance   yplus :  0.16028E+00 0.28961E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        603
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29676E+04    1898   0.40907E-02   0.47779E+00 
c  VelocityY    0.29676E+04    1898   0.40907E-02   0.00000E+00 
c  VelocityZ    0.29676E+04    1898   0.40907E-02   0.00000E+00 
c  Pressure     0.38793E+00    6992   0.29194E-01   0.17877E+00 
c  k            0.37452E+04    1310   0.60099E-04   0.43784E+01 
c  omega        0.12372E+08     450   0.72961E-03   0.28367E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00059815                             3
a  omega               -1.6942e+05                             3
a  Local Time Step      1.1425e-05                         44336


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8387          1.8588       0.0061258      1.0479e-06
v  Velocity[Y]                 -15.102          32.066          7.0932          20.055
v  Velocity[Z]                 -29.541          28.707         0.13414       -0.053613
v  ǁVelocityǁ                 0.016482          33.031          10.807          20.212
v  Pressure                    -389.06          347.14         -55.982          28.821
v  k                        1.3321e-07            53.8          3.9253          2.5603
v  omega                         1e-24      4.1889e+08           10071          12.081
v  turbulent_viscosity       1.582e-13          1.9817        0.017265         0.19695
v  CourantNb                  0.058789          2317.9           45.93          1.3771
v  FourierNb                  0.010787           14192          85.864          1.0072
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14895        0.010789         0.04475


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14247          131.79          2.3843


 TIME FOR THE TIME STEP              188:        0.46647E+02

===============================================================


 INSTANT    0.189000000E+02   TIME STEP NUMBER             189
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.869043293E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31986E+02 0.13015E+02
   Friction velocity        uet   :  0.79199E-03 0.28781E+01
   Friction velocity        uk    :  0.20626E-01 0.30025E+01
   Dimensionless distance   yplus :  0.72633E-01 0.30307E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29656E+04    1852   0.41806E-02   0.50461E+00 
c  VelocityY    0.29656E+04    1852   0.41806E-02   0.00000E+00 
c  VelocityZ    0.29656E+04    1852   0.41806E-02   0.00000E+00 
c  Pressure     0.39832E+00    6975   0.29378E-01   0.18309E+00 
c  k            0.36621E+04    1335   0.53569E-04   0.41429E+01 
c  omega        0.69732E+09     120   0.55443E-05   0.71908E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.0623e-08                             2
a  omega               -1.1473e+05                             2
a  Local Time Step      1.1506e-05                         44323


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8141          2.0176       0.0056438      1.0019e-06
v  Velocity[Y]                 -14.936           32.24          7.0736          20.055
v  Velocity[Z]                 -28.708          28.756        0.098104       -0.058072
v  ǁVelocityǁ                 0.022943          33.181          10.786          20.212
v  Pressure                    -384.82          348.29         -55.566          28.551
v  k                        2.2327e-09          49.932          3.8983          2.5322
v  omega                         1e-24      2.0957e+08            9130          12.017
v  turbulent_viscosity      3.3803e-14          1.9659        0.017241          0.1961
v  CourantNb                  0.035889          2326.1           45.66          1.3772
v  FourierNb                  0.010767           14350          87.013          1.0063
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14928        0.010789        0.044794


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14405          132.67          2.3835


 TIME FOR THE TIME STEP              189:        0.44466E+02

===============================================================


 INSTANT    0.190000000E+02   TIME STEP NUMBER             190
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.227128642E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29424E+02 0.21852E+02
   Friction velocity        uet   :  0.12902E-02 0.27850E+01
   Friction velocity        uk    :  0.17989E-01 0.38006E+01
   Dimensionless distance   yplus :  0.20090E+00 0.34181E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        520
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29636E+04    1931   0.39576E-02   0.52115E+00 
c  VelocityY    0.29636E+04    1931   0.39576E-02   0.00000E+00 
c  VelocityZ    0.29636E+04    1931   0.39576E-02   0.00000E+00 
c  Pressure     0.42310E+00    6940   0.30670E-01   0.19717E+00 
c  k            0.35810E+04    1375   0.46464E-04   0.38250E+01 
c  omega        0.17503E+09      99   0.47640E-04   0.15717E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6022e+05                             3
a  Local Time Step      1.2254e-05                         44380


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7553          2.0728       0.0051328      5.7697e-07
v  Velocity[Y]                  -15.43          31.853          7.0296          20.055
v  Velocity[Z]                 -29.639          28.806        0.063351       -0.061313
v  ǁVelocityǁ                 0.012873          32.858          10.765          20.212
v  Pressure                    -375.83          348.83          -55.17           28.45
v  k                        4.6122e-08          39.137          3.8785           2.503
v  omega                         1e-24      3.2024e+08          9625.4          12.034
v  turbulent_viscosity      1.9625e-15          1.9495        0.017201         0.19499
v  CourantNb                  0.012353          2329.9          45.321          1.3776
v  FourierNb                  0.010749           14689          86.444          1.0037
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14914        0.010789        0.044811


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14744          131.77          2.3813


 TIME FOR THE TIME STEP              190:        0.45048E+02

===============================================================


 INSTANT    0.191000000E+02   TIME STEP NUMBER             191
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.212547946E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33975E+02 0.20936E+02
   Friction velocity        uet   :  0.17921E-02 0.26608E+01
   Friction velocity        uk    :  0.17277E-01 0.32843E+01
   Dimensionless distance   yplus :  0.10466E+00 0.29767E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        536
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29613E+04    1997   0.39695E-02   0.53083E+00 
c  VelocityY    0.29613E+04    1997   0.39695E-02   0.00000E+00 
c  VelocityZ    0.29613E+04    1997   0.39695E-02   0.00000E+00 
c  Pressure     0.36870E+00    6982   0.28835E-01   0.17049E+00 
c  k            0.35024E+04    1366   0.45163E-04   0.36590E+01 
c  omega        0.40175E+09      79   0.84122E-05   0.39609E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80383                             2
a  Local Time Step      1.1916e-05                         44444


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6559           2.009        0.004748      2.1328e-07
v  Velocity[Y]                 -17.816          30.264          6.9996          20.054
v  Velocity[Z]                 -30.304          28.665         0.03024       -0.063874
v  ǁVelocityǁ                0.0084684          36.738          10.753          20.211
v  Pressure                    -364.07          349.73         -54.194          28.541
v  k                         3.033e-08          39.889          3.8687          2.4725
v  omega                         1e-24      1.6027e+08          8701.8          11.976
v  turbulent_viscosity      1.9271e-15          1.9336         0.01717         0.19362
v  CourantNb                  0.035348          2332.5          45.362           1.378
v  FourierNb                  0.010733           15074          86.776          1.0006
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14926        0.010789        0.044868


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91708           15131          132.14          2.3786


 TIME FOR THE TIME STEP              191:        0.44958E+02

===============================================================


 INSTANT    0.192000000E+02   TIME STEP NUMBER             192
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.459196479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29971E+02 0.19829E+02
   Friction velocity        uet   :  0.15163E-02 0.29620E+01
   Friction velocity        uk    :  0.10712E-01 0.29666E+01
   Dimensionless distance   yplus :  0.10599E+00 0.27737E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        485
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29591E+04    2006   0.40687E-02   0.53273E+00 
c  VelocityY    0.29591E+04    2006   0.40687E-02   0.00000E+00 
c  VelocityZ    0.29591E+04    2006   0.40687E-02   0.00000E+00 
c  Pressure     0.39981E+00    7053   0.29631E-01   0.18558E+00 
c  k            0.34274E+04    1266   0.45509E-04   0.35351E+01 
c  omega        0.10147E+09     104   0.16597E-04   0.10188E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00028198                             2
a  omega               -3.0275e+05                             4
a  Local Time Step      1.1832e-05                         44511


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5586          1.8355       0.0040086     -1.4238e-06
v  Velocity[Y]                 -15.141          31.912          7.0075          20.053
v  Velocity[Z]                 -30.852          28.749       0.0052676       -0.064934
v  ǁVelocityǁ                  0.01131          37.521          10.765           20.21
v  Pressure                    -366.47          350.49         -52.729          29.171
v  k                        2.5674e-08          51.602           3.868           2.441
v  omega                         1e-24      8.0488e+07          8237.1          11.952
v  turbulent_viscosity      6.7327e-16           1.919        0.017134         0.19199
v  CourantNb                  0.020339          2348.2           45.32          1.3781
v  FourierNb                  0.010719           15454          87.014         0.99665
v  total_pressure           1.0096e+05      1.0168e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14875         0.01079        0.044903


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15513          132.33          2.3747


 TIME FOR THE TIME STEP              192:        0.44535E+02

===============================================================


 INSTANT    0.193000000E+02   TIME STEP NUMBER             193
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.166295894E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30980E+02 0.14067E+02
   Friction velocity        uet   :  0.73574E-03 0.31571E+01
   Friction velocity        uk    :  0.67291E-02 0.31923E+01
   Dimensionless distance   yplus :  0.78656E-01 0.27899E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        500
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29570E+04    1978   0.42960E-02   0.53853E+00 
c  VelocityY    0.29570E+04    1978   0.42960E-02   0.00000E+00 
c  VelocityZ    0.29570E+04    1978   0.42960E-02   0.00000E+00 
c  Pressure     0.39580E+00    6988   0.32295E-01   0.18255E+00 
c  k            0.33576E+04     865   0.47949E-04   0.34181E+01 
c  omega        0.27795E+08     163   0.48898E-04   0.66390E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00026151                             1
a  omega               -1.9941e+05                             1
a  Local Time Step      1.1728e-05                         44580


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5948          1.9934       0.0027963     -4.0212e-07
v  Velocity[Y]                 -14.963          34.745          7.0431          20.053
v  Velocity[Z]                 -32.925          28.451         0.00852       -0.065086
v  ǁVelocityǁ                  0.01163          37.319          10.795           20.21
v  Pressure                    -417.62          350.96         -51.088          29.846
v  k                        5.7644e-08          62.115           3.866          2.4083
v  omega                         1e-24      4.2346e+07            8337          11.965
v  turbulent_viscosity      5.6001e-15          1.9039        0.017105         0.19012
v  CourantNb                  0.036432          2483.2          45.169          1.3781
v  FourierNb                  0.010707           15714          86.896           0.992
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0135e+05
v  Local Time Step                0.01         0.14758        0.010791         0.04496


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15775          132.07          2.3701


 TIME FOR THE TIME STEP              193:        0.43307E+02

===============================================================


 INSTANT    0.194000000E+02   TIME STEP NUMBER             194
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.529329649E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28823E+02 0.13748E+02
   Friction velocity        uet   :  0.18002E-03 0.33747E+01
   Friction velocity        uk    :  0.19898E-01 0.30765E+01
   Dimensionless distance   yplus :  0.19755E+00 0.27787E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        470
   Nb of faces within the viscous sub-layer     :        950
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29551E+04    1978   0.42500E-02   0.54224E+00 
c  VelocityY    0.29551E+04    1978   0.42500E-02   0.00000E+00 
c  VelocityZ    0.29551E+04    1978   0.42500E-02   0.00000E+00 
c  Pressure     0.39894E+00    7096   0.35624E-01   0.18312E+00 
c  k            0.32935E+04    1245   0.50158E-04   0.32522E+01 
c  omega        0.17990E+08     239   0.16531E-03   0.28348E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00084445                             1
a  omega               -3.3739e+05                             1
a  Local Time Step      1.2477e-05                         44588


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8419          2.0396       0.0010458     -1.7286e-06
v  Velocity[Y]                 -16.418          31.359          7.0739          20.055
v  Velocity[Z]                 -32.798          28.489        0.038166       -0.063954
v  ǁVelocityǁ                0.0089361          34.597          10.793          20.212
v  Pressure                    -437.58          351.09         -49.689          30.599
v  k                        1.2808e-07          63.228          3.8322          2.3746
v  omega                         1e-24      1.1543e+08          8548.5          11.972
v  turbulent_viscosity      1.0384e-14          1.8878         0.01707         0.18801
v  CourantNb                  0.015951          2909.9          45.191          1.3782
v  FourierNb                  0.010696           15750          87.497         0.98662
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010792        0.045011


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15813          132.69          2.3648


 TIME FOR THE TIME STEP              194:        0.46366E+02

===============================================================


 INSTANT    0.195000000E+02   TIME STEP NUMBER             195
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.610213123E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30341E+02 0.14192E+02
   Friction velocity        uet   :  0.24072E-02 0.31211E+01
   Friction velocity        uk    :  0.19958E-01 0.30207E+01
   Dimensionless distance   yplus :  0.15208E+00 0.27708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        442
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29532E+04    1956   0.42041E-02   0.52240E+00 
c  VelocityY    0.29532E+04    1956   0.42041E-02   0.00000E+00 
c  VelocityZ    0.29532E+04    1956   0.42041E-02   0.00000E+00 
c  Pressure     0.41810E+00    7074   0.35030E-01   0.19227E+00 
c  k            0.32317E+04    1401   0.48622E-04   0.31220E+01 
c  omega        0.71425E+08     120   0.19387E-04   0.10579E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030217                             2
a  omega          
a  Local Time Step      1.2191e-05                         44623


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0785          2.1375      -0.0011319     -2.4051e-06
v  Velocity[Y]                 -22.458          30.178          7.0555          20.055
v  Velocity[Z]                  -32.99          28.539        0.073721         -0.0617
v  ǁVelocityǁ                 0.018754          34.344          10.759          20.212
v  Pressure                    -438.78          351.09          -49.18          30.756
v  k                        1.9854e-07          53.569          3.7739          2.3396
v  omega                         1e-24      5.7966e+07          8476.7          11.996
v  turbulent_viscosity      4.8365e-14          1.8718        0.016983         0.18569
v  CourantNb                  0.013993            2737          45.321          1.3784
v  FourierNb                  0.010687           15643          87.147         0.98009
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14806        0.010793        0.045072


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15706          132.47          2.3585


 TIME FOR THE TIME STEP              195:        0.45443E+02

===============================================================


 INSTANT    0.196000000E+02   TIME STEP NUMBER             196
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.233405686E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30958E+02 0.14007E+02
   Friction velocity        uet   :  0.23375E-02 0.28949E+01
   Friction velocity        uk    :  0.24664E-01 0.30310E+01
   Dimensionless distance   yplus :  0.12313E+00 0.27312E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        411
   Nb of faces within the viscous sub-layer     :       1066
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29513E+04    1916   0.42265E-02   0.49763E+00 
c  VelocityY    0.29513E+04    1916   0.42265E-02   0.00000E+00 
c  VelocityZ    0.29513E+04    1916   0.42265E-02   0.00000E+00 
c  Pressure     0.41731E+00    7031   0.32271E-01   0.19338E+00 
c  k            0.31681E+04    1430   0.49995E-04   0.29677E+01 
c  omega        0.25663E+08     166   0.30475E-04   0.75520E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011108                             1
a  omega               -1.8371e+05                             1
a  Local Time Step      1.0748e-05                         44633


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3225          2.1313      -0.0033646     -2.7815e-06
v  Velocity[Y]                 -29.482          30.056          6.9742          20.055
v  Velocity[Z]                 -31.053          28.793         0.10129       -0.058509
v  ǁVelocityǁ                 0.013022           32.82          10.727          20.212
v  Pressure                    -423.65          351.38         -49.031          31.036
v  k                        3.7258e-07          55.121          3.7486          2.3037
v  omega                         1e-24      2.9487e+07          8650.6          12.051
v  turbulent_viscosity      2.2113e-14          1.8585        0.016854         0.18316
v  CourantNb                  0.018202          2450.4          45.281          1.3785
v  FourierNb                   0.01068           15322          86.138         0.97227
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14922        0.010795         0.04511


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15385          131.42          2.3507


 TIME FOR THE TIME STEP              196:        0.44967E+02

===============================================================


 INSTANT    0.197000000E+02   TIME STEP NUMBER             197
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.150324848E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31576E+02 0.19433E+02
   Friction velocity        uet   :  0.23889E-02 0.27633E+01
   Friction velocity        uk    :  0.28800E-01 0.31223E+01
   Dimensionless distance   yplus :  0.12636E+00 0.27300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :       1065
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29496E+04    1847   0.43206E-02   0.48471E+00 
c  VelocityY    0.29496E+04    1847   0.43206E-02   0.00000E+00 
c  VelocityZ    0.29496E+04    1847   0.43206E-02   0.00000E+00 
c  Pressure     0.44377E+00    6984   0.32290E-01   0.20674E+00 
c  k            0.30993E+04    1380   0.62919E-04   0.27743E+01 
c  omega        0.15286E+08     293   0.32340E-04   0.37872E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012842                             2
a  omega               -1.1485e+05                             1
a  Local Time Step      1.1402e-05                         44620


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5032          2.1133      -0.0049508     -2.0372e-06
v  Velocity[Y]                 -22.236          30.015          6.8953          20.055
v  Velocity[Z]                 -28.867          28.587           0.103       -0.054127
v  ǁVelocityǁ                 0.014192          33.113          10.747          20.213
v  Pressure                    -403.88           351.3         -49.945           31.25
v  k                        3.3983e-07          90.089          3.7935           2.267
v  omega                         1e-24      1.5744e+07          8390.1          12.009
v  turbulent_viscosity      6.0035e-14          1.8438        0.016715         0.18046
v  CourantNb                  0.020918          2439.5          45.218          1.3784
v  FourierNb                  0.010673           14997          86.039         0.96378
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14812        0.010796        0.045142


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15060          131.26          2.3422


 TIME FOR THE TIME STEP              197:        0.43464E+02

===============================================================


 INSTANT    0.198000000E+02   TIME STEP NUMBER             198
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.793039891E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31670E+02 0.14885E+02
   Friction velocity        uet   :  0.11536E-02 0.24840E+01
   Friction velocity        uk    :  0.16152E-01 0.30643E+01
   Dimensionless distance   yplus :  0.44716E-01 0.27019E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1073
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29481E+04    1815   0.43154E-02   0.48626E+00 
c  VelocityY    0.29481E+04    1815   0.43154E-02   0.00000E+00 
c  VelocityZ    0.29481E+04    1815   0.43154E-02   0.00000E+00 
c  Pressure     0.43127E+00    7036   0.34453E-01   0.20072E+00 
c  k            0.30224E+04    1285   0.83446E-04   0.25817E+01 
c  omega        0.12187E+08     509   0.75626E-04   0.56734E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00041958                             1
a  omega               -2.5238e+05                             1
a  Local Time Step      1.1174e-05                         44604


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5898          2.0777      -0.0055768     -2.4164e-06
v  Velocity[Y]                 -31.496          29.938          6.8944          20.055
v  Velocity[Z]                 -28.861          28.879         0.10092       -0.048611
v  ǁVelocityǁ                0.0049653          33.137          10.785          20.213
v  Pressure                    -404.78          352.03         -50.891          32.002
v  k                        2.2445e-09          84.234           3.881            2.23
v  omega                         1e-24      2.7153e+07          8488.1          12.004
v  turbulent_viscosity      9.0835e-14           1.829         0.01659         0.17762
v  CourantNb                  0.054739          2409.7          45.261          1.3786
v  FourierNb                  0.010668           14936          86.431         0.95476
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010797        0.045181


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14993          131.69          2.3333


 TIME FOR THE TIME STEP              198:        0.43610E+02

===============================================================


 INSTANT    0.199000000E+02   TIME STEP NUMBER             199
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.512324437E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32441E+02 0.15296E+02
   Friction velocity        uet   :  0.19152E-02 0.29844E+01
   Friction velocity        uk    :  0.12397E-01 0.32120E+01
   Dimensionless distance   yplus :  0.11194E+00 0.32487E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :       1077
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29468E+04    1968   0.42796E-02   0.48946E+00 
c  VelocityY    0.29468E+04    1968   0.42796E-02   0.00000E+00 
c  VelocityZ    0.29468E+04    1968   0.42796E-02   0.00000E+00 
c  Pressure     0.39347E+00    6976   0.35263E-01   0.18311E+00 
c  k            0.29417E+04    1253   0.88023E-04   0.23735E+01 
c  omega        0.12409E+08     446   0.25946E-03   0.23604E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2114e+05                             2
a  Local Time Step      1.0883e-05                         44536


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5708          2.1603      -0.0050586     -1.7815e-06
v  Velocity[Y]                 -20.376          30.501          6.9291          20.056
v  Velocity[Z]                  -28.55          28.859        0.088485       -0.042554
v  ǁVelocityǁ                0.0066633          33.303          10.804          20.213
v  Pressure                    -403.82          352.69         -52.212          32.443
v  k                        2.0706e-08          75.102          3.9433          2.1928
v  omega                         1e-24      5.9933e+07          9282.9          12.028
v  turbulent_viscosity      9.1509e-16           1.822          0.0165         0.17465
v  CourantNb                  0.066578          2928.1          45.717          1.3789
v  FourierNb                  0.010653           14895          87.291         0.94582
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889        0.010799        0.045258


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14948          133.01          2.3247


 TIME FOR THE TIME STEP              199:        0.44718E+02

===============================================================


 INSTANT    0.200000000E+02   TIME STEP NUMBER             200
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.279335584E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31391E+02 0.14102E+02
   Friction velocity        uet   :  0.18466E-02 0.27245E+01
   Friction velocity        uk    :  0.20761E-01 0.30204E+01
   Dimensionless distance   yplus :  0.88627E-01 0.27339E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1053
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29456E+04    2259   0.43542E-02   0.49513E+00 
c  VelocityY    0.29456E+04    2259   0.43542E-02   0.00000E+00 
c  VelocityZ    0.29456E+04    2259   0.43542E-02   0.00000E+00 
c  Pressure     0.41233E+00    6978   0.32741E-01   0.19072E+00 
c  k            0.28625E+04     925   0.81070E-04   0.21304E+01 
c  omega        0.28945E+08     317   0.10115E-03   0.28936E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.8365e+05                             1
a  Local Time Step      1.0573e-05                         44465


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4388          2.2386      -0.0040731     -2.2544e-06
v  Velocity[Y]                 -17.807          31.918          6.9798          20.055
v  Velocity[Z]                 -28.708          29.092        0.068853       -0.035658
v  ǁVelocityǁ                0.0090606          33.505          10.789          20.213
v  Pressure                    -411.61          353.87         -52.563          32.901
v  k                        1.8313e-10          81.648          3.9866          2.1555
v  omega                         1e-24      1.2514e+08          9139.7          12.015
v  turbulent_viscosity      1.0599e-14          1.8046        0.016419          0.1716
v  CourantNb                  0.027401          2577.2          45.844          1.3792
v  FourierNb                  0.010636           14854          88.437         0.93681
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010802        0.045351


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14905          134.28           2.316


 TIME FOR THE TIME STEP              200:        0.47244E+02

===============================================================


 INSTANT    0.201000000E+02   TIME STEP NUMBER             201
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.392981118E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31607E+02 0.14384E+02
   Friction velocity        uet   :  0.20460E-02 0.28974E+01
   Friction velocity        uk    :  0.19662E-01 0.32500E+01
   Dimensionless distance   yplus :  0.17586E+00 0.27252E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        557
   Nb of faces within the viscous sub-layer     :       1093
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29446E+04    1896   0.46233E-02   0.50585E+00 
c  VelocityY    0.29446E+04    1896   0.46233E-02   0.00000E+00 
c  VelocityZ    0.29446E+04    1896   0.46233E-02   0.00000E+00 
c  Pressure     0.40995E+00    6998   0.29809E-01   0.18958E+00 
c  k            0.27839E+04    1096   0.80807E-04   0.22021E+01 
c  omega        0.62703E+08     334   0.23896E-04   0.86328E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2849e+05                             1
a  Local Time Step      1.1475e-05                         44434


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2069          2.3927      -0.0030067     -2.3413e-06
v  Velocity[Y]                   -15.9          32.519          7.0108          20.055
v  Velocity[Z]                 -28.486          28.821        0.056432       -0.028584
v  ǁVelocityǁ                 0.013117          33.411          10.739          20.213
v  Pressure                    -423.96          354.67         -52.208          33.079
v  k                        3.8857e-08          61.186          3.9541          2.1183
v  omega                         1e-24      6.3024e+07          8692.9          11.978
v  turbulent_viscosity      3.1678e-16          1.7817        0.016336         0.16849
v  CourantNb                  0.025844            2339          45.822          1.3795
v  FourierNb                  0.010623           14793          89.776         0.92781
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010804         0.04539


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14845           135.6          2.3073


 TIME FOR THE TIME STEP              201:        0.43519E+02

===============================================================


 INSTANT    0.202000000E+02   TIME STEP NUMBER             202
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.940049738E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30799E+02 0.15773E+02
   Friction velocity        uet   :  0.12326E-02 0.28261E+01
   Friction velocity        uk    :  0.15862E-01 0.30144E+01
   Dimensionless distance   yplus :  0.13262E+00 0.30223E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29435E+04    1956   0.43988E-02   0.51784E+00 
c  VelocityY    0.29435E+04    1956   0.43988E-02   0.00000E+00 
c  VelocityZ    0.29435E+04    1956   0.43988E-02   0.00000E+00 
c  Pressure     0.45491E+00    7007   0.30106E-01   0.21138E+00 
c  k            0.27030E+04    1108   0.66043E-04   0.20929E+01 
c  omega        0.22679E+08     309   0.34280E-04   0.28830E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034528                             1
a  omega                -3.135e+05                             1
a  Local Time Step      1.1364e-05                         44433


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1407          2.1583      -0.0014744     -2.3384e-06
v  Velocity[Y]                 -15.044          32.427          6.9909          20.056
v  Velocity[Z]                 -28.849          28.753        0.030885       -0.021408
v  ǁVelocityǁ                 0.013763          33.097          10.705          20.213
v  Pressure                    -425.81          353.83         -51.938          32.712
v  k                        1.4066e-07          88.568          3.9144          2.0817
v  omega                         1e-24      3.2464e+07          8379.4          11.919
v  turbulent_viscosity      4.0965e-14          1.7483        0.016225         0.16535
v  CourantNb                  0.038074            2321          45.519          1.3796
v  FourierNb                  0.010613           14694          89.235         0.91817
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010807        0.045461


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88443           14750          134.75          2.2978


 TIME FOR THE TIME STEP              202:        0.45650E+02

===============================================================


 INSTANT    0.203000000E+02   TIME STEP NUMBER             203
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.132301725E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33228E+02 0.18036E+02
   Friction velocity        uet   :  0.88858E-03 0.27660E+01
   Friction velocity        uk    :  0.15837E-01 0.39151E+01
   Dimensionless distance   yplus :  0.14348E+00 0.36169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        416
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1998   0.41440E-02   0.53367E+00 
c  VelocityY    0.29424E+04    1998   0.41440E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1998   0.41440E-02   0.00000E+00 
c  Pressure     0.44214E+00    6922   0.30574E-01   0.20505E+00 
c  k            0.26256E+04    1248   0.50347E-04   0.19106E+01 
c  omega        0.12924E+08     268   0.36640E-04   0.27989E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00044975                             1
a  omega                     -7151                             1
a  Local Time Step      1.1928e-05                         44455


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3608          2.1417      -0.0002587       5.495e-07
v  Velocity[Y]                 -15.044          31.867          6.9568          20.055
v  Velocity[Z]                 -28.921           28.62       -0.005609       -0.013986
v  ǁVelocityǁ                 0.013125          32.678            10.7          20.212
v  Pressure                    -417.55          352.54         -51.568          32.297
v  k                        8.0645e-08          107.82          3.8743          2.0459
v  omega                         1e-24      1.9361e+07          8151.8          11.889
v  turbulent_viscosity       2.535e-14          1.7074        0.016102          0.1622
v  CourantNb                  0.012673          2300.7          45.058          1.3796
v  FourierNb                    0.0106           14589          88.316         0.90806
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010809        0.045511


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88693           14652          133.37          2.2877


 TIME FOR THE TIME STEP              203:        0.44850E+02

===============================================================


 INSTANT    0.204000000E+02   TIME STEP NUMBER             204
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.345234086E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30587E+02 0.20820E+02
   Friction velocity        uet   :  0.22024E-02 0.26598E+01
   Friction velocity        uk    :  0.15852E-01 0.34061E+01
   Dimensionless distance   yplus :  0.13195E+00 0.32677E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :        952
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1984   0.41668E-02   0.53580E+00 
c  VelocityY    0.29411E+04    1984   0.41668E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1984   0.41668E-02   0.00000E+00 
c  Pressure     0.42067E+00    6994   0.28926E-01   0.19582E+00 
c  k            0.25524E+04    1263   0.52792E-04   0.19444E+01 
c  omega        0.11881E+08     190   0.21395E-04   0.11722E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00042173                             1
a  omega          
a  Local Time Step      1.1058e-05                         44483


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4725          2.1866      0.00063576       7.583e-08
v  Velocity[Y]                 -14.876          30.405          6.9419          20.054
v  Velocity[Z]                 -30.108          28.741       -0.035567      -0.0070226
v  ǁVelocityǁ                0.0059841          34.829           10.71          20.211
v  Pressure                     -403.4          352.18         -50.231          32.594
v  k                         6.808e-08          113.58           3.845          2.0112
v  omega                         1e-24      1.2435e+07          7994.8          11.863
v  turbulent_viscosity      8.1477e-15          1.6593         0.01598         0.15906
v  CourantNb                  0.053344          2275.7           44.95          1.3798
v  FourierNb                  0.010589           14464          87.436         0.89793
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010811        0.045543


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14534          132.39          2.2778


 TIME FOR THE TIME STEP              204:        0.45725E+02

===============================================================


 INSTANT    0.205000000E+02   TIME STEP NUMBER             205
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.250394602E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30863E+02 0.20412E+02
   Friction velocity        uet   :  0.73288E-03 0.27981E+01
   Friction velocity        uk    :  0.17105E-01 0.31298E+01
   Dimensionless distance   yplus :  0.15772E+00 0.32664E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        385
   Nb of faces within the viscous sub-layer     :        948
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1988   0.43060E-02   0.52127E+00 
c  VelocityY    0.29400E+04    1988   0.43060E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1988   0.43060E-02   0.00000E+00 
c  Pressure     0.42527E+00    6778   0.29921E-01   0.19819E+00 
c  k            0.24858E+04    1278   0.56526E-04   0.20249E+01 
c  omega        0.10729E+08     315   0.86250E-04   0.33259E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -24103                             1
a  Local Time Step      1.1701e-05                         44467


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4308          2.2335       0.0012892     -1.9113e-06
v  Velocity[Y]                 -15.084          30.712           6.965          20.055
v  Velocity[Z]                 -30.842          28.694       -0.047354     -0.00042247
v  ǁVelocityǁ                 0.010132          37.021          10.757          20.212
v  Pressure                    -388.84          352.02         -48.715          32.956
v  k                        1.1527e-07          96.942          3.8362          1.9777
v  omega                         1e-24      4.0388e+07          8091.1          11.863
v  turbulent_viscosity      9.8638e-15          1.6074         0.01587         0.15596
v  CourantNb                  0.013075          2254.4          44.961          1.3797
v  FourierNb                   0.01058           14367          87.175         0.88729
v  total_pressure           1.0094e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010813        0.045564


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95222           14431          132.14           2.267


 TIME FOR THE TIME STEP              205:        0.45215E+02

===============================================================


 INSTANT    0.206000000E+02   TIME STEP NUMBER             206
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.248297567E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31150E+02 0.17121E+02
   Friction velocity        uet   :  0.11114E-02 0.30652E+01
   Friction velocity        uk    :  0.22595E-01 0.33079E+01
   Dimensionless distance   yplus :  0.81442E-01 0.38009E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        409
   Nb of faces within the viscous sub-layer     :        937
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1968   0.43279E-02   0.50859E+00 
c  VelocityY    0.29389E+04    1968   0.43279E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1968   0.43279E-02   0.00000E+00 
c  Pressure     0.41370E+00    7081   0.33947E-01   0.19225E+00 
c  k            0.24297E+04    1255   0.62841E-04   0.20937E+01 
c  omega        0.12714E+08     232   0.47709E-04   0.22883E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2909e+05                             1
a  Local Time Step      1.2109e-05                         44446


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2827          2.2737       0.0013113     -3.3475e-06
v  Velocity[Y]                 -14.877          33.556          7.0204          20.055
v  Velocity[Z]                 -32.077          28.773       -0.030236       0.0054932
v  ǁVelocityǁ                 0.011161          36.594          10.823          20.212
v  Pressure                    -404.52          351.45         -47.309          33.257
v  k                        1.0615e-07          67.506          3.8367          1.9457
v  omega                         1e-24      2.1461e+07          8163.5          11.863
v  turbulent_viscosity      1.6697e-14           1.554        0.015779         0.15289
v  CourantNb                    0.0724          2410.1          45.126          1.3796
v  FourierNb                  0.010574           14386          86.674         0.87564
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010815        0.045594


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14450           131.8          2.2552


 TIME FOR THE TIME STEP              206:        0.44546E+02

===============================================================


 INSTANT    0.207000000E+02   TIME STEP NUMBER             207
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.446430493E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31643E+02 0.13862E+02
   Friction velocity        uet   :  0.16053E-02 0.32673E+01
   Friction velocity        uk    :  0.11322E-01 0.34172E+01
   Dimensionless distance   yplus :  0.10054E+00 0.39264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        409
   Nb of faces within the viscous sub-layer     :        938
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1850   0.42203E-02   0.50439E+00 
c  VelocityY    0.29379E+04    1850   0.42203E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1850   0.42203E-02   0.00000E+00 
c  Pressure     0.40897E+00    6993   0.38661E-01   0.19067E+00 
c  k            0.23860E+04    1271   0.68203E-04   0.20800E+01 
c  omega        0.10725E+08     296   0.24580E-03   0.23881E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011987                             1
a  omega          
a  Local Time Step      1.1709e-05                         44477


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0283           2.301      0.00054775     -5.1048e-06
v  Velocity[Y]                 -17.026          30.565          7.0725          20.056
v  Velocity[Z]                 -31.386          28.728        0.023397        0.010356
v  ǁVelocityǁ                 0.019566          33.425          10.861          20.213
v  Pressure                    -426.24          350.31         -46.753          33.325
v  k                        3.0175e-08          69.417          3.8162          1.9151
v  omega                         1e-24       1.191e+08          8312.9          11.883
v  turbulent_viscosity      1.5371e-14          1.5147        0.015702         0.14989
v  CourantNb                   0.05875          2858.1          45.307          1.3796
v  FourierNb                  0.010572           14340          87.334         0.86383
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14921        0.010818        0.045624


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14405          132.64          2.2434


 TIME FOR THE TIME STEP              207:        0.43518E+02

===============================================================


 INSTANT    0.208000000E+02   TIME STEP NUMBER             208
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.111014173E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30829E+02 0.14109E+02
   Friction velocity        uet   :  0.24528E-02 0.30859E+01
   Friction velocity        uk    :  0.16730E-01 0.28712E+01
   Dimensionless distance   yplus :  0.17418E+00 0.32753E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29369E+04    1774   0.42385E-02   0.47469E+00 
c  VelocityY    0.29369E+04    1774   0.42385E-02   0.00000E+00 
c  VelocityZ    0.29369E+04    1774   0.42385E-02   0.00000E+00 
c  Pressure     0.41014E+00    6842   0.38940E-01   0.19200E+00 
c  k            0.23514E+04    1142   0.70978E-04   0.20976E+01 
c  omega        0.66068E+08     124   0.19461E-04   0.10093E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00031944                             1
a  omega          
a  Local Time Step      1.1529e-05                         44435


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7158            2.34     -0.00025382     -5.2274e-06
v  Velocity[Y]                 -22.814          30.231          7.0601          20.055
v  Velocity[Z]                 -31.609          28.777        0.090344        0.014439
v  ǁVelocityǁ                  0.01461          32.709          10.823          20.212
v  Pressure                    -426.23          350.14         -46.292          33.259
v  k                        7.5597e-08          58.497          3.7777          1.8858
v  omega                         1e-24      5.9783e+07          8296.1          11.902
v  turbulent_viscosity      4.3682e-15          1.4968        0.015597         0.14697
v  CourantNb                  0.049153          2701.6          45.667          1.3797
v  FourierNb                  0.010568           14238          86.828         0.85107
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14824        0.010821        0.045641


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97508           14302          132.49          2.2308


 TIME FOR THE TIME STEP              208:        0.41480E+02

===============================================================


 INSTANT    0.209000000E+02   TIME STEP NUMBER             209
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.207205395E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.35548E+02 0.14118E+02
   Friction velocity        uet   :  0.20220E-02 0.27958E+01
   Friction velocity        uk    :  0.23903E-01 0.29164E+01
   Dimensionless distance   yplus :  0.12049E+00 0.26034E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :        953
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29360E+04    1701   0.42926E-02   0.44320E+00 
c  VelocityY    0.29360E+04    1701   0.42926E-02   0.00000E+00 
c  VelocityZ    0.29360E+04    1701   0.42926E-02   0.00000E+00 
c  Pressure     0.41961E+00    7062   0.34045E-01   0.19691E+00 
c  k            0.23201E+04     968   0.73060E-04   0.20857E+01 
c  omega        0.20282E+08     228   0.36098E-04   0.53300E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0013843                             2
a  omega          
a  Local Time Step      1.1553e-05                         44437


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5824          2.5614     -0.00082082     -3.9406e-06
v  Velocity[Y]                 -31.271           30.08          6.9726          20.055
v  Velocity[Z]                 -30.992          28.907         0.13167        0.017833
v  ǁVelocityǁ                 0.012376          32.941          10.763          20.212
v  Pressure                     -412.3          350.08         -46.351          33.264
v  k                        2.2163e-08           55.85          3.7694          1.8578
v  omega                         1e-24      3.0369e+07          8191.9          11.914
v  turbulent_viscosity       1.094e-14          1.4863        0.015468         0.14412
v  CourantNb                  0.021716          2222.6          45.578          1.3796
v  FourierNb                  0.010567           14118          85.815          0.8374
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14793        0.010824        0.045654


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76791           14181          131.39           2.217


 TIME FOR THE TIME STEP              209:        0.42836E+02

===============================================================


 INSTANT    0.210000000E+02   TIME STEP NUMBER             210
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.322794727E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31863E+02 0.21628E+02
   Friction velocity        uet   :  0.24405E-02 0.28610E+01
   Friction velocity        uk    :  0.22957E-01 0.29105E+01
   Dimensionless distance   yplus :  0.10717E+00 0.26038E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29351E+04    1630   0.43142E-02   0.42222E+00 
c  VelocityY    0.29351E+04    1630   0.43142E-02   0.00000E+00 
c  VelocityZ    0.29351E+04    1630   0.43142E-02   0.00000E+00 
c  Pressure     0.42363E+00    6996   0.32352E-01   0.19827E+00 
c  k            0.22857E+04    1281   0.89716E-04   0.19584E+01 
c  omega        0.11471E+08     298   0.39513E-04   0.63030E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030124                             2
a  omega          
a  Local Time Step        1.12e-05                         44424


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6364          2.7129      -0.0013094     -1.5068e-06
v  Velocity[Y]                 -22.194          29.937          6.8662          20.055
v  Velocity[Z]                 -29.505          28.794         0.14804        0.020308
v  ǁVelocityǁ                0.0081919          33.255          10.736          20.212
v  Pressure                    -398.82          349.99         -46.812          33.235
v  k                        5.2193e-07          83.739          3.8278          1.8313
v  omega                         1e-24      1.6143e+07          8400.1           11.95
v  turbulent_viscosity      5.5236e-15          1.4789        0.015349         0.14137
v  CourantNb                  0.043289          2225.5          45.386          1.3794
v  FourierNb                  0.010566           14118          86.079         0.82427
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14749        0.010827        0.045659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14180          131.47          2.2036


 TIME FOR THE TIME STEP              210:        0.43641E+02

===============================================================


 INSTANT    0.211000000E+02   TIME STEP NUMBER             211
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.231159990E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30709E+02 0.17177E+02
   Friction velocity        uet   :  0.19137E-02 0.25457E+01
   Friction velocity        uk    :  0.17104E-01 0.35815E+01
   Dimensionless distance   yplus :  0.96404E-01 0.30964E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        424
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29344E+04    1745   0.41015E-02   0.41069E+00 
c  VelocityY    0.29344E+04    1745   0.41015E-02   0.00000E+00 
c  VelocityZ    0.29344E+04    1745   0.41015E-02   0.00000E+00 
c  Pressure     0.42908E+00    7070   0.36515E-01   0.20185E+00 
c  k            0.22474E+04    1437   0.10072E-03   0.17862E+01 
c  omega        0.10851E+08     465   0.75491E-04   0.68467E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00065956                             1
a  omega               -2.5098e+05                             1
a  Local Time Step      1.1537e-05                         44416


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7656          2.7327       -0.001746      1.2378e-06
v  Velocity[Y]                 -36.282          30.313          6.8348          20.055
v  Velocity[Z]                  -28.57          29.021         0.15983        0.022227
v  ǁVelocityǁ                 0.011408          36.683          10.723          20.212
v  Pressure                    -403.28          350.07          -47.74          33.582
v  k                         2.349e-08           75.76          3.8812          1.8062
v  omega                         1e-24      2.1255e+07          8567.5          11.961
v  turbulent_viscosity       7.551e-14          1.4727        0.015258          0.1387
v  CourantNb                  0.036807          2230.9          45.335          1.3791
v  FourierNb                   0.01057           14207          87.349         0.81226
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14827         0.01083        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14263          132.68          2.1914


 TIME FOR THE TIME STEP              211:        0.45794E+02

===============================================================


 INSTANT    0.212000000E+02   TIME STEP NUMBER             212
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.459065487E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39074E+02 0.14934E+02
   Friction velocity        uet   :  0.33025E-02 0.34063E+01
   Friction velocity        uk    :  0.15413E-01 0.39476E+01
   Dimensionless distance   yplus :  0.64122E-01 0.37262E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29338E+04    1867   0.42823E-02   0.39784E+00 
c  VelocityY    0.29338E+04    1867   0.42823E-02   0.00000E+00 
c  VelocityZ    0.29338E+04    1867   0.42823E-02   0.00000E+00 
c  Pressure     0.40915E+00    7128   0.39061E-01   0.19182E+00 
c  k            0.22091E+04    1515   0.92798E-04   0.16455E+01 
c  omega        0.11449E+08     389   0.11691E-03   0.15446E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0002394                             1
a  omega                   -2789.2                             1
a  Local Time Step      1.1474e-05                         44430


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8115          2.6082      -0.0017792       -3.02e-07
v  Velocity[Y]                 -22.972          30.786           6.841          20.055
v  Velocity[Z]                 -28.867           28.98          0.1484        0.023598
v  ǁVelocityǁ                 0.010771          33.772          10.703          20.212
v  Pressure                    -406.27          349.98         -48.861          33.929
v  k                        4.9739e-09          49.018          3.9012          1.7824
v  omega                         1e-24      3.4411e+07          8973.4           11.98
v  turbulent_viscosity      1.0529e-14          1.4654        0.015205         0.13612
v  CourantNb                  0.035947          3272.3          45.682           1.379
v  FourierNb                  0.010572           14332          87.664         0.80096
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010831        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14386          133.35            2.18


 TIME FOR THE TIME STEP              212:        0.46399E+02

===============================================================


 INSTANT    0.213000000E+02   TIME STEP NUMBER             213
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.181775785E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30933E+02 0.13672E+02
   Friction velocity        uet   :  0.25089E-02 0.26737E+01
   Friction velocity        uk    :  0.16731E-01 0.29750E+01
   Dimensionless distance   yplus :  0.14018E+00 0.26588E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29334E+04    1882   0.44738E-02   0.38902E+00 
c  VelocityY    0.29334E+04    1882   0.44738E-02   0.00000E+00 
c  VelocityZ    0.29334E+04    1882   0.44738E-02   0.00000E+00 
c  Pressure     0.40643E+00    7082   0.36399E-01   0.19022E+00 
c  k            0.21739E+04    1537   0.77235E-04   0.14716E+01 
c  omega        0.16198E+08     221   0.27792E-03   0.49585E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1169e-05                         44353


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7804          2.3394      -0.0010613      1.3128e-06
v  Velocity[Y]                 -17.931          31.481          6.8606          20.055
v  Velocity[Z]                 -28.583          28.887         0.11471        0.023884
v  ǁVelocityǁ                0.0090469          33.661          10.675          20.211
v  Pressure                    -407.12          352.04          -49.28          34.143
v  k                        7.8389e-09           56.38          3.9557          1.7598
v  omega                         1e-24      1.1609e+08          9762.7          11.989
v  turbulent_viscosity      2.9718e-15          1.4571        0.015168         0.13364
v  CourantNb                  0.031971          2842.7          45.653          1.3789
v  FourierNb                  0.010571           14553          87.637         0.78999
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010831        0.045699


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96672           14607          133.29          2.1688


 TIME FOR THE TIME STEP              213:        0.46076E+02

===============================================================


 INSTANT    0.214000000E+02   TIME STEP NUMBER             214
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.215324229E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           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+02 0.13315E+02
   Friction velocity        uet   :  0.45223E-03 0.28859E+01
   Friction velocity        uk    :  0.91256E-02 0.32087E+01
   Dimensionless distance   yplus :  0.75298E-01 0.27202E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        561
   Nb of faces within the viscous sub-layer     :       1080
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29332E+04    1888   0.44685E-02   0.38279E+00 
c  VelocityY    0.29332E+04    1888   0.44685E-02   0.00000E+00 
c  VelocityZ    0.29332E+04    1888   0.44685E-02   0.00000E+00 
c  Pressure     0.41402E+00    7012   0.36311E-01   0.19440E+00 
c  k            0.21415E+04    1493   0.82772E-04   0.15031E+01 
c  omega        0.65940E+08     205   0.30153E-04   0.14676E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.3581e-05                             2
a  omega               -2.0162e+05                             1
a  Local Time Step      1.0145e-05                         44320


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0239          1.9386      8.9103e-05      3.8992e-07
v  Velocity[Y]                 -16.783          32.481          6.8832          20.056
v  Velocity[Z]                 -29.971          29.467        0.072781         0.02422
v  ǁVelocityǁ                 0.013964          33.656          10.642          20.212
v  Pressure                    -404.27          353.28         -49.415          34.396
v  k                         1.847e-08           61.51           3.978          1.7385
v  omega                         1e-24      5.8535e+07          9014.5          11.937
v  turbulent_viscosity      5.0329e-15          1.4461        0.015158         0.13125
v  CourantNb                 0.0062005          2304.2          45.309          1.3786
v  FourierNb                  0.010571           14828           89.26            0.78
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14832        0.010832        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           14884          134.57          2.1585


 TIME FOR THE TIME STEP              214:        0.46396E+02

===============================================================


 INSTANT    0.215000000E+02   TIME STEP NUMBER             215
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.714104469E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34127E+02 0.15359E+02
   Friction velocity        uet   :  0.13985E-02 0.28511E+01
   Friction velocity        uk    :  0.26781E-01 0.31708E+01
   Dimensionless distance   yplus :  0.12081E+00 0.31647E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29330E+04    1834   0.42818E-02   0.38361E+00 
c  VelocityY    0.29330E+04    1834   0.42818E-02   0.00000E+00 
c  VelocityZ    0.29330E+04    1834   0.42818E-02   0.00000E+00 
c  Pressure     0.43101E+00    6718   0.33150E-01   0.20310E+00 
c  k            0.21097E+04    1327   0.86765E-04   0.15031E+01 
c  omega        0.23645E+08     330   0.44666E-04   0.66279E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00030922                             4
a  omega          
a  Local Time Step      1.1058e-05                         44265


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2825          1.4214       0.0015027      4.8694e-07
v  Velocity[Y]                  -15.06          31.926          6.8907          20.056
v  Velocity[Z]                 -29.052          28.996        0.035754        0.023706
v  ǁVelocityǁ                 0.015181          33.561          10.611          20.212
v  Pressure                     -404.9          347.25         -50.338          33.748
v  k                        6.9852e-09          91.264          3.9555          1.7184
v  omega                         1e-24      3.0289e+07          8656.1          11.914
v  turbulent_viscosity      1.5973e-14          1.4328        0.015142         0.12896
v  CourantNb                  0.042949          2313.7          45.048          1.3783
v  FourierNb                  0.010576           15036          90.257         0.77066
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14793        0.010833        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78995           15098          135.31           2.149


 TIME FOR THE TIME STEP              215:        0.44266E+02

===============================================================


 INSTANT    0.216000000E+02   TIME STEP NUMBER             216
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.267576418E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29945E+02 0.14358E+02
   Friction velocity        uet   :  0.84616E-03 0.26795E+01
   Friction velocity        uk    :  0.29529E-01 0.29773E+01
   Dimensionless distance   yplus :  0.96961E-01 0.39582E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        461
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29329E+04    1880   0.44182E-02   0.37994E+00 
c  VelocityY    0.29329E+04    1880   0.44182E-02   0.00000E+00 
c  VelocityZ    0.29329E+04    1880   0.44182E-02   0.00000E+00 
c  Pressure     0.40404E+00    6950   0.31978E-01   0.19072E+00 
c  k            0.20782E+04     977   0.79116E-04   0.14086E+01 
c  omega        0.13728E+08     308   0.37779E-04   0.22785E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0005536                             2
a  omega          
a  Local Time Step       1.086e-05                         44232


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5158          1.4618       0.0027354      -1.314e-06
v  Velocity[Y]                 -16.476          32.205          6.8663          20.057
v  Velocity[Z]                 -28.635          29.011      -0.0017462        0.022868
v  ǁVelocityǁ                 0.013389          32.976          10.611          20.212
v  Pressure                    -403.35          345.35         -51.099          33.206
v  k                        7.1024e-09            84.5          3.9197          1.6996
v  omega                         1e-24      1.7147e+07          8407.7           11.92
v  turbulent_viscosity       1.745e-15          1.4158        0.015086         0.12678
v  CourantNb                  0.054242          2317.9          44.897          1.3783
v  FourierNb                  0.010581           15142          90.049         0.76092
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010833        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15211          134.95          2.1392


 TIME FOR THE TIME STEP              216:        0.45407E+02

===============================================================


 INSTANT    0.217000000E+02   TIME STEP NUMBER             217
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.421417420E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30635E+02 0.19653E+02
   Friction velocity        uet   :  0.10934E-02 0.25986E+01
   Friction velocity        uk    :  0.94104E-02 0.33683E+01
   Dimensionless distance   yplus :  0.11628E+00 0.33877E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29328E+04    1924   0.44371E-02   0.38165E+00 
c  VelocityY    0.29328E+04    1924   0.44371E-02   0.00000E+00 
c  VelocityZ    0.29328E+04    1924   0.44371E-02   0.00000E+00 
c  Pressure     0.41917E+00    6936   0.28115E-01   0.19767E+00 
c  k            0.20491E+04    1206   0.79966E-04   0.14609E+01 
c  omega        0.11087E+08     204   0.41983E-04   0.25005E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00012698                             2
a  omega          
a  Local Time Step      1.0528e-05                         44242


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7625          1.8135       0.0033768     -8.6699e-08
v  Velocity[Y]                 -16.418          30.419          6.8645          20.057
v  Velocity[Z]                 -28.801          29.001       -0.016233        0.021571
v  ǁVelocityǁ                 0.010365          33.628          10.631          20.212
v  Pressure                    -397.99          345.07         -50.695           33.16
v  k                         2.937e-09          44.939          3.8781           1.682
v  omega                         1e-24      1.7534e+07          8408.4          11.888
v  turbulent_viscosity      6.6568e-14          1.3963        0.015012          0.1247
v  CourantNb                  0.031716          2316.9          44.842          1.3785
v  FourierNb                  0.010587           15269          89.441         0.75114
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14919        0.010833        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15348          134.28          2.1296


 TIME FOR THE TIME STEP              217:        0.46371E+02

===============================================================


 INSTANT    0.218000000E+02   TIME STEP NUMBER             218
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.314928835E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30790E+02 0.19522E+02
   Friction velocity        uet   :  0.13114E-02 0.27349E+01
   Friction velocity        uk    :  0.27064E-01 0.30935E+01
   Dimensionless distance   yplus :  0.13535E+00 0.32713E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        472
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29328E+04    1918   0.42471E-02   0.36748E+00 
c  VelocityY    0.29328E+04    1918   0.42471E-02   0.00000E+00 
c  VelocityZ    0.29328E+04    1918   0.42471E-02   0.00000E+00 
c  Pressure     0.42015E+00    6968   0.28343E-01   0.19837E+00 
c  k            0.20241E+04    1311   0.84100E-04   0.15985E+01 
c  omega        0.11048E+08     213   0.77989E-04   0.61133E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -2.2561e-06                             1
a  omega               -1.2087e+05                             1
a  Local Time Step      1.0536e-05                         44287


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8974          2.1172       0.0036537      1.3869e-06
v  Velocity[Y]                 -14.982          31.162          6.8996          20.056
v  Velocity[Z]                 -31.181          28.936       -0.028059        0.019697
v  ǁVelocityǁ                 0.011856          36.516          10.662          20.211
v  Pressure                    -391.16          346.57          -49.02          33.522
v  k                        1.5227e-09          57.644          3.8639          1.6658
v  omega                         1e-24      3.4783e+07          8491.7          11.877
v  turbulent_viscosity       7.178e-15          1.3749        0.014962         0.12273
v  CourantNb                  0.030173          2325.1           45.08          1.3786
v  FourierNb                  0.010589           15329          88.409         0.74222
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010832        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15411          133.49          2.1208


 TIME FOR THE TIME STEP              218:        0.45516E+02

===============================================================


 INSTANT    0.219000000E+02   TIME STEP NUMBER             219
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.192061412E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32947E+02 0.16852E+02
   Friction velocity        uet   :  0.99370E-03 0.31200E+01
   Friction velocity        uk    :  0.23118E-01 0.32428E+01
   Dimensionless distance   yplus :  0.12794E+00 0.26035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29327E+04    1868   0.43859E-02   0.35520E+00 
c  VelocityY    0.29327E+04    1868   0.43859E-02   0.00000E+00 
c  VelocityZ    0.29327E+04    1868   0.43859E-02   0.00000E+00 
c  Pressure     0.39108E+00    7015   0.33634E-01   0.18343E+00 
c  k            0.20069E+04    1362   0.93875E-04   0.17529E+01 
c  omega        0.12932E+08     214   0.69090E-04   0.39615E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.1538e-05                             2
a  omega          
a  Local Time Step      1.1495e-05                         44244


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9191           2.418       0.0038411      4.9676e-06
v  Velocity[Y]                 -15.092          32.781          6.9618          20.055
v  Velocity[Z]                  -32.39          28.996      -0.0070359        0.017791
v  ǁVelocityǁ                 0.021521          35.651          10.727          20.211
v  Pressure                     -396.4          347.76         -47.482          33.857
v  k                        1.9072e-09           69.45          3.8512          1.6509
v  omega                         1e-24      3.4553e+07          8344.4          11.862
v  turbulent_viscosity      8.6314e-15          1.3519         0.01493         0.12087
v  CourantNb                   0.04072            2345          45.132          1.3785
v  FourierNb                  0.010591           15343          87.809         0.73382
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010832        0.045788


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0032           15423          132.94          2.1123


 TIME FOR THE TIME STEP              219:        0.45315E+02

===============================================================


 INSTANT    0.220000000E+02   TIME STEP NUMBER             220
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.308360425E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31584E+02 0.14141E+02
   Friction velocity        uet   :  0.22616E-02 0.32056E+01
   Friction velocity        uk    :  0.22770E-01 0.29761E+01
   Dimensionless distance   yplus :  0.12790E+00 0.25900E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29329E+04    1856   0.44200E-02   0.35800E+00 
c  VelocityY    0.29329E+04    1856   0.44200E-02   0.00000E+00 
c  VelocityZ    0.29329E+04    1856   0.44200E-02   0.00000E+00 
c  Pressure     0.42169E+00    7118   0.39135E-01   0.19693E+00 
c  k            0.19995E+04    1371   0.96340E-04   0.18137E+01 
c  omega        0.12138E+08     242   0.10719E-03   0.51280E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1271e-05                         44116


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8096          2.6313       0.0034868      4.1588e-06
v  Velocity[Y]                 -15.531          30.727          7.0306          20.056
v  Velocity[Z]                 -32.206          28.948        0.049661         0.01585
v  ǁVelocityǁ                0.0028866          34.389          10.788          20.211
v  Pressure                    -419.47          348.62         -46.162          34.162
v  k                         4.556e-08          72.538          3.8279          1.6373
v  omega                         1e-24      4.0974e+07          8258.2          11.848
v  turbulent_viscosity      1.5185e-14          1.3264        0.014893         0.11912
v  CourantNb                  0.015436          2823.7          45.246          1.3785
v  FourierNb                  0.010597           15294          87.232         0.72582
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010832        0.045797


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90077           15369          132.48          2.1043


 TIME FOR THE TIME STEP              220:        0.46170E+02

===============================================================


 INSTANT    0.221000000E+02   TIME STEP NUMBER             221
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.347581293E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31673E+02 0.13960E+02
   Friction velocity        uet   :  0.14070E-02 0.30935E+01
   Friction velocity        uk    :  0.23549E-01 0.29700E+01
   Dimensionless distance   yplus :  0.68379E-01 0.25725E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29332E+04    1862   0.43336E-02   0.34722E+00 
c  VelocityY    0.29332E+04    1862   0.43336E-02   0.00000E+00 
c  VelocityZ    0.29332E+04    1862   0.43336E-02   0.00000E+00 
c  Pressure     0.42287E+00    7104   0.40225E-01   0.19856E+00 
c  k            0.19992E+04    1296   0.96481E-04   0.18474E+01 
c  omega        0.13568E+08     160   0.53515E-04   0.30376E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1234e-05                         44113


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.612          2.5737       0.0023217      3.3523e-06
v  Velocity[Y]                 -21.901          30.135          7.0607          20.056
v  Velocity[Z]                 -32.647          29.011          0.1222        0.013609
v  ǁVelocityǁ                  0.01729          33.917          10.791          20.212
v  Pressure                    -421.26          349.49         -45.278          34.274
v  k                        5.7243e-07          63.411          3.7925          1.6249
v  omega                         1e-24      2.1824e+07          8058.4          11.836
v  turbulent_viscosity      3.2727e-13          1.3001        0.014846         0.11748
v  CourantNb                  0.051564          2751.5          45.451          1.3785
v  FourierNb                    0.0106           15187          86.745          0.7185
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010832        0.045773


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82206           15255           132.2           2.097


 TIME FOR THE TIME STEP              221:        0.45224E+02

===============================================================


 INSTANT    0.222000000E+02   TIME STEP NUMBER             222
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.268664326E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31718E+02 0.13617E+02
   Friction velocity        uet   :  0.91515E-03 0.28894E+01
   Friction velocity        uk    :  0.20594E-01 0.32261E+01
   Dimensionless distance   yplus :  0.11660E+00 0.25826E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        372
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29333E+04    1760   0.42201E-02   0.31406E+00 
c  VelocityY    0.29333E+04    1760   0.42201E-02   0.00000E+00 
c  VelocityZ    0.29333E+04    1760   0.42201E-02   0.00000E+00 
c  Pressure     0.38941E+00    6986   0.35821E-01   0.18310E+00 
c  k            0.20008E+04     965   0.91873E-04   0.18548E+01 
c  omega        0.11899E+08     176   0.10795E-03   0.14380E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -7.713e-05                             2
a  omega               -1.7734e+05                             1
a  Local Time Step      1.0898e-05                         44173


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3663          2.5449       0.0013897      2.4998e-06
v  Velocity[Y]                 -26.519          29.975          7.0223          20.055
v  Velocity[Z]                 -32.009          28.891         0.17918        0.011375
v  ǁVelocityǁ                0.0087095          32.609          10.743          20.212
v  Pressure                       -408          350.67         -44.598          34.292
v  k                        1.5147e-08          52.384          3.7743          1.6135
v  omega                         1e-24       4.714e+07            8694          11.896
v  turbulent_viscosity      7.0522e-14          1.2732        0.014778         0.11595
v  CourantNb                  0.024586          2358.1          45.665          1.3787
v  FourierNb                    0.0106           15053          85.835         0.71154
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14866        0.010832        0.045787


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15109           131.5          2.0902


 TIME FOR THE TIME STEP              222:        0.42989E+02

===============================================================


 INSTANT    0.223000000E+02   TIME STEP NUMBER             223
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.499526431E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31415E+02 0.18687E+02
   Friction velocity        uet   :  0.26794E-02 0.27611E+01
   Friction velocity        uk    :  0.16046E-01 0.32562E+01
   Dimensionless distance   yplus :  0.59297E-01 0.25915E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        361
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29334E+04    1745   0.45522E-02   0.28981E+00 
c  VelocityY    0.29334E+04    1745   0.45522E-02   0.00000E+00 
c  VelocityZ    0.29334E+04    1745   0.45522E-02   0.00000E+00 
c  Pressure     0.41819E+00    7073   0.31823E-01   0.19702E+00 
c  k            0.19988E+04    1205   0.10717E-03   0.17401E+01 
c  omega        0.26069E+08     179   0.25329E-04   0.65197E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.5804e-05                             3
a  omega                   -5752.4                             3
a  Local Time Step       1.146e-05                         44146


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0024          2.3621       0.0007617      4.4389e-07
v  Velocity[Y]                 -34.348          29.854          6.9268          20.055
v  Velocity[Z]                 -29.529          28.571         0.20294       0.0091197
v  ǁVelocityǁ                0.0062605          34.923          10.723          20.212
v  Pressure                    -390.93          351.54         -44.536          34.426
v  k                        4.4851e-08          83.239          3.8293          1.6033
v  omega                         1e-24      2.3574e+07          8436.8            11.9
v  turbulent_viscosity      6.8879e-14           1.246        0.014735         0.11453
v  CourantNb                  0.018304          2322.1          45.615          1.3786
v  FourierNb                    0.0106           14986          86.177         0.70526
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010832        0.045786


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0094           15039          131.79          2.0839


 TIME FOR THE TIME STEP              223:        0.43144E+02

===============================================================


 INSTANT    0.224000000E+02   TIME STEP NUMBER             224
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.217963812E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29526E+02 0.24240E+02
   Friction velocity        uet   :  0.64335E-03 0.30044E+01
   Friction velocity        uk    :  0.15363E-01 0.33660E+01
   Dimensionless distance   yplus :  0.85336E-01 0.32640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :       1112
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29334E+04    1899   0.46468E-02   0.28081E+00 
c  VelocityY    0.29334E+04    1899   0.46468E-02   0.00000E+00 
c  VelocityZ    0.29334E+04    1899   0.46468E-02   0.00000E+00 
c  Pressure     0.41809E+00    6998   0.34536E-01   0.19675E+00 
c  k            0.19910E+04    1407   0.13152E-03   0.15466E+01 
c  omega        0.13102E+08     398   0.13749E-03   0.15339E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.4266e-06                             1
a  omega          
a  Local Time Step      1.1292e-05                         44213


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4855          2.4209      3.3928e-05     -2.5848e-07
v  Velocity[Y]                 -38.629          30.144          6.8701          20.055
v  Velocity[Z]                 -28.661          28.603         0.22195       0.0070782
v  ǁVelocityǁ                0.0028134          39.044          10.709          20.212
v  Pressure                    -396.01          351.46         -45.537          34.398
v  k                        9.1375e-09          92.716          3.9107          1.5943
v  omega                         1e-24      8.6289e+07          8845.1          11.952
v  turbulent_viscosity      1.1733e-14          1.2251        0.014716         0.11322
v  CourantNb                  0.030757          2281.9          45.646          1.3786
v  FourierNb                  0.010601           14973          87.647         0.69988
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14834        0.010833        0.045801


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15024          133.29          2.0784


 TIME FOR THE TIME STEP              224:        0.46286E+02

===============================================================


 INSTANT    0.225000000E+02   TIME STEP NUMBER             225
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.256355254E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.47215E+02 0.13971E+02
   Friction velocity        uet   :  0.46614E-02 0.34986E+01
   Friction velocity        uk    :  0.15671E-01 0.52383E+01
   Dimensionless distance   yplus :  0.12996E+00 0.42884E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :       1128
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29335E+04    1938   0.44061E-02   0.28198E+00 
c  VelocityY    0.29335E+04    1938   0.44061E-02   0.00000E+00 
c  VelocityZ    0.29335E+04    1938   0.44061E-02   0.00000E+00 
c  Pressure     0.40223E+00    7117   0.39639E-01   0.18968E+00 
c  k            0.19825E+04    1469   0.11438E-03   0.14137E+01 
c  omega        0.31518E+08     286   0.39888E-04   0.13658E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00036596                             2
a  omega          
a  Local Time Step      1.0545e-05                         44281


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1043            2.48     -0.00066365     -2.9545e-07
v  Velocity[Y]                 -27.512          30.558          6.8638          20.056
v  Velocity[Z]                 -28.694          28.279         0.22296       0.0051931
v  ǁVelocityǁ                0.0050315          33.461          10.693          20.213
v  Pressure                    -399.59          350.84         -47.353          34.427
v  k                        8.2871e-09          42.844          3.9253          1.5866
v  omega                         1e-24      4.3838e+07          9019.6          11.983
v  turbulent_viscosity      7.9782e-15          1.2377        0.014721         0.11201
v  CourantNb                  0.026261          2707.5          45.763          1.3786
v  FourierNb                  0.010603           14983          88.145         0.69455
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14845        0.010832        0.045799


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8693           15037          133.91          2.0732


 TIME FOR THE TIME STEP              225:        0.46414E+02

===============================================================


 INSTANT    0.226000000E+02   TIME STEP NUMBER             226
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.106540863E-19
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30732E+02 0.13960E+02
   Friction velocity        uet   :  0.23162E-02 0.28138E+01
   Friction velocity        uk    :  0.74343E-02 0.33358E+01
   Dimensionless distance   yplus :  0.62998E-01 0.26894E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :       1098
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29335E+04    1991   0.46073E-02   0.28950E+00 
c  VelocityY    0.29335E+04    1991   0.46073E-02   0.00000E+00 
c  VelocityZ    0.29335E+04    1991   0.46073E-02   0.00000E+00 
c  Pressure     0.42124E+00    7120   0.38922E-01   0.19768E+00 
c  k            0.19767E+04    1458   0.76451E-04   0.12654E+01 
c  omega        0.16749E+08     256   0.17561E-03   0.23544E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.053e-05                         44383


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2135          2.5105     -0.00094878     -3.7607e-07
v  Velocity[Y]                 -17.435          31.031          6.8654          20.056
v  Velocity[Z]                 -28.661          28.548         0.19466       0.0035237
v  ǁVelocityǁ                0.0031675          33.789          10.664          20.214
v  Pressure                    -409.85          350.11         -48.799          34.441
v  k                        7.3337e-11          45.227          3.9638            1.58
v  omega                         1e-24      6.8087e+07          9256.4          11.953
v  turbulent_viscosity      4.3929e-15          1.2491        0.014747         0.11091
v  CourantNb                  0.041626          2936.6          45.759          1.3786
v  FourierNb                  0.010604           15140          88.113           0.689
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14859        0.010829        0.045786


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15199          133.87          2.0676


 TIME FOR THE TIME STEP              226:        0.47654E+02

===============================================================


 INSTANT    0.227000000E+02   TIME STEP NUMBER             227
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.377849776E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30133E+02 0.13790E+02
   Friction velocity        uet   :  0.10761E-02 0.27658E+01
   Friction velocity        uk    :  0.13389E-01 0.32578E+01
   Dimensionless distance   yplus :  0.15913E+00 0.27635E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        524
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    2083   0.43758E-02   0.31188E+00 
c  VelocityY    0.29336E+04    2083   0.43758E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    2083   0.43758E-02   0.00000E+00 
c  Pressure     0.40707E+00    7031   0.35788E-01   0.19139E+00 
c  k            0.19738E+04    1380   0.74615E-04   0.12190E+01 
c  omega        0.29858E+08     161   0.60267E-04   0.15443E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2509e+05                             1
a  Local Time Step      1.1116e-05                         44454


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4915          2.5531      -0.0005526      -5.946e-07
v  Velocity[Y]                 -17.168          31.562          6.8675          20.056
v  Velocity[Z]                  -28.71          28.421         0.14302       0.0020659
v  ǁVelocityǁ                 0.018884           34.04          10.636          20.214
v  Pressure                    -418.96          355.68         -49.611          34.315
v  k                        3.1684e-07           48.17          4.0214          1.5744
v  omega                         1e-24      6.4147e+07          8780.1          11.915
v  turbulent_viscosity      5.9818e-17          1.2589        0.014792         0.10992
v  CourantNb                 0.0054352          2225.2          45.309          1.3785
v  FourierNb                  0.010602           15336          89.268         0.68395
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14757        0.010827         0.04577


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15400          134.58          2.0624


 TIME FOR THE TIME STEP              227:        0.47496E+02

===============================================================


 INSTANT    0.228000000E+02   TIME STEP NUMBER             228
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.208845568E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30341E+02 0.14787E+02
   Friction velocity        uet   :  0.94992E-03 0.27954E+01
   Friction velocity        uk    :  0.11890E-01 0.29676E+01
   Dimensionless distance   yplus :  0.11764E+00 0.32254E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    2096   0.46079E-02   0.33666E+00 
c  VelocityY    0.29336E+04    2096   0.46079E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    2096   0.46079E-02   0.00000E+00 
c  Pressure     0.41759E+00    7041   0.34146E-01   0.19611E+00 
c  k            0.19720E+04    1245   0.77074E-04   0.13079E+01 
c  omega        0.27989E+08     265   0.31914E-04   0.48412E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.068e-05                         44517


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6738          2.5292      0.00062805      1.4362e-06
v  Velocity[Y]                 -15.728           31.94          6.8715          20.056
v  Velocity[Z]                 -28.813          28.551        0.078958      0.00056647
v  ǁVelocityǁ                0.0070283          33.796          10.616          20.214
v  Pressure                    -421.28          349.75          -50.95           33.85
v  k                         3.098e-08           51.56           4.029          1.5698
v  omega                         1e-24      3.2201e+07          8427.6          11.879
v  turbulent_viscosity      1.9213e-14          1.2663        0.014845         0.10902
v  CourantNb                  0.040702          2215.8          44.725          1.3783
v  FourierNb                  0.010598           15555          92.509         0.67988
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14857        0.010825        0.045769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15621          137.23          2.0582


 TIME FOR THE TIME STEP              228:        0.47627E+02

===============================================================


 INSTANT    0.229000000E+02   TIME STEP NUMBER             229
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.336333622E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31239E+02 0.13551E+02
   Friction velocity        uet   :  0.84303E-03 0.26747E+01
   Friction velocity        uk    :  0.10976E-01 0.32654E+01
   Dimensionless distance   yplus :  0.13298E+00 0.36514E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        449
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    2067   0.45057E-02   0.36234E+00 
c  VelocityY    0.29336E+04    2067   0.45057E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    2067   0.45057E-02   0.00000E+00 
c  Pressure     0.43912E+00    6931   0.33140E-01   0.20696E+00 
c  k            0.19703E+04    1194   0.78157E-04   0.12699E+01 
c  omega        0.12426E+08     298   0.48329E-04   0.20486E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6825e+05                             1
a  Local Time Step      1.1524e-05                         44549


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7532          2.5071       0.0021838      3.1764e-06
v  Velocity[Y]                 -17.298          31.655          6.8409          20.056
v  Velocity[Z]                 -28.653          28.824        0.013592     -0.00054206
v  ǁVelocityǁ                0.0043623          33.318          10.614          20.215
v  Pressure                    -413.58           344.8         -52.071          33.346
v  k                        6.8658e-07          40.483           4.012          1.5663
v  omega                         1e-24      1.6398e+07          8382.9          11.858
v  turbulent_viscosity      2.1814e-15          1.2702        0.014864         0.10822
v  CourantNb                   0.04848          2199.8          44.512          1.3786
v  FourierNb                  0.010596           15684          93.233          0.6754
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14794        0.010823         0.04577


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15753          137.74           2.054


 TIME FOR THE TIME STEP              229:        0.47087E+02

===============================================================


 INSTANT    0.230000000E+02   TIME STEP NUMBER             230
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.511211929E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30758E+02 0.22673E+02
   Friction velocity        uet   :  0.93410E-03 0.25640E+01
   Friction velocity        uk    :  0.23195E-01 0.31873E+01
   Dimensionless distance   yplus :  0.11741E+00 0.37332E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    2041   0.44480E-02   0.37655E+00 
c  VelocityY    0.29336E+04    2041   0.44480E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    2041   0.44480E-02   0.00000E+00 
c  Pressure     0.42771E+00    6955   0.32025E-01   0.20157E+00 
c  k            0.19693E+04    1130   0.77240E-04   0.13160E+01 
c  omega        0.14492E+08     248   0.24919E-04   0.12952E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00020415                             1
a  omega          
a  Local Time Step      1.0548e-05                         44498


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1478          2.7301       0.0042639      3.7154e-06
v  Velocity[Y]                 -15.195          30.962          6.8128          20.057
v  Velocity[Z]                 -28.923          28.674       -0.032142      -0.0014915
v  ǁVelocityǁ                0.0037262           32.66          10.608          20.216
v  Pressure                    -399.96          343.87         -52.456          32.897
v  k                        4.4354e-08          43.534          3.9797          1.5638
v  omega                         1e-24      1.3343e+07          8305.5          11.848
v  turbulent_viscosity      1.2361e-13           1.276        0.014863         0.10751
v  CourantNb                  0.034588          2180.9          44.449          1.3789
v  FourierNb                  0.010589           15756          92.298         0.67059
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14818        0.010821        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15827          136.75          2.0495


 TIME FOR THE TIME STEP              230:        0.46795E+02

===============================================================


 INSTANT    0.231000000E+02   TIME STEP NUMBER             231
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.111049460E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30948E+02 0.20676E+02
   Friction velocity        uet   :  0.10798E-02 0.25986E+01
   Friction velocity        uk    :  0.20088E-01 0.31030E+01
   Dimensionless distance   yplus :  0.87480E-01 0.28934E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29336E+04    2002   0.45298E-02   0.39404E+00 
c  VelocityY    0.29336E+04    2002   0.45298E-02   0.00000E+00 
c  VelocityZ    0.29336E+04    2002   0.45298E-02   0.00000E+00 
c  Pressure     0.42531E+00    6985   0.29104E-01   0.20005E+00 
c  k            0.19700E+04    1085   0.81451E-04   0.14555E+01 
c  omega        0.11818E+08     221   0.32172E-04   0.21687E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039403                             2
a  omega          
a  Local Time Step      1.1597e-05                         44487


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0554          2.8953       0.0060654      3.7216e-06
v  Velocity[Y]                 -14.415          30.449          6.8234          20.056
v  Velocity[Z]                 -30.877          28.874       -0.067923      -0.0023919
v  ǁVelocityǁ                0.0047993          35.864          10.612          20.215
v  Pressure                    -385.65           345.5         -51.003          32.856
v  k                        6.2339e-08          54.391          3.9561          1.5622
v  omega                         1e-24      1.7019e+07            8204          11.848
v  turbulent_viscosity      1.4463e-14           1.279        0.014852         0.10689
v  CourantNb                  0.011954          2167.1          44.548          1.3792
v  FourierNb                  0.010585           15819          91.129         0.66605
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14809         0.01082        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15892          135.68          2.0452


 TIME FOR THE TIME STEP              231:        0.44802E+02

===============================================================


 INSTANT    0.232000000E+02   TIME STEP NUMBER             232
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.667209838E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31832E+02 0.18472E+02
   Friction velocity        uet   :  0.12859E-02 0.30257E+01
   Friction velocity        uk    :  0.11199E-01 0.30684E+01
   Dimensionless distance   yplus :  0.12165E+00 0.26446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29337E+04    1960   0.44651E-02   0.39943E+00 
c  VelocityY    0.29337E+04    1960   0.44651E-02   0.00000E+00 
c  VelocityZ    0.29337E+04    1960   0.44651E-02   0.00000E+00 
c  Pressure     0.42005E+00    7037   0.31505E-01   0.19695E+00 
c  k            0.19748E+04    1302   0.90084E-04   0.16202E+01 
c  omega        0.62249E+09      82   0.73819E-06   0.35610E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047314                             2
a  omega          
a  Local Time Step       1.078e-05                         44515


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4383          2.9056       0.0074175      1.7157e-06
v  Velocity[Y]                 -15.077          31.987          6.8619          20.056
v  Velocity[Z]                 -31.529           28.76       -0.096106      -0.0029216
v  ǁVelocityǁ                0.0052109          36.508          10.639          20.215
v  Pressure                    -398.25          347.85         -49.374          33.165
v  k                        2.7761e-07          64.121           3.933          1.5616
v  omega                         1e-24      1.8572e+07          8284.1          11.855
v  turbulent_viscosity      1.5578e-14           1.278        0.014857         0.10635
v  CourantNb                  0.047837          2164.5          44.549          1.3792
v  FourierNb                  0.010588           15925          90.506         0.66228
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14782        0.010819        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0106           15999          135.06          2.0414


 TIME FOR THE TIME STEP              232:        0.47437E+02

===============================================================


 INSTANT    0.233000000E+02   TIME STEP NUMBER             233
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.146600856E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31734E+02 0.17357E+02
   Friction velocity        uet   :  0.21218E-02 0.30914E+01
   Friction velocity        uk    :  0.22533E-01 0.33595E+01
   Dimensionless distance   yplus :  0.21512E+00 0.26251E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29339E+04    1917   0.45287E-02   0.42325E+00 
c  VelocityY    0.29339E+04    1917   0.45287E-02   0.00000E+00 
c  VelocityZ    0.29339E+04    1917   0.45287E-02   0.00000E+00 
c  Pressure     0.43478E+00    7109   0.38016E-01   0.20441E+00 
c  k            0.19857E+04    1336   0.94873E-04   0.17377E+01 
c  omega        0.11102E+08     241   0.94688E-04   0.52118E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00035868                             3
a  omega          
a  Local Time Step      1.0735e-05                         44537


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1666          2.7358       0.0079733      5.5998e-06
v  Velocity[Y]                 -15.103          32.625          6.9215          20.056
v  Velocity[Z]                 -33.145          28.814       -0.089752      -0.0028194
v  ǁVelocityǁ                  0.01629           34.55          10.682          20.216
v  Pressure                    -431.85          349.98         -47.791           33.46
v  k                        8.4764e-07          68.682          3.9013          1.5617
v  omega                         1e-24      3.8509e+07          8183.3          11.848
v  turbulent_viscosity      2.0688e-13          1.2809        0.014844         0.10589
v  CourantNb                  0.019052          2456.1          44.534           1.379
v  FourierNb                  0.010591           16040          89.319         0.65862
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14913        0.010818        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93257           16113          133.85          2.0376


 TIME FOR THE TIME STEP              233:        0.44852E+02

===============================================================


 INSTANT    0.234000000E+02   TIME STEP NUMBER             234
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.494207263E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31127E+02 0.16570E+02
   Friction velocity        uet   :  0.56983E-03 0.31726E+01
   Friction velocity        uk    :  0.26689E-01 0.29510E+01
   Dimensionless distance   yplus :  0.19907E+00 0.26346E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29341E+04    1889   0.45293E-02   0.44042E+00 
c  VelocityY    0.29341E+04    1889   0.45293E-02   0.00000E+00 
c  VelocityZ    0.29341E+04    1889   0.45293E-02   0.00000E+00 
c  Pressure     0.41879E+00    7113   0.40667E-01   0.19630E+00 
c  k            0.20014E+04    1197   0.93012E-04   0.17972E+01 
c  omega        0.13919E+08     186   0.13080E-03   0.96994E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00016947                             2
a  omega          
a  Local Time Step      1.0836e-05                         44505


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3893           2.389       0.0075108      7.3264e-06
v  Velocity[Y]                 -20.372           30.37          6.9693          20.056
v  Velocity[Z]                 -33.246          28.833       -0.049631      -0.0025839
v  ǁVelocityǁ                 0.014792          34.622          10.696          20.216
v  Pressure                    -445.14          351.17         -46.962          33.455
v  k                        5.3031e-07          64.409          3.8654          1.5624
v  omega                         1e-24      6.5052e+07          8291.7          11.883
v  turbulent_viscosity      1.4296e-13          1.2813         0.01483         0.10551
v  CourantNb                  0.033459          2729.5          44.769          1.3789
v  FourierNb                  0.010595           16134          87.879         0.65572
v  total_pressure           1.0088e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14937        0.010817        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16199          132.65          2.0346


 TIME FOR THE TIME STEP              234:        0.45698E+02

===============================================================


 INSTANT    0.235000000E+02   TIME STEP NUMBER             235
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.468080101E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32505E+02 0.15180E+02
   Friction velocity        uet   :  0.25417E-03 0.29496E+01
   Friction velocity        uk    :  0.23243E-01 0.32169E+01
   Dimensionless distance   yplus :  0.16112E+00 0.26603E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :        990
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29343E+04    1954   0.46020E-02   0.42700E+00 
c  VelocityY    0.29343E+04    1954   0.46020E-02   0.00000E+00 
c  VelocityZ    0.29343E+04    1954   0.46020E-02   0.00000E+00 
c  Pressure     0.41572E+00    6827   0.37306E-01   0.19513E+00 
c  k            0.20168E+04    1197   0.92256E-04   0.18308E+01 
c  omega        0.20956E+08     143   0.62412E-04   0.10094E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7251e+05                             1
a  Local Time Step      1.1073e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3087          1.8875        0.006233      6.5439e-06
v  Velocity[Y]                 -23.561          30.282          6.9575          20.056
v  Velocity[Z]                 -33.557          28.601       -0.011115       -0.002248
v  ǁVelocityǁ                 0.017388          34.286          10.673          20.216
v  Pressure                    -438.89          352.11         -46.548          33.292
v  k                        1.1172e-07          51.442          3.8402          1.5635
v  omega                         1e-24      3.3366e+07          8754.8          11.927
v  turbulent_viscosity      7.6759e-14          1.2783        0.014804         0.10521
v  CourantNb                   0.05046          2444.7          44.975          1.3789
v  FourierNb                  0.010599           16136          87.155         0.65313
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010816        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88229           16200          132.13           2.032


 TIME FOR THE TIME STEP              235:        0.44927E+02

===============================================================


 INSTANT    0.236000000E+02   TIME STEP NUMBER             236
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.649949225E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30682E+02 0.13816E+02
   Friction velocity        uet   :  0.24749E-02 0.29097E+01
   Friction velocity        uk    :  0.20976E-01 0.28274E+01
   Dimensionless distance   yplus :  0.11443E+00 0.27119E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29346E+04    2046   0.45938E-02   0.40559E+00 
c  VelocityY    0.29346E+04    2046   0.45938E-02   0.00000E+00 
c  VelocityZ    0.29346E+04    2046   0.45938E-02   0.00000E+00 
c  Pressure     0.43027E+00    7031   0.33382E-01   0.20206E+00 
c  k            0.20281E+04    1259   0.96585E-04   0.17907E+01 
c  omega        0.12994E+08     205   0.53847E-04   0.64277E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.5224e-05                             1
a  omega          
a  Local Time Step      1.1051e-05                         44522


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5691          1.5992       0.0047087      4.5118e-06
v  Velocity[Y]                 -35.064          30.216          6.8769          20.056
v  Velocity[Z]                 -30.172          28.395       0.0010451       -0.001276
v  ǁVelocityǁ                 0.011273          35.173          10.663          20.216
v  Pressure                    -417.58          352.58         -46.348          33.095
v  k                        1.0314e-07          76.683          3.8713          1.5649
v  omega                         1e-24        1.83e+07          8444.2          11.928
v  turbulent_viscosity      1.6167e-14          1.2747        0.014794         0.10496
v  CourantNb                  0.038816          2205.8          45.007          1.3787
v  FourierNb                  0.010602           16127          87.272         0.65164
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14911        0.010816          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16190          132.28          2.0303


 TIME FOR THE TIME STEP              236:        0.46978E+02

===============================================================


 INSTANT    0.237000000E+02   TIME STEP NUMBER             237
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.525964430E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.34378E+02 0.24282E+02
   Friction velocity        uet   :  0.77479E-03 0.31192E+01
   Friction velocity        uk    :  0.19230E-01 0.29012E+01
   Dimensionless distance   yplus :  0.12931E+00 0.27056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :       1072
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29348E+04    2127   0.46362E-02   0.40184E+00 
c  VelocityY    0.29348E+04    2127   0.46362E-02   0.00000E+00 
c  VelocityZ    0.29348E+04    2127   0.46362E-02   0.00000E+00 
c  Pressure     0.44810E+00    7012   0.35167E-01   0.21195E+00 
c  k            0.20314E+04    1236   0.12408E-03   0.16455E+01 
c  omega        0.11595E+08     374   0.49688E-04   0.47161E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.6486e-05                             1
a  omega          
a  Local Time Step      1.0955e-05                         44537


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.789          1.9173       0.0028246      1.8321e-06
v  Velocity[Y]                 -34.604          30.374          6.7914          20.056
v  Velocity[Z]                 -29.552           28.34       0.0018434     -0.00041431
v  ǁVelocityǁ                0.0054908          40.569          10.691          20.216
v  Pressure                    -416.62          352.09         -47.119          33.108
v  k                        9.6587e-09          106.75          3.9665          1.5666
v  omega                         1e-24      1.7377e+07          8416.3          11.943
v  turbulent_viscosity       2.572e-14          1.2696        0.014799         0.10478
v  CourantNb                  0.040327            2184          45.029          1.3785
v  FourierNb                  0.010606           16080          88.634         0.65131
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14817        0.010815        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0098           16150          133.66          2.0298


 TIME FOR THE TIME STEP              237:        0.47463E+02

===============================================================


 INSTANT    0.238000000E+02   TIME STEP NUMBER             238
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.124772354E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57658E+02 0.16584E+02
   Friction velocity        uet   :  0.11237E-02 0.35051E+01
   Friction velocity        uk    :  0.91623E-02 0.41921E+01
   Dimensionless distance   yplus :  0.77641E-01 0.36143E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29350E+04    2141   0.45529E-02   0.40610E+00 
c  VelocityY    0.29350E+04    2141   0.45529E-02   0.00000E+00 
c  VelocityZ    0.29350E+04    2141   0.45529E-02   0.00000E+00 
c  Pressure     0.45121E+00    7103   0.39042E-01   0.21415E+00 
c  k            0.20280E+04    1235   0.14370E-03   0.14877E+01 
c  omega        0.10567E+08     499   0.28111E-03   0.25667E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0837e-05                         44559


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0428          2.2872      0.00098301      2.9544e-06
v  Velocity[Y]                 -31.876          30.897           6.773          20.056
v  Velocity[Z]                 -29.106          28.358       0.0027876      0.00052621
v  ǁVelocityǁ                0.0096154          33.667          10.701          20.217
v  Pressure                    -419.03          350.54         -49.169          33.287
v  k                        4.4673e-09           85.21          4.0443          1.5688
v  omega                         1e-24      6.2645e+07          9231.1          11.995
v  turbulent_viscosity      5.0535e-14          1.2647        0.014818         0.10466
v  CourantNb                  0.065458          2157.1          45.181          1.3785
v  FourierNb                  0.010611           16053          89.507         0.65132
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010815        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16123          134.69          2.0298


 TIME FOR THE TIME STEP              238:        0.47900E+02

===============================================================


 INSTANT    0.239000000E+02   TIME STEP NUMBER             239
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.300442173E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30089E+02 0.14916E+02
   Friction velocity        uet   :  0.21368E-02 0.30897E+01
   Friction velocity        uk    :  0.12300E-01 0.34688E+01
   Dimensionless distance   yplus :  0.10990E+00 0.33892E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :       1033
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29351E+04    2102   0.44197E-02   0.41101E+00 
c  VelocityY    0.29351E+04    2102   0.44197E-02   0.00000E+00 
c  VelocityZ    0.29351E+04    2102   0.44197E-02   0.00000E+00 
c  Pressure     0.42807E+00    7108   0.40047E-01   0.20209E+00 
c  k            0.20234E+04    1332   0.11248E-03   0.14084E+01 
c  omega        0.29759E+08     265   0.97484E-04   0.23708E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8689e+05                             1
a  Local Time Step      1.0107e-05                         44562


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1739          2.5709     -0.00096794      6.0701e-06
v  Velocity[Y]                 -17.751          31.406          6.7828          20.056
v  Velocity[Z]                 -28.643          28.183      -0.0049955       0.0015718
v  ǁVelocityǁ                 0.007931          34.209          10.689          20.217
v  Pressure                    -420.64          348.81         -51.586          33.223
v  k                        7.9956e-09          46.162          4.0903           1.571
v  omega                         1e-24      7.5252e+07          9288.1          11.993
v  turbulent_viscosity      4.1304e-15          1.2612        0.014869         0.10459
v  CourantNb                   0.01916          3055.9          45.392          1.3785
v  FourierNb                  0.010616           16093          89.601         0.65165
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14836        0.010815        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16166          134.99          2.0302


 TIME FOR THE TIME STEP              239:        0.47931E+02

===============================================================


 INSTANT    0.240000000E+02   TIME STEP NUMBER             240
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.593929411E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29775E+02 0.13031E+02
   Friction velocity        uet   :  0.37954E-02 0.28100E+01
   Friction velocity        uk    :  0.19237E-01 0.34492E+01
   Dimensionless distance   yplus :  0.14534E+00 0.27000E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        541
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    2091   0.46415E-02   0.42461E+00 
c  VelocityY    0.29353E+04    2091   0.46415E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    2091   0.46415E-02   0.00000E+00 
c  Pressure     0.40213E+00    7120   0.35092E-01   0.18907E+00 
c  k            0.20197E+04    1478   0.79152E-04   0.12617E+01 
c  omega        0.33719E+08     215   0.85724E-04   0.23536E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -33433                             2
a  Local Time Step      1.0942e-05                         44537


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1881          2.7665        -0.00263      6.6072e-06
v  Velocity[Y]                 -17.684          32.379           6.799          20.056
v  Velocity[Z]                 -29.856          28.293       -0.028983       0.0025382
v  ǁVelocityǁ                 0.010639          34.393          10.652          20.217
v  Pressure                    -435.21           347.5         -53.271          33.138
v  k                        1.6167e-10          50.524          4.1588          1.5734
v  omega                         1e-24      7.2826e+07            9138           11.95
v  turbulent_viscosity      1.4048e-14          1.2589        0.014929         0.10456
v  CourantNb                  0.024282          2265.2          45.202          1.3785
v  FourierNb                  0.010619           16145          91.428         0.65263
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14822        0.010814        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16219          136.63          2.0312


 TIME FOR THE TIME STEP              240:        0.50018E+02

===============================================================


 INSTANT    0.241000000E+02   TIME STEP NUMBER             241
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.485892509E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33540E+02 0.13325E+02
   Friction velocity        uet   :  0.22901E-02 0.29239E+01
   Friction velocity        uk    :  0.15704E-01 0.28563E+01
   Dimensionless distance   yplus :  0.10200E+00 0.28453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29354E+04    2112   0.46503E-02   0.43879E+00 
c  VelocityY    0.29354E+04    2112   0.46503E-02   0.00000E+00 
c  VelocityZ    0.29354E+04    2112   0.46503E-02   0.00000E+00 
c  Pressure     0.42593E+00    7006   0.32206E-01   0.20079E+00 
c  k            0.20166E+04    1552   0.79568E-04   0.13034E+01 
c  omega        0.32470E+08     328   0.42657E-04   0.63534E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0009e+05                             2
a  Local Time Step      1.1039e-05                         44494


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0914           3.002      -0.0034174      5.5242e-06
v  Velocity[Y]                 -16.158          33.153          6.8091          20.057
v  Velocity[Z]                 -28.549          28.475         -0.0549       0.0040315
v  ǁVelocityǁ                 0.013918          34.039          10.627          20.218
v  Pressure                    -439.41          346.14         -54.853          32.897
v  k                         4.287e-10          54.438          4.1699          1.5757
v  omega                         1e-24      3.7098e+07          8461.1          11.871
v  turbulent_viscosity      5.1922e-16          1.2539        0.015007         0.10457
v  CourantNb                  0.068998          2126.5          44.749          1.3785
v  FourierNb                  0.010623           16051          94.864          0.6543
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14818        0.010812        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           16126          139.61          2.0328


 TIME FOR THE TIME STEP              241:        0.47682E+02

===============================================================


 INSTANT    0.242000000E+02   TIME STEP NUMBER             242
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.155137600E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30729E+02 0.15237E+02
   Friction velocity        uet   :  0.13300E-02 0.28495E+01
   Friction velocity        uk    :  0.19962E-01 0.29153E+01
   Dimensionless distance   yplus :  0.17261E+00 0.32722E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :        949
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29354E+04    2104   0.43497E-02   0.45544E+00 
c  VelocityY    0.29354E+04    2104   0.43497E-02   0.00000E+00 
c  VelocityZ    0.29354E+04    2104   0.43497E-02   0.00000E+00 
c  Pressure     0.43069E+00    7014   0.32736E-01   0.20208E+00 
c  k            0.20120E+04    1544   0.76769E-04   0.12580E+01 
c  omega        0.13533E+08     352   0.48934E-04   0.26033E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9796e+05                             3
a  Local Time Step      1.1147e-05                         44420


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9283          3.1853       -0.003866      2.9635e-06
v  Velocity[Y]                 -15.037           32.69          6.7787          20.057
v  Velocity[Z]                 -28.485          28.796        -0.09054       0.0050774
v  ǁVelocityǁ                0.0076111          33.725          10.628          20.218
v  Pressure                    -427.46          344.75         -56.418          32.146
v  k                        1.2571e-07          40.537          4.1368           1.578
v  omega                         1e-24      1.9923e+07          8272.7          11.848
v  turbulent_viscosity      4.5133e-16          1.2458        0.015045         0.10462
v  CourantNb                  0.050465            2112          44.389          1.3786
v  FourierNb                  0.010627           15879          96.415         0.65538
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010811        0.045732


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15954           140.8           2.034


 TIME FOR THE TIME STEP              242:        0.48757E+02

===============================================================


 INSTANT    0.243000000E+02   TIME STEP NUMBER             243
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.331613862E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31276E+02 0.23430E+02
   Friction velocity        uet   :  0.15049E-02 0.26878E+01
   Friction velocity        uk    :  0.29007E-01 0.30553E+01
   Dimensionless distance   yplus :  0.74064E-01 0.37908E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :        913
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    2041   0.43433E-02   0.46118E+00 
c  VelocityY    0.29353E+04    2041   0.43433E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    2041   0.43433E-02   0.00000E+00 
c  Pressure     0.41681E+00    6982   0.32531E-01   0.19702E+00 
c  k            0.20069E+04    1457   0.72606E-04   0.12392E+01 
c  omega        0.10685E+08     295   0.32915E-04   0.11386E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66440                             2
a  Local Time Step      1.0916e-05                         44382


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7698          3.3395      -0.0034973     -1.1459e-06
v  Velocity[Y]                 -14.463          31.767           6.741          20.056
v  Velocity[Z]                 -28.403          29.115        -0.10159       0.0061775
v  ǁVelocityǁ                   0.0111          33.385          10.628          20.217
v  Pressure                    -404.13          344.59         -57.215          31.659
v  k                        1.4658e-07          40.082          4.1109          1.5802
v  omega                         1e-24      1.2544e+07          8102.6           11.83
v  turbulent_viscosity      2.0419e-14          1.2371        0.015056         0.10469
v  CourantNb                  0.045556          2082.3          44.281           1.379
v  FourierNb                  0.010632           15646          95.724         0.65563
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010811        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15719             140          2.0346


 TIME FOR THE TIME STEP              243:        0.47475E+02

===============================================================


 INSTANT    0.244000000E+02   TIME STEP NUMBER             244
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.389930294E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31754E+02 0.22004E+02
   Friction velocity        uet   :  0.20381E-02 0.26030E+01
   Friction velocity        uk    :  0.26856E-01 0.32371E+01
   Dimensionless distance   yplus :  0.14161E+00 0.28692E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        462
   Nb of faces within the viscous sub-layer     :        897
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29352E+04    1961   0.43480E-02   0.46459E+00 
c  VelocityY    0.29352E+04    1961   0.43480E-02   0.00000E+00 
c  VelocityZ    0.29352E+04    1961   0.43480E-02   0.00000E+00 
c  Pressure     0.40620E+00    7006   0.31274E-01   0.19119E+00 
c  k            0.20022E+04    1211   0.77702E-04   0.13536E+01 
c  omega        0.10258E+08     304   0.28699E-04   0.12310E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7899e+05                             2
a  Local Time Step      1.0911e-05                         44353


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5194          3.2649      -0.0026911     -5.2334e-06
v  Velocity[Y]                 -15.106          30.702          6.7354          20.056
v  Velocity[Z]                 -31.309          29.057        -0.10113       0.0071774
v  ǁVelocityǁ                 0.010495          37.154           10.63          20.217
v  Pressure                    -377.33          346.76         -56.006          31.972
v  k                        1.3694e-06          49.941          4.0761          1.5824
v  omega                         1e-24      1.4172e+07          8015.1          11.821
v  turbulent_viscosity       1.378e-14          1.2281        0.015067         0.10478
v  CourantNb                    0.0604          2057.1          44.481          1.3794
v  FourierNb                  0.010636           15421          95.898         0.65617
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14825        0.010812        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15492          140.38          2.0356


 TIME FOR THE TIME STEP              244:        0.46057E+02

===============================================================


 INSTANT    0.245000000E+02   TIME STEP NUMBER             245
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.266721543E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31517E+02 0.20024E+02
   Friction velocity        uet   :  0.24077E-02 0.31205E+01
   Friction velocity        uk    :  0.25348E-01 0.32253E+01
   Dimensionless distance   yplus :  0.16696E+00 0.26653E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :        940
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29352E+04    1995   0.44738E-02   0.45699E+00 
c  VelocityY    0.29352E+04    1995   0.44738E-02   0.00000E+00 
c  VelocityZ    0.29352E+04    1995   0.44738E-02   0.00000E+00 
c  Pressure     0.44168E+00    7088   0.32855E-01   0.20788E+00 
c  k            0.20000E+04    1131   0.82616E-04   0.15110E+01 
c  omega        0.10330E+08     216   0.54344E-04   0.29048E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9464e+05                             3
a  Local Time Step      1.1564e-05                         44388


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0394          3.2974      -0.0018278     -2.6481e-06
v  Velocity[Y]                 -15.106          30.833          6.7614          20.057
v  Velocity[Z]                 -32.712          29.146       -0.092668       0.0080978
v  ǁVelocityǁ                 0.012555          36.934          10.648          20.218
v  Pressure                    -401.26          349.15         -54.345          32.287
v  k                        4.0013e-07          61.058          4.0376          1.5846
v  omega                         1e-24      1.8083e+07          8182.7          11.834
v  turbulent_viscosity      1.5545e-13          1.2192        0.015078         0.10488
v  CourantNb                  0.063704          2046.3           44.56          1.3795
v  FourierNb                  0.010639           15316          95.769         0.65663
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14846        0.010812        0.045706


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15385          140.33          2.0362


 TIME FOR THE TIME STEP              245:        0.45819E+02

===============================================================


 INSTANT    0.246000000E+02   TIME STEP NUMBER             246
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.316112067E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30738E+02 0.13757E+02
   Friction velocity        uet   :  0.80755E-03 0.31728E+01
   Friction velocity        uk    :  0.24105E-01 0.32912E+01
   Dimensionless distance   yplus :  0.15045E+00 0.26660E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        372
   Nb of faces within the viscous sub-layer     :        937
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    2007   0.43682E-02   0.45543E+00 
c  VelocityY    0.29353E+04    2007   0.43682E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    2007   0.43682E-02   0.00000E+00 
c  Pressure     0.43576E+00    7116   0.37581E-01   0.20478E+00 
c  k            0.20034E+04    1074   0.88302E-04   0.16428E+01 
c  omega        0.13996E+08     233   0.32431E-04   0.18674E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -46233                             2
a  Local Time Step      1.1561e-05                         44447


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3506          2.7377      -0.0011955     -5.8096e-06
v  Velocity[Y]                  -14.96          31.153          6.8092          20.057
v  Velocity[Z]                 -32.843          29.076       -0.056069       0.0091755
v  ǁVelocityǁ                 0.011621          35.471          10.679          20.218
v  Pressure                    -442.46          350.94         -52.247          32.701
v  k                        9.2866e-08          70.968          3.9981          1.5865
v  omega                         1e-24      1.5214e+07          8037.7          11.845
v  turbulent_viscosity      7.5539e-14          1.2101        0.015072         0.10499
v  CourantNb                  0.086921          2305.8          44.615          1.3795
v  FourierNb                  0.010642           15236           94.66         0.65664
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14924        0.010812          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15303          139.28          2.0361


 TIME FOR THE TIME STEP              246:        0.45596E+02

===============================================================


 INSTANT    0.247000000E+02   TIME STEP NUMBER             247
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.242914491E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29815E+02 0.14226E+02
   Friction velocity        uet   :  0.54079E-03 0.30643E+01
   Friction velocity        uk    :  0.25667E-01 0.29667E+01
   Dimensionless distance   yplus :  0.17272E+00 0.26729E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        371
   Nb of faces within the viscous sub-layer     :        925
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    1937   0.44641E-02   0.46004E+00 
c  VelocityY    0.29353E+04    1937   0.44641E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    1937   0.44641E-02   0.00000E+00 
c  Pressure     0.44810E+00    7126   0.40753E-01   0.21176E+00 
c  k            0.20125E+04    1039   0.88576E-04   0.17044E+01 
c  omega        0.11064E+08     319   0.18812E-03   0.11968E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.5907e-05                             1
a  omega               -1.7593e+05                             7
a  Local Time Step      1.1612e-05                         44489


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95152          2.7282     -0.00081086     -5.2668e-06
v  Velocity[Y]                 -19.264          30.632          6.8575          20.056
v  Velocity[Z]                 -33.682          28.984       0.0098297        0.010099
v  ǁVelocityǁ                 0.014072          35.493          10.688          20.217
v  Pressure                    -457.58          351.27         -50.741          32.773
v  k                        6.4806e-07           70.59          3.9528          1.5881
v  omega                         1e-24      5.9175e+07          8333.3          11.879
v  turbulent_viscosity      1.7026e-14          1.2013         0.01505         0.10511
v  CourantNb                  0.012735          2756.3          44.895          1.3794
v  FourierNb                  0.010645           15175          92.825          0.6565
v  total_pressure           1.0087e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14873        0.010813        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97404           15235          137.72          2.0359


 TIME FOR THE TIME STEP              247:        0.44960E+02

===============================================================


 INSTANT    0.248000000E+02   TIME STEP NUMBER             248
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.252171568E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31005E+02 0.14592E+02
   Friction velocity        uet   :  0.13634E-02 0.30429E+01
   Friction velocity        uk    :  0.17201E-01 0.31926E+01
   Dimensionless distance   yplus :  0.16157E+00 0.26679E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        363
   Nb of faces within the viscous sub-layer     :        940
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    1885   0.44031E-02   0.43934E+00 
c  VelocityY    0.29353E+04    1885   0.44031E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    1885   0.44031E-02   0.00000E+00 
c  Pressure     0.43459E+00    7101   0.37927E-01   0.20397E+00 
c  k            0.20232E+04    1169   0.87909E-04   0.17458E+01 
c  omega        0.21442E+08     168   0.14955E-03   0.26352E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.7346e-05                             1
a  omega               -2.6062e+05                             2
a  Local Time Step      1.0794e-05                         44508


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1938           2.849     -0.00065254      -5.225e-06
v  Velocity[Y]                  -23.91          30.426          6.8503          20.057
v  Velocity[Z]                 -33.819          28.786         0.07521        0.010888
v  ǁVelocityǁ                0.0088602          34.747          10.643          20.218
v  Pressure                    -451.98          350.65         -49.638          32.845
v  k                        6.2866e-08          88.168          3.9155          1.5893
v  omega                         1e-24      2.9607e+08          9189.1          11.978
v  turbulent_viscosity      7.2157e-14          1.1929        0.015028         0.10522
v  CourantNb                  0.035468          2504.8          45.081          1.3793
v  FourierNb                  0.010648           15054          92.145         0.65672
v  total_pressure           1.0087e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010814        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15120          137.23           2.036


 TIME FOR THE TIME STEP              248:        0.44167E+02

===============================================================


 INSTANT    0.249000000E+02   TIME STEP NUMBER             249
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.102963505E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30275E+02 0.17043E+02
   Friction velocity        uet   :  0.45414E-02 0.29429E+01
   Friction velocity        uk    :  0.23611E-01 0.30811E+01
   Dimensionless distance   yplus :  0.11877E+00 0.26653E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :        959
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    1864   0.43889E-02   0.40012E+00 
c  VelocityY    0.29353E+04    1864   0.43889E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    1864   0.43889E-02   0.00000E+00 
c  Pressure     0.42836E+00    7003   0.32713E-01   0.20170E+00 
c  k            0.20311E+04    1209   0.89376E-04   0.17271E+01 
c  omega        0.76397E+09      39   0.22883E-05   0.73701E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015585                             2
a  omega               -1.6629e+05                             5
a  Local Time Step      1.1552e-05                         44536


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6202          2.8826     -0.00078692     -6.2352e-06
v  Velocity[Y]                 -30.695           30.27           6.767          20.057
v  Velocity[Z]                  -30.97          28.725         0.12016        0.011022
v  ǁVelocityǁ                0.0077406          33.396           10.59          20.218
v  Pressure                    -431.34          349.33         -48.988           32.87
v  k                        2.2263e-09          109.08          3.9188            1.59
v  omega                         1e-24      1.4803e+08          9190.8          11.961
v  turbulent_viscosity      6.9956e-15          1.1843        0.015015         0.10533
v  CourantNb                  0.036783          2013.1          45.037          1.3792
v  FourierNb                   0.01065           14970          91.719         0.65711
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1482        0.010815        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15041          136.76          2.0363


 TIME FOR THE TIME STEP              249:        0.44474E+02

===============================================================


 INSTANT    0.250000000E+02   TIME STEP NUMBER             250
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.593301289E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29660E+02 0.21318E+02
   Friction velocity        uet   :  0.20330E-02 0.27592E+01
   Friction velocity        uk    :  0.20567E-01 0.30890E+01
   Dimensionless distance   yplus :  0.12360E+00 0.26514E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        387
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        250, Physical time    0.25000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 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                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
   End writing the wall distance                        
 End writing


 Time for restart files:    0.17656E+01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29353E+04    1858   0.44727E-02   0.37052E+00 
c  VelocityY    0.29353E+04    1858   0.44727E-02   0.00000E+00 
c  VelocityZ    0.29353E+04    1858   0.44727E-02   0.00000E+00 
c  Pressure     0.42024E+00    7003   0.32693E-01   0.19792E+00 
c  k            0.20320E+04    1239   0.10901E-03   0.16091E+01 
c  omega        0.19119E+09     103   0.46514E-05   0.21314E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66948                             3
a  Local Time Step      1.1136e-05                         44522


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9922          2.8588      -0.0010336     -3.8366e-06
v  Velocity[Y]                 -22.676          30.202          6.6658          20.055
v  Velocity[Z]                 -29.711           28.47         0.13344        0.011471
v  ǁVelocityǁ                0.0045343          33.607          10.582          20.217
v  Pressure                    -415.51          346.52         -49.255          32.709
v  k                        2.5583e-09          111.25          3.9944          1.5904
v  omega                         1e-24      7.3988e+07          8621.9          11.903
v  turbulent_viscosity      1.5192e-15          1.1781        0.015017         0.10543
v  CourantNb                   0.05716          1977.9          44.853          1.3789
v  FourierNb                  0.010652           14928           91.59         0.65792
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14714        0.010817        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91676           15004          136.44          2.0369


 TIME FOR THE TIME STEP              250:        0.46040E+02

===============================================================


 INSTANT    0.251000000E+02   TIME STEP NUMBER             251
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.284477537E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39821E+02 0.16755E+02
   Friction velocity        uet   :  0.14580E-02 0.26903E+01
   Friction velocity        uk    :  0.17771E-01 0.38995E+01
   Dimensionless distance   yplus :  0.14478E+00 0.35612E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29354E+04    1867   0.45013E-02   0.36127E+00 
c  VelocityY    0.29354E+04    1867   0.45013E-02   0.00000E+00 
c  VelocityZ    0.29354E+04    1867   0.45013E-02   0.00000E+00 
c  Pressure     0.45251E+00    7105   0.36471E-01   0.21268E+00 
c  k            0.20259E+04    1245   0.12219E-03   0.14364E+01 
c  omega        0.48818E+08     310   0.21885E-04   0.16639E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -52581                             2
a  Local Time Step      1.1096e-05                         44543


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.229          2.9124      -0.0014295     -3.9689e-06
v  Velocity[Y]                 -36.503           30.72          6.6229          20.056
v  Velocity[Z]                 -28.563          28.306         0.14298        0.011421
v  ǁVelocityǁ                 0.012211          37.258          10.582          20.217
v  Pressure                    -417.92          343.42         -50.472          32.779
v  k                        3.6911e-08            86.8          4.0738          1.5905
v  omega                         1e-24      4.5188e+07          8704.5          11.933
v  turbulent_viscosity      3.4399e-15          1.1735        0.015032         0.10551
v  CourantNb                  0.028878          1998.8          44.855          1.3789
v  FourierNb                  0.010653           14861          91.698          0.6592
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14809        0.010818        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14938          136.55          2.0381


 TIME FOR THE TIME STEP              251:        0.44644E+02

===============================================================


 INSTANT    0.252000000E+02   TIME STEP NUMBER             252
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.460855406E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40096E+02 0.13834E+02
   Friction velocity        uet   :  0.20816E-02 0.34360E+01
   Friction velocity        uk    :  0.21120E-01 0.35936E+01
   Dimensionless distance   yplus :  0.11999E+00 0.39885E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1036
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29356E+04    1784   0.43900E-02   0.35108E+00 
c  VelocityY    0.29356E+04    1784   0.43900E-02   0.00000E+00 
c  VelocityZ    0.29356E+04    1784   0.43900E-02   0.00000E+00 
c  Pressure     0.42132E+00    7126   0.40222E-01   0.19951E+00 
c  k            0.20181E+04    1097   0.11609E-03   0.13508E+01 
c  omega        0.24694E+08     250   0.12422E-03   0.36369E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1023e+05                             2
a  Local Time Step      1.1049e-05                         44537


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2959          3.1714      -0.0019732     -2.0002e-06
v  Velocity[Y]                 -22.217          31.203          6.6117          20.056
v  Velocity[Z]                 -28.614           28.54         0.13271        0.010967
v  ǁVelocityǁ                0.0048925          34.125          10.569          20.217
v  Pressure                     -418.9          340.48         -52.073          32.924
v  k                        1.9426e-08          42.205          4.1108          1.5903
v  omega                         1e-24      6.8717e+07          9473.2          11.965
v  turbulent_viscosity       5.008e-14          1.1691        0.015077         0.10558
v  CourantNb                  0.016144          3150.5          45.081          1.3788
v  FourierNb                  0.010653           14801          91.607         0.66051
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14741         0.01082        0.045669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99194           14877          136.69          2.0393


 TIME FOR THE TIME STEP              252:        0.44502E+02

===============================================================


 INSTANT    0.253000000E+02   TIME STEP NUMBER             253
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.130658529E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30818E+02 0.13682E+02
   Friction velocity        uet   :  0.16841E-02 0.26997E+01
   Friction velocity        uk    :  0.14121E-01 0.30861E+01
   Dimensionless distance   yplus :  0.12508E+00 0.35360E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        511
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29358E+04    1658   0.44689E-02   0.35640E+00 
c  VelocityY    0.29358E+04    1658   0.44689E-02   0.00000E+00 
c  VelocityZ    0.29358E+04    1658   0.44689E-02   0.00000E+00 
c  Pressure     0.41985E+00    7141   0.39103E-01   0.19774E+00 
c  k            0.20118E+04    1009   0.77624E-04   0.11854E+01 
c  omega        0.39705E+08     196   0.39281E-04   0.17969E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3171e+05                             2
a  Local Time Step      1.0861e-05                         44503


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2413          3.3347      -0.0026221     -4.7696e-07
v  Velocity[Y]                 -17.371          31.756          6.6166          20.056
v  Velocity[Z]                 -28.567          28.554         0.10771        0.010192
v  ǁVelocityǁ                0.0055752          34.156          10.538          20.217
v  Pressure                     -417.4          344.28         -53.222          32.923
v  k                        2.2258e-09          43.327          4.1844          1.5897
v  omega                         1e-24      4.6024e+07          8934.5          11.925
v  turbulent_viscosity      1.1573e-14          1.1652        0.015151         0.10563
v  CourantNb                   0.06613          2783.6          44.801          1.3785
v  FourierNb                  0.010654           14780           92.45         0.66174
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14695         0.01082        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14855          137.25          2.0403


 TIME FOR THE TIME STEP              253:        0.43393E+02

===============================================================


 INSTANT    0.254000000E+02   TIME STEP NUMBER             254
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.825036230E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31351E+02 0.13436E+02
   Friction velocity        uet   :  0.92168E-03 0.28662E+01
   Friction velocity        uk    :  0.23533E-01 0.31987E+01
   Dimensionless distance   yplus :  0.14432E+00 0.27877E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29360E+04    1661   0.44873E-02   0.37918E+00 
c  VelocityY    0.29360E+04    1661   0.44873E-02   0.00000E+00 
c  VelocityZ    0.29360E+04    1661   0.44873E-02   0.00000E+00 
c  Pressure     0.43148E+00    7096   0.36096E-01   0.20250E+00 
c  k            0.20066E+04    1305   0.80371E-04   0.11575E+01 
c  omega        0.22435E+08     186   0.47549E-04   0.55807E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4023e+05                             3
a  Local Time Step      1.1403e-05                         44548


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5557          3.3299      -0.0030387     -1.8449e-07
v  Velocity[Y]                  -16.81           33.06            6.64          20.056
v  Velocity[Z]                 -28.775          28.867         0.07414         0.00944
v  ǁVelocityǁ                0.0081027          34.196          10.505          20.217
v  Pressure                     -412.4          349.66         -54.113          32.789
v  k                        1.3383e-08          54.517          4.2465          1.5887
v  omega                         1e-24      2.3188e+07          8537.4          11.905
v  turbulent_viscosity      5.0065e-15          1.1624        0.015257         0.10566
v  CourantNb                  0.046512          2077.7          44.265          1.3782
v  FourierNb                  0.010653           14814          94.853         0.66343
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14826        0.010818        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           14884          139.12          2.0417


 TIME FOR THE TIME STEP              254:        0.42973E+02

===============================================================


 INSTANT    0.255000000E+02   TIME STEP NUMBER             255
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.514525263E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31949E+02 0.14403E+02
   Friction velocity        uet   :  0.20728E-02 0.28522E+01
   Friction velocity        uk    :  0.24703E-01 0.27840E+01
   Dimensionless distance   yplus :  0.14708E+00 0.31233E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1004
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29362E+04    1727   0.45056E-02   0.39636E+00 
c  VelocityY    0.29362E+04    1727   0.45056E-02   0.00000E+00 
c  VelocityZ    0.29362E+04    1727   0.45056E-02   0.00000E+00 
c  Pressure     0.43742E+00    6773   0.33987E-01   0.20605E+00 
c  k            0.20018E+04    1465   0.78453E-04   0.12071E+01 
c  omega        0.17059E+08     327   0.30914E-04   0.32606E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9516e+05                             3
a  Local Time Step      1.1396e-05                         44574


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2903          3.1552      -0.0033452      1.2999e-06
v  Velocity[Y]                 -15.152          32.597          6.6624          20.056
v  Velocity[Z]                 -28.482          29.292        0.044884       0.0085054
v  ǁVelocityǁ                0.0070322          34.101          10.505          20.217
v  Pressure                    -397.43           342.7         -55.218          32.353
v  k                        6.6696e-08          47.671           4.242          1.5875
v  omega                         1e-24      1.2366e+07          8504.4          11.905
v  turbulent_viscosity      8.7828e-15          1.1734        0.015361         0.10568
v  CourantNb                  0.024608          2092.2          43.891          1.3781
v  FourierNb                  0.010651           14937           98.31         0.66544
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010818        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9697           14999           142.2          2.0435


 TIME FOR THE TIME STEP              255:        0.42816E+02

===============================================================


 INSTANT    0.256000000E+02   TIME STEP NUMBER             256
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.472166936E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30959E+02 0.20111E+02
   Friction velocity        uet   :  0.19803E-02 0.26927E+01
   Friction velocity        uk    :  0.30238E-01 0.30547E+01
   Dimensionless distance   yplus :  0.13652E+00 0.38394E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29364E+04    1718   0.46805E-02   0.40506E+00 
c  VelocityY    0.29364E+04    1718   0.46805E-02   0.00000E+00 
c  VelocityZ    0.29364E+04    1718   0.46805E-02   0.00000E+00 
c  Pressure     0.42296E+00    6980   0.31731E-01   0.19922E+00 
c  k            0.19976E+04    1569   0.78706E-04   0.11649E+01 
c  omega        0.12067E+08     325   0.30423E-04   0.12430E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4727e+05                             1
a  Local Time Step      1.1445e-05                         44573


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2086          2.7816      -0.0032335      1.4015e-06
v  Velocity[Y]                 -15.524          31.882          6.6536          20.056
v  Velocity[Z]                 -28.514          29.269        0.017253        0.007305
v  ǁVelocityǁ                0.0080295          33.434          10.506          20.217
v  Pressure                    -384.06          337.53         -55.212          32.048
v  k                        6.1039e-08          44.108          4.2158          1.5862
v  omega                         1e-24      1.1822e+07          8221.8          11.851
v  turbulent_viscosity      7.4332e-15          1.1846        0.015428         0.10568
v  CourantNb                  0.028241          2093.6          43.806          1.3783
v  FourierNb                   0.01065           15115           99.24         0.66626
v  total_pressure           1.0094e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14887        0.010817        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87058           15176          143.05          2.0445


 TIME FOR THE TIME STEP              256:        0.43674E+02

===============================================================


 INSTANT    0.257000000E+02   TIME STEP NUMBER             257
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.452626647E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30698E+02 0.20651E+02
   Friction velocity        uet   :  0.23509E-02 0.26097E+01
   Friction velocity        uk    :  0.23211E-01 0.31266E+01
   Dimensionless distance   yplus :  0.11849E+00 0.29460E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29367E+04    1801   0.46320E-02   0.40983E+00 
c  VelocityY    0.29367E+04    1801   0.46320E-02   0.00000E+00 
c  VelocityZ    0.29367E+04    1801   0.46320E-02   0.00000E+00 
c  Pressure     0.43485E+00    7008   0.30654E-01   0.20647E+00 
c  k            0.19951E+04    1657   0.81212E-04   0.12383E+01 
c  omega        0.10581E+08     297   0.29007E-04   0.11171E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -28033                             1
a  Local Time Step      1.0976e-05                         44544


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4133          2.2581       -0.001597     -1.1417e-06
v  Velocity[Y]                  -15.38          30.753           6.659          20.056
v  Velocity[Z]                 -29.869          29.317        0.012833         0.00598
v  ǁVelocityǁ                0.0051579          35.323          10.501          20.217
v  Pressure                    -368.71          339.28         -54.227          31.954
v  k                        3.3136e-08           44.64          4.1848          1.5849
v  omega                         1e-24      1.1905e+07          8186.2          11.838
v  turbulent_viscosity      1.5257e-14          1.1976         0.01547         0.10566
v  CourantNb                  0.044796            2088          43.771          1.3785
v  FourierNb                  0.010649           15354          99.266         0.66625
v  total_pressure           1.0096e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010818        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89677           15418          143.04          2.0447


 TIME FOR THE TIME STEP              257:        0.44743E+02

===============================================================


 INSTANT    0.258000000E+02   TIME STEP NUMBER             258
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.246283366E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31159E+02 0.19850E+02
   Friction velocity        uet   :  0.27875E-02 0.29194E+01
   Friction velocity        uk    :  0.18355E-01 0.32134E+01
   Dimensionless distance   yplus :  0.67614E-01 0.26297E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        411
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29369E+04    1876   0.45077E-02   0.43084E+00 
c  VelocityY    0.29369E+04    1876   0.45077E-02   0.00000E+00 
c  VelocityZ    0.29369E+04    1876   0.45077E-02   0.00000E+00 
c  Pressure     0.42263E+00    7024   0.29679E-01   0.19974E+00 
c  k            0.19961E+04    1697   0.84931E-04   0.13635E+01 
c  omega        0.29391E+16       2   0.10234E-11   0.14098E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62466                             2
a  Local Time Step      1.1491e-05                         44508


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6236          1.6103     -0.00022401     -3.4821e-06
v  Velocity[Y]                 -17.732          30.532          6.6819          20.056
v  Velocity[Z]                 -31.776          29.399        0.004996        0.004707
v  ǁVelocityǁ                0.0063179          37.291          10.502          20.217
v  Pressure                    -361.48          341.91         -51.824           32.07
v  k                        1.5752e-08          55.443          4.1613          1.5838
v  omega                         1e-24      1.1905e+07          8097.5          11.831
v  turbulent_viscosity      1.7554e-14          1.2113        0.015498         0.10563
v  CourantNb                  0.026135          2072.1          43.744          1.3784
v  FourierNb                  0.010648           15658          99.226         0.66612
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14792         0.01082        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80059           15725          142.97          2.0445


 TIME FOR THE TIME STEP              258:        0.45084E+02

===============================================================


 INSTANT    0.259000000E+02   TIME STEP NUMBER             259
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.238894012E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30508E+02 0.15972E+02
   Friction velocity        uet   :  0.30481E-02 0.31397E+01
   Friction velocity        uk    :  0.92859E-02 0.29523E+01
   Dimensionless distance   yplus :  0.12239E+00 0.26613E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        442
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    1881   0.45026E-02   0.44441E+00 
c  VelocityY    0.29372E+04    1881   0.45026E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    1881   0.45026E-02   0.00000E+00 
c  Pressure     0.42757E+00    7123   0.32440E-01   0.20089E+00 
c  k            0.20025E+04    1698   0.90689E-04   0.15452E+01 
c  omega        0.10184E+08     296   0.36217E-04   0.17539E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1512e+05                             3
a  Local Time Step      1.1415e-05                         44487


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7939          1.6249     -6.2848e-05     -6.7103e-06
v  Velocity[Y]                 -15.083          30.423          6.7256          20.056
v  Velocity[Z]                 -33.426          29.249      -0.0067648       0.0033039
v  ǁVelocityǁ                0.0043287          37.338          10.541          20.218
v  Pressure                    -420.01          344.21          -49.44          32.288
v  k                        2.9749e-08          62.487          4.1268          1.5827
v  omega                         1e-24      1.6115e+07          8075.6          11.856
v  turbulent_viscosity      6.8569e-14           1.215        0.015507         0.10556
v  CourantNb                  0.024529          2051.3          43.762          1.3781
v  FourierNb                  0.010646           16150          97.292         0.66523
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14746         0.01082        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16221          141.05          2.0434


 TIME FOR THE TIME STEP              259:        0.46111E+02

===============================================================


 INSTANT    0.260000000E+02   TIME STEP NUMBER             260
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.320079126E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30108E+02 0.15444E+02
   Friction velocity        uet   :  0.17011E-02 0.32081E+01
   Friction velocity        uk    :  0.13640E-01 0.30961E+01
   Dimensionless distance   yplus :  0.14481E+00 0.26781E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    1918   0.43687E-02   0.46169E+00 
c  VelocityY    0.29375E+04    1918   0.43687E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    1918   0.43687E-02   0.00000E+00 
c  Pressure     0.42534E+00    7138   0.37582E-01   0.20153E+00 
c  k            0.20166E+04    1452   0.88734E-04   0.15821E+01 
c  omega        0.10206E+08     236   0.22549E-03   0.15028E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7859e+05                             2
a  Local Time Step      1.1265e-05                         44484


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9803          1.9459       -0.001234     -7.5767e-06
v  Velocity[Y]                 -16.119          30.302          6.7823          20.056
v  Velocity[Z]                 -32.824          28.776        0.009704       0.0018615
v  ǁVelocityǁ                0.0087212          35.092          10.579          20.218
v  Pressure                    -444.54          345.33         -47.506          32.526
v  k                        4.5356e-07          65.359          4.0775          1.5819
v  omega                         1e-24       6.309e+07          8417.6           11.86
v  turbulent_viscosity      2.1138e-13          1.2331        0.015497         0.10551
v  CourantNb                  0.023441          2380.8          43.945          1.3779
v  FourierNb                  0.010645           16518          96.386         0.66437
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14772         0.01082         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94268           16590          140.33          2.0423


 TIME FOR THE TIME STEP              260:        0.47413E+02

===============================================================


 INSTANT    0.261000000E+02   TIME STEP NUMBER             261
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.523761466E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29870E+02 0.14737E+02
   Friction velocity        uet   :  0.72967E-03 0.29853E+01
   Friction velocity        uk    :  0.22586E-01 0.29373E+01
   Dimensionless distance   yplus :  0.16192E+00 0.26589E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    1990   0.44481E-02   0.47066E+00 
c  VelocityY    0.29377E+04    1990   0.44481E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    1990   0.44481E-02   0.00000E+00 
c  Pressure     0.42729E+00    7128   0.38812E-01   0.20079E+00 
c  k            0.20323E+04    1338   0.89219E-04   0.16125E+01 
c  omega        0.26254E+08     181   0.40902E-04   0.50633E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3774e+05                             2
a  Local Time Step      1.0737e-05                         44495


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1294          2.2086      -0.0030106     -9.1834e-06
v  Velocity[Y]                 -23.657          30.134          6.8131          20.056
v  Velocity[Z]                 -33.174          28.858        0.056163      6.0102e-05
v  ǁVelocityǁ                0.0062034          34.408          10.571          20.218
v  Pressure                    -447.99          344.82         -46.424          32.553
v  k                        1.3836e-09           58.85          4.0441          1.5811
v  omega                         1e-24      3.2372e+07          8200.4          11.848
v  turbulent_viscosity      1.7647e-13          1.2453        0.015504         0.10546
v  CourantNb                  0.044298          2583.7          44.211          1.3777
v  FourierNb                  0.010644           16736          95.306         0.66374
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14773         0.01082        0.045666


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16814          139.52          2.0414


 TIME FOR THE TIME STEP              261:        0.47760E+02

===============================================================


 INSTANT    0.262000000E+02   TIME STEP NUMBER             262
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.318640444E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29961E+02 0.13512E+02
   Friction velocity        uet   :  0.65078E-04 0.29054E+01
   Friction velocity        uk    :  0.27521E-01 0.31834E+01
   Dimensionless distance   yplus :  0.12197E+00 0.26475E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        394
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    2030   0.45121E-02   0.45012E+00 
c  VelocityY    0.29379E+04    2030   0.45121E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    2030   0.45121E-02   0.00000E+00 
c  Pressure     0.42667E+00    7085   0.36303E-01   0.20075E+00 
c  k            0.20447E+04    1554   0.91413E-04   0.16355E+01 
c  omega        0.12076E+08     292   0.19700E-03   0.20298E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1262e+05                             4
a  Local Time Step      1.1119e-05                         44516


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1701           2.419      -0.0046267     -5.6644e-06
v  Velocity[Y]                 -30.322          29.963          6.7716          20.056
v  Velocity[Z]                 -32.383          28.506        0.089954      -0.0013757
v  ǁVelocityǁ                 0.005665          33.324          10.529          20.218
v  Pressure                    -433.84          343.76         -45.648          32.626
v  k                        9.6576e-08          51.402          4.0422          1.5805
v  omega                         1e-24      2.2389e+08          8896.3          11.953
v  turbulent_viscosity      6.0435e-15          1.2554        0.015516         0.10541
v  CourantNb                  0.041647          2223.2          44.404          1.3776
v  FourierNb                  0.010643           16764          95.299         0.66367
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14855         0.01082        0.045653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16845           139.7          2.0412


 TIME FOR THE TIME STEP              262:        0.47628E+02

===============================================================


 INSTANT    0.263000000E+02   TIME STEP NUMBER             263
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.155512271E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30116E+02 0.21670E+02
   Friction velocity        uet   :  0.30671E-02 0.28584E+01
   Friction velocity        uk    :  0.29835E-01 0.29286E+01
   Dimensionless distance   yplus :  0.10445E+00 0.26302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1967   0.46253E-02   0.43534E+00 
c  VelocityY    0.29379E+04    1967   0.46253E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1967   0.46253E-02   0.00000E+00 
c  Pressure     0.43868E+00    7088   0.31834E-01   0.20689E+00 
c  k            0.20512E+04    1636   0.10468E-03   0.15958E+01 
c  omega        0.59281E+09      64   0.57734E-05   0.78489E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00047258                             1
a  omega               -1.9208e+05                             6
a  Local Time Step      1.0746e-05                         44529


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0691          2.6639      -0.0056486     -3.5996e-06
v  Velocity[Y]                 -31.116          29.864          6.6744          20.057
v  Velocity[Z]                 -29.734          28.438        0.096087      -0.0026764
v  ǁVelocityǁ                0.0058054          33.454           10.52          20.219
v  Pressure                    -409.77          341.83         -46.014          32.515
v  k                         1.213e-06          96.184          4.1113          1.5801
v  omega                         1e-24      1.1196e+08          9389.9          11.947
v  turbulent_viscosity       9.222e-14           1.268        0.015543         0.10535
v  CourantNb                  0.019973          2102.3          44.427          1.3774
v  FourierNb                  0.010644           16710          94.996         0.66406
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1477         0.01082        0.045669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16800          139.42          2.0414


 TIME FOR THE TIME STEP              263:        0.46469E+02

===============================================================


 INSTANT    0.264000000E+02   TIME STEP NUMBER             264
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.112528724E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30203E+02 0.21335E+02
   Friction velocity        uet   :  0.16146E-02 0.25999E+01
   Friction velocity        uk    :  0.20951E-01 0.33662E+01
   Dimensionless distance   yplus :  0.10886E+00 0.34881E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :       1075
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1876   0.45170E-02   0.43847E+00 
c  VelocityY    0.29379E+04    1876   0.45170E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1876   0.45170E-02   0.00000E+00 
c  Pressure     0.44624E+00    7070   0.33595E-01   0.21072E+00 
c  k            0.20506E+04    1641   0.14765E-03   0.14961E+01 
c  omega        0.15309E+09     180   0.14358E-04   0.30782E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0003865                             2
a  omega               -1.2558e+05                             3
a  Local Time Step      1.1309e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8738          2.9089      -0.0062755     -3.1104e-06
v  Velocity[Y]                 -41.106          30.392           6.616          20.057
v  Velocity[Z]                 -28.685          28.254        0.095128      -0.0041041
v  ǁVelocityǁ                0.0038297          41.434          10.526           20.22
v  Pressure                    -414.09          339.64         -47.789          32.342
v  k                        1.0573e-07          114.11          4.2141            1.58
v  omega                         1e-24      5.8994e+07          9208.8          11.954
v  turbulent_viscosity      3.0105e-13          1.2787        0.015588         0.10531
v  CourantNb                  0.047988          2100.5          44.411          1.3772
v  FourierNb                  0.010645           16402          94.792         0.66437
v  total_pressure           1.0091e+05      1.0166e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14712         0.01082         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84009           16492           139.2          2.0416


 TIME FOR THE TIME STEP              264:        0.45952E+02

===============================================================


 INSTANT    0.265000000E+02   TIME STEP NUMBER             265
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.234899442E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56360E+02 0.12481E+02
   Friction velocity        uet   :  0.28275E-02 0.36867E+01
   Friction velocity        uk    :  0.11363E-01 0.49463E+01
   Dimensionless distance   yplus :  0.10175E+00 0.42730E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :       1105
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1706   0.44494E-02   0.44006E+00 
c  VelocityY    0.29379E+04    1706   0.44494E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1706   0.44494E-02   0.00000E+00 
c  Pressure     0.42702E+00    7144   0.39117E-01   0.20192E+00 
c  k            0.20472E+04    1532   0.15399E-03   0.14078E+01 
c  omega        0.45094E+08     326   0.24840E-04   0.10474E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043173                             7
a  omega               -1.8371e+05                             7
a  Local Time Step      1.1095e-05                         44505


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.697          3.0826      -0.0067111     -3.0375e-06
v  Velocity[Y]                 -29.938           30.74          6.6134          20.056
v  Velocity[Z]                 -28.593          28.419        0.086898      -0.0050917
v  ǁVelocityǁ                0.0068106          33.786          10.534           20.22
v  Pressure                    -415.94          338.18         -50.496          32.261
v  k                        1.6206e-08          51.718           4.232          1.5803
v  omega                         1e-24      3.0516e+07          8874.4          11.951
v  turbulent_viscosity      6.4685e-14           1.286        0.015625         0.10527
v  CourantNb                 0.0036572          2547.4          44.445          1.3772
v  FourierNb                  0.010646           16109          94.828         0.66458
v  total_pressure           1.0091e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14758        0.010821        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16194          139.27          2.0418


 TIME FOR THE TIME STEP              265:        0.45236E+02

===============================================================


 INSTANT    0.266000000E+02   TIME STEP NUMBER             266
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.351521486E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31138E+02 0.12920E+02
   Friction velocity        uet   :  0.19656E-02 0.30641E+01
   Friction velocity        uk    :  0.21086E-01 0.30828E+01
   Dimensionless distance   yplus :  0.14652E+00 0.26042E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        533
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1640   0.45271E-02   0.44163E+00 
c  VelocityY    0.29379E+04    1640   0.45271E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1640   0.45271E-02   0.00000E+00 
c  Pressure     0.40817E+00    7170   0.40877E-01   0.19399E+00 
c  k            0.20452E+04    1252   0.80106E-04   0.12836E+01 
c  omega        0.16552E+08     267   0.17055E-03   0.27549E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00052444                             1
a  omega               -1.4563e+05                             2
a  Local Time Step      1.1311e-05                         44487


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5354          3.1171      -0.0068915     -9.5815e-07
v  Velocity[Y]                 -17.749          31.005          6.6352          20.057
v  Velocity[Z]                  -28.47          28.833        0.067368      -0.0059178
v  ǁVelocityǁ                 0.012163          33.614          10.533          20.221
v  Pressure                    -417.33          337.52          -53.27          32.226
v  k                        8.4537e-09          47.678          4.2724          1.5809
v  omega                         1e-24      6.3819e+07          9384.7          11.956
v  turbulent_viscosity      6.1875e-15          1.2908        0.015653         0.10523
v  CourantNb                  0.030507            3057          44.339          1.3771
v  FourierNb                  0.010648           15951          94.908          0.6646
v  total_pressure           1.0091e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485         0.01082        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16028          139.25          2.0417


 TIME FOR THE TIME STEP              266:        0.43378E+02

===============================================================


 INSTANT    0.267000000E+02   TIME STEP NUMBER             267
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.230367882E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31177E+02 0.13361E+02
   Friction velocity        uet   :  0.15414E-02 0.28347E+01
   Friction velocity        uk    :  0.17706E-01 0.28306E+01
   Dimensionless distance   yplus :  0.10996E+00 0.28137E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    1976   0.46578E-02   0.44817E+00 
c  VelocityY    0.29378E+04    1976   0.46578E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    1976   0.46578E-02   0.00000E+00 
c  Pressure     0.42056E+00    7123   0.35845E-01   0.19937E+00 
c  k            0.20454E+04    1243   0.78873E-04   0.12496E+01 
c  omega        0.30774E+08     271   0.40737E-04   0.21026E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0010893                             2
a  omega               -1.8927e+05                             2
a  Local Time Step      1.1147e-05                         44469


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1664          3.1382       -0.006274      1.7583e-06
v  Velocity[Y]                 -17.283          32.215          6.6773          20.057
v  Velocity[Z]                  -28.32           30.28        0.046421        -0.00672
v  ǁVelocityǁ                 0.013923          34.022          10.521          20.221
v  Pressure                    -415.61          343.24         -55.244          32.003
v  k                        5.9934e-08          52.919          4.3379          1.5819
v  omega                         1e-24      3.5995e+07          8881.1          11.955
v  turbulent_viscosity      1.9876e-15          1.2952        0.015696         0.10521
v  CourantNb                  0.035494          2115.8          43.974          1.3771
v  FourierNb                  0.010651           15851          96.965           0.665
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010817        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15921          140.94          2.0421


 TIME FOR THE TIME STEP              267:        0.46771E+02

===============================================================


 INSTANT    0.268000000E+02   TIME STEP NUMBER             268
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.313508367E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31307E+02 0.15472E+02
   Friction velocity        uet   :  0.53045E-03 0.28674E+01
   Friction velocity        uk    :  0.28363E-01 0.28039E+01
   Dimensionless distance   yplus :  0.96472E-01 0.31153E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1906   0.45549E-02   0.45924E+00 
c  VelocityY    0.29376E+04    1906   0.45549E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1906   0.45549E-02   0.00000E+00 
c  Pressure     0.44532E+00    6808   0.31394E-01   0.21174E+00 
c  k            0.20465E+04    1488   0.81144E-04   0.13620E+01 
c  omega        0.33179E+08     359   0.21195E-04   0.95229E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -4.4861e-05                             1
a  omega                    -48016                             1
a  Local Time Step       1.122e-05                         44452


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5858          3.1859      -0.0046228      2.8223e-06
v  Velocity[Y]                 -15.392          33.269          6.7213          20.056
v  Velocity[Z]                 -28.245          28.948        0.032239      -0.0072662
v  ǁVelocityǁ                 0.014094           33.94          10.511           20.22
v  Pressure                    -406.75          339.03         -57.012          31.543
v  k                        6.1783e-08          54.483          4.3327          1.5833
v  omega                         1e-24      3.2539e+07          8474.3          11.903
v  turbulent_viscosity      2.2146e-14          1.3001        0.015744          0.1052
v  CourantNb                  0.036283          2041.4          43.653          1.3772
v  FourierNb                  0.010655           15802           100.7         0.66583
v  total_pressure           1.0092e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010817        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15866          144.35           2.043


 TIME FOR THE TIME STEP              268:        0.45360E+02

===============================================================


 INSTANT    0.269000000E+02   TIME STEP NUMBER             269
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.105483015E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29444E+02 0.13650E+02
   Friction velocity        uet   :  0.17228E-02 0.28088E+01
   Friction velocity        uk    :  0.24058E-01 0.29829E+01
   Dimensionless distance   yplus :  0.16531E+00 0.36125E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        449
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    1911   0.46052E-02   0.45537E+00 
c  VelocityY    0.29375E+04    1911   0.46052E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    1911   0.46052E-02   0.00000E+00 
c  Pressure     0.41239E+00    6811   0.30421E-01   0.19529E+00 
c  k            0.20471E+04    1554   0.79806E-04   0.13419E+01 
c  omega        0.18036E+08     327   0.22116E-04   0.33820E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6545e+05                             2
a  Local Time Step      1.1583e-05                         44394


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.251          2.7859      -0.0019391      3.1082e-06
v  Velocity[Y]                 -15.118           33.57          6.7293          20.056
v  Velocity[Z]                 -28.243          28.974        0.022139      -0.0077786
v  ǁVelocityǁ                 0.009194          33.688           10.52          20.219
v  Pressure                    -388.31          339.75         -58.766           30.79
v  k                         3.548e-09          42.146          4.2659           1.585
v  omega                         1e-24      1.6265e+07            8348          11.879
v  turbulent_viscosity      2.5699e-14          1.3014         0.01575          0.1052
v  CourantNb                  0.053996          2009.4          43.561          1.3775
v  FourierNb                   0.01066           15836          101.08         0.66582
v  total_pressure           1.0094e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14929        0.010817        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15898          144.64          2.0433


 TIME FOR THE TIME STEP              269:        0.45556E+02

===============================================================


 INSTANT    0.270000000E+02   TIME STEP NUMBER             270
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.186062103E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28926E+02 0.21295E+02
   Friction velocity        uet   :  0.20541E-02 0.27439E+01
   Friction velocity        uk    :  0.32021E-01 0.30498E+01
   Dimensionless distance   yplus :  0.12997E+00 0.37152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        474
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    1784   0.45331E-02   0.44559E+00 
c  VelocityY    0.29372E+04    1784   0.45331E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    1784   0.45331E-02   0.00000E+00 
c  Pressure     0.43284E+00    6921   0.28799E-01   0.20701E+00 
c  k            0.20492E+04    1558   0.78732E-04   0.13525E+01 
c  omega        0.10818E+08     297   0.25556E-04   0.16522E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2597e+05                             2
a  Local Time Step       1.181e-05                         44325


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5494           2.766       0.0014437      3.8342e-06
v  Velocity[Y]                 -14.925          31.323          6.7448          20.057
v  Velocity[Z]                  -28.37          28.902        0.024134      -0.0080383
v  ǁVelocityǁ                 0.027492          33.619          10.521           20.22
v  Pressure                    -375.66          341.62         -59.082          30.692
v  k                        2.8049e-10          40.041          4.1919          1.5871
v  omega                         1e-24      1.1779e+07          8221.3          11.854
v  turbulent_viscosity      4.6456e-16          1.3018        0.015727         0.10521
v  CourantNb                  0.048488          1981.6          43.595           1.378
v  FourierNb                  0.010666           16010          100.13          0.6651
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010816        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16076          143.72          2.0431


 TIME FOR THE TIME STEP              270:        0.45763E+02

===============================================================


 INSTANT    0.271000000E+02   TIME STEP NUMBER             271
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271286306E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30245E+02 0.20705E+02
   Friction velocity        uet   :  0.12283E-02 0.27283E+01
   Friction velocity        uk    :  0.33739E-01 0.29657E+01
   Dimensionless distance   yplus :  0.14868E+00 0.29808E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29371E+04    1624   0.45442E-02   0.43943E+00 
c  VelocityY    0.29371E+04    1624   0.45442E-02   0.00000E+00 
c  VelocityZ    0.29371E+04    1624   0.45442E-02   0.00000E+00 
c  Pressure     0.40983E+00    7055   0.27541E-01   0.19526E+00 
c  k            0.20536E+04    1470   0.81120E-04   0.14519E+01 
c  omega        0.10157E+08     258   0.33315E-04   0.16300E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3074e+05                             2
a  Local Time Step      1.1797e-05                         44307


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8553          2.8799       0.0046497      1.5915e-06
v  Velocity[Y]                 -15.122          30.506          6.7868          20.057
v  Velocity[Z]                 -31.713          29.013        0.020943      -0.0081373
v  ǁVelocityǁ                 0.015496          36.559          10.539           20.22
v  Pressure                    -347.98          344.89         -57.077          30.932
v  k                        1.4281e-09          49.376          4.1143          1.5896
v  omega                         1e-24      1.2189e+07          8076.8          11.834
v  turbulent_viscosity      1.1035e-16           1.303        0.015701         0.10523
v  CourantNb                  0.033429          1992.4          43.964          1.3784
v  FourierNb                  0.010674           16233          98.348         0.66411
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14899        0.010816        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16303          142.31          2.0425


 TIME FOR THE TIME STEP              271:        0.43084E+02

===============================================================


 INSTANT    0.272000000E+02   TIME STEP NUMBER             272
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.522096219E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29897E+02 0.17542E+02
   Friction velocity        uet   :  0.19877E-03 0.30719E+01
   Friction velocity        uk    :  0.28557E-01 0.31810E+01
   Dimensionless distance   yplus :  0.16263E+00 0.27158E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29370E+04    1837   0.44124E-02   0.43155E+00 
c  VelocityY    0.29370E+04    1837   0.44124E-02   0.00000E+00 
c  VelocityZ    0.29370E+04    1837   0.44124E-02   0.00000E+00 
c  Pressure     0.41069E+00    7108   0.31263E-01   0.19435E+00 
c  k            0.20622E+04    1081   0.84812E-04   0.15955E+01 
c  omega        0.10130E+08     240   0.55957E-04   0.28474E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0178e+05                             3
a  Local Time Step       1.179e-05                         44337


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1042          2.8741       0.0069848      2.1316e-06
v  Velocity[Y]                 -14.959           30.42          6.8525          20.056
v  Velocity[Z]                 -31.935          28.682        0.014635      -0.0077374
v  ǁVelocityǁ                  0.01152          36.612          10.583           20.22
v  Pressure                    -401.11          347.05         -54.648          31.156
v  k                        1.2048e-09          59.826          4.0436          1.5924
v  omega                         1e-24       1.622e+07          8129.9          11.829
v  turbulent_viscosity      3.7237e-15          1.3024        0.015677         0.10527
v  CourantNb                  0.048744          2011.8          44.223          1.3785
v  FourierNb                  0.010683           16458          96.822         0.66319
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14812        0.010814        0.045735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99081           16534          141.04          2.0417


 TIME FOR THE TIME STEP              272:        0.44708E+02

===============================================================


 INSTANT    0.273000000E+02   TIME STEP NUMBER             273
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.575286249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29596E+02 0.12621E+02
   Friction velocity        uet   :  0.11711E-02 0.31050E+01
   Friction velocity        uk    :  0.12670E-01 0.32411E+01
   Dimensionless distance   yplus :  0.36790E-01 0.27111E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29371E+04    1874   0.46198E-02   0.42486E+00 
c  VelocityY    0.29371E+04    1874   0.46198E-02   0.00000E+00 
c  VelocityZ    0.29371E+04    1874   0.46198E-02   0.00000E+00 
c  Pressure     0.41368E+00    7108   0.36501E-01   0.19592E+00 
c  k            0.20770E+04    1537   0.85982E-04   0.17156E+01 
c  omega        0.14813E+08     199   0.97881E-04   0.72088E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2623e+05                             3
a  Local Time Step      1.2337e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5449          2.8365       0.0079299      -1.211e-07
v  Velocity[Y]                 -15.146          32.336          6.9339          20.057
v  Velocity[Z]                  -33.04          28.633        0.031771      -0.0070475
v  ǁVelocityǁ                 0.015931          35.195          10.634           20.22
v  Pressure                    -431.78          348.43         -51.916           31.78
v  k                        3.3939e-09          65.725           3.994          1.5956
v  omega                         1e-24      6.0113e+07          8197.2          11.819
v  turbulent_viscosity      3.0619e-15          1.3001        0.015659         0.10532
v  CourantNb                  0.063778          2401.5          44.573          1.3785
v  FourierNb                  0.010693           16591          95.624         0.66273
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14848        0.010812        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16673           140.2          2.0412


 TIME FOR THE TIME STEP              273:        0.47332E+02

===============================================================


 INSTANT    0.274000000E+02   TIME STEP NUMBER             274
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.411263183E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28747E+02 0.13091E+02
   Friction velocity        uet   :  0.18450E-03 0.31745E+01
   Friction velocity        uk    :  0.24535E-01 0.28552E+01
   Dimensionless distance   yplus :  0.13570E+00 0.26815E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :        934
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    1894   0.44183E-02   0.41843E+00 
c  VelocityY    0.29372E+04    1894   0.44183E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    1894   0.44183E-02   0.00000E+00 
c  Pressure     0.43547E+00    6974   0.38771E-01   0.20568E+00 
c  k            0.20965E+04    1693   0.85232E-04   0.17718E+01 
c  omega        0.20507E+08     146   0.78569E-04   0.82071E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9549e+05                             3
a  Local Time Step      1.2174e-05                         44358


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6059          2.9836         0.00729     -7.3457e-07
v  Velocity[Y]                 -20.602          30.082          6.9831          20.056
v  Velocity[Z]                  -33.13          28.649        0.068121      -0.0062439
v  ǁVelocityǁ                 0.010374          34.897          10.646          20.219
v  Pressure                    -439.86          348.24         -49.956          31.998
v  k                        1.3331e-09          62.035          3.9599          1.5989
v  omega                         1e-24      6.2199e+07          8167.1          11.802
v  turbulent_viscosity      8.5079e-15          1.2959        0.015654         0.10538
v  CourantNb                  0.025876          2760.5          44.974          1.3783
v  FourierNb                  0.010704           16509          94.838          0.6626
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010812        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16593          139.81          2.0409


 TIME FOR THE TIME STEP              274:        0.46479E+02

===============================================================


 INSTANT    0.275000000E+02   TIME STEP NUMBER             275
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.292940323E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30342E+02 0.14751E+02
   Friction velocity        uet   :  0.28324E-02 0.29806E+01
   Friction velocity        uk    :  0.17734E-01 0.29197E+01
   Dimensionless distance   yplus :  0.15028E+00 0.26566E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :        945
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    1833   0.45475E-02   0.38221E+00 
c  VelocityY    0.29375E+04    1833   0.45475E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    1833   0.45475E-02   0.00000E+00 
c  Pressure     0.43065E+00    7093   0.36313E-01   0.20348E+00 
c  k            0.21160E+04    1728   0.87927E-04   0.18105E+01 
c  omega        0.19854E+08     160   0.45782E-04   0.50010E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -58399                             2
a  Local Time Step      1.1364e-05                         44364


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5612          3.1089       0.0059328     -1.2833e-06
v  Velocity[Y]                 -24.409          29.894          6.9476          20.056
v  Velocity[Z]                 -33.282          28.317         0.11713       -0.005521
v  ǁVelocityǁ                 0.019009          34.031          10.594          20.219
v  Pressure                    -429.37          348.01         -48.473          32.186
v  k                         1.328e-07          50.421          3.9529          1.6022
v  omega                         1e-24      3.1942e+07          8331.5          11.835
v  turbulent_viscosity      4.0366e-15          1.2922        0.015639         0.10545
v  CourantNb                  0.033769          2473.1          45.222          1.3782
v  FourierNb                  0.010705           16247          94.424          0.6625
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14789        0.010811         0.04565


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16330          139.65          2.0407


 TIME FOR THE TIME STEP              275:        0.46507E+02

===============================================================


 INSTANT    0.276000000E+02   TIME STEP NUMBER             276
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.319511250E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30586E+02 0.15928E+02
   Friction velocity        uet   :  0.56924E-03 0.28752E+01
   Friction velocity        uk    :  0.19739E-01 0.30875E+01
   Dimensionless distance   yplus :  0.85796E-01 0.26341E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    1707   0.45798E-02   0.34770E+00 
c  VelocityY    0.29377E+04    1707   0.45798E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    1707   0.45798E-02   0.00000E+00 
c  Pressure     0.41986E+00    7070   0.30953E-01   0.19812E+00 
c  k            0.21314E+04    1629   0.99033E-04   0.17898E+01 
c  omega        0.11927E+08     216   0.53897E-03   0.15058E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0782e+05                             4
a  Local Time Step      1.0936e-05                         44344


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5832          3.0845       0.0038614     -1.6908e-06
v  Velocity[Y]                 -31.671           29.74          6.8407          20.057
v  Velocity[Z]                  -29.97           28.37          0.1333      -0.0043979
v  ǁVelocityǁ                 0.014939           33.21          10.561          20.219
v  Pressure                    -405.46          347.04         -48.098          31.906
v  k                        8.4943e-07           74.67          3.9948          1.6056
v  omega                         1e-24      3.0244e+08          9742.8          11.951
v  turbulent_viscosity        7.41e-14          1.2862        0.015629         0.10554
v  CourantNb                  0.016158          2070.8          45.012          1.3778
v  FourierNb                  0.010701           15877          93.008         0.66263
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01           0.148         0.01081         0.04563


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15958          138.02          2.0405


 TIME FOR THE TIME STEP              276:        0.45097E+02

===============================================================


 INSTANT    0.277000000E+02   TIME STEP NUMBER             277
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.455730460E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31261E+02 0.21460E+02
   Friction velocity        uet   :  0.10842E-02 0.27861E+01
   Friction velocity        uk    :  0.67148E-02 0.30986E+01
   Dimensionless distance   yplus :  0.60469E-01 0.26249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1042
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    1627   0.44264E-02   0.32939E+00 
c  VelocityY    0.29378E+04    1627   0.44264E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    1627   0.44264E-02   0.00000E+00 
c  Pressure     0.43876E+00    7040   0.30021E-01   0.20654E+00 
c  k            0.21387E+04    1445   0.11848E-03   0.16744E+01 
c  omega        0.36275E+09      78   0.78929E-05   0.42369E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                      -0.00207                             2
a  omega                    -96528                             6
a  Local Time Step      1.1288e-05                         44260


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8206          2.8604       0.0017928     -4.7356e-06
v  Velocity[Y]                 -36.621          30.044          6.7489          20.056
v  Velocity[Z]                 -28.501           28.55         0.14626      -0.0033813
v  ǁVelocityǁ                0.0081255           41.32          10.552          20.219
v  Pressure                    -406.28          345.93         -49.134          31.743
v  k                        2.6175e-08          95.141          4.0749          1.6091
v  omega                         1e-24       1.514e+08          9327.5          11.952
v  turbulent_viscosity      1.3446e-13           1.283        0.015625         0.10564
v  CourantNb                  0.026709            2072          44.819          1.3775
v  FourierNb                  0.010698           15601          92.281         0.66337
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010811        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15677           137.1          2.0409


 TIME FOR THE TIME STEP              277:        0.43257E+02

===============================================================


 INSTANT    0.278000000E+02   TIME STEP NUMBER             278
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.533782793E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63769E+02 0.13527E+02
   Friction velocity        uet   :  0.14670E-02 0.35142E+01
   Friction velocity        uk    :  0.85312E-02 0.43134E+01
   Dimensionless distance   yplus :  0.98405E-01 0.34103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        452
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1753   0.42151E-02   0.32608E+00 
c  VelocityY    0.29379E+04    1753   0.42151E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1753   0.42151E-02   0.00000E+00 
c  Pressure     0.40323E+00    7112   0.35036E-01   0.19037E+00 
c  k            0.21398E+04    1130   0.12112E-03   0.15271E+01 
c  omega        0.91812E+08     276   0.72656E-04   0.10376E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -6.7824e-05                             1
a  omega               -2.5059e+05                             6
a  Local Time Step      1.0981e-05                         44204


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4533          2.4537     -0.00058418     -2.4721e-06
v  Velocity[Y]                 -33.749          30.217          6.7001          20.056
v  Velocity[Z]                 -28.452           28.43         0.14451      -0.0022562
v  ǁVelocityǁ                0.0091545          34.519          10.551          20.218
v  Pressure                    -409.08          345.42          -51.07          31.951
v  k                        1.7329e-09          51.657          4.1225          1.6126
v  omega                         1e-24      2.5152e+08          9771.1          11.977
v  turbulent_viscosity      2.5391e-14          1.2772        0.015648         0.10576
v  CourantNb                  0.043791          2063.7           44.67          1.3774
v  FourierNb                  0.010695           15334          92.425         0.66457
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010812        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15404           137.1          2.0419


 TIME FOR THE TIME STEP              278:        0.44558E+02

===============================================================


 INSTANT    0.279000000E+02   TIME STEP NUMBER             279
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.553855521E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31331E+02 0.13412E+02
   Friction velocity        uet   :  0.18001E-02 0.32382E+01
   Friction velocity        uk    :  0.17530E-01 0.30104E+01
   Dimensionless distance   yplus :  0.14465E+00 0.26220E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        486
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1870   0.45880E-02   0.32342E+00 
c  VelocityY    0.29381E+04    1870   0.45880E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1870   0.45880E-02   0.00000E+00 
c  Pressure     0.40125E+00    6942   0.38685E-01   0.18912E+00 
c  k            0.21389E+04    1324   0.81708E-04   0.13913E+01 
c  omega        0.24907E+09     152   0.10784E-04   0.34362E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00069632                             1
a  omega          
a  Local Time Step      1.0996e-05                         44170


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6368          1.8813      -0.0031605      4.0147e-07
v  Velocity[Y]                 -19.689          31.856          6.6761          20.056
v  Velocity[Z]                 -28.729          28.624         0.13075     -0.00081244
v  ǁVelocityǁ                0.0095512          33.568          10.543          20.218
v  Pressure                    -410.76          345.18         -53.489           31.87
v  k                        1.1619e-10          54.784          4.1698           1.616
v  omega                         1e-24      1.2597e+08          9186.7          11.942
v  turbulent_viscosity      1.8716e-15          1.2731        0.015689         0.10588
v  CourantNb                  0.049133          3150.7          44.681          1.3772
v  FourierNb                  0.010694           15297          92.868         0.66588
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14785        0.010812        0.045629


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15360          137.55          2.0431


 TIME FOR THE TIME STEP              279:        0.44843E+02

===============================================================


 INSTANT    0.280000000E+02   TIME STEP NUMBER             280
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.263357631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30739E+02 0.13274E+02
   Friction velocity        uet   :  0.53072E-03 0.29686E+01
   Friction velocity        uk    :  0.18699E-01 0.31209E+01
   Dimensionless distance   yplus :  0.14653E+00 0.26955E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1910   0.43606E-02   0.33453E+00 
c  VelocityY    0.29382E+04    1910   0.43606E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1910   0.43606E-02   0.00000E+00 
c  Pressure     0.42718E+00    7104   0.36603E-01   0.20059E+00 
c  k            0.21375E+04    1499   0.75796E-04   0.12948E+01 
c  omega        0.67197E+08     189   0.21304E-04   0.99755E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2627e+05                             1
a  Local Time Step      1.0472e-05                         44140


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8314          1.6441      -0.0056011      2.8366e-06
v  Velocity[Y]                 -17.358          34.105          6.6793          20.056
v  Velocity[Z]                 -28.458          28.953         0.10486      0.00044742
v  ǁVelocityǁ                 0.023492          34.507          10.532          20.218
v  Pressure                    -409.13          344.97         -55.524          31.944
v  k                        4.0157e-09          52.378          4.2291          1.6195
v  omega                         1e-24      6.3434e+07          8647.9          11.893
v  turbulent_viscosity      3.1147e-16          1.2676         0.01576         0.10602
v  CourantNb                  0.026479            2490          44.191          1.3771
v  FourierNb                  0.010692           15345          94.664         0.66781
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14827        0.010812        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15400          138.86          2.0449


 TIME FOR THE TIME STEP              280:        0.46752E+02

===============================================================


 INSTANT    0.281000000E+02   TIME STEP NUMBER             281
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.165767938E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30630E+02 0.13727E+02
   Friction velocity        uet   :  0.81366E-03 0.30335E+01
   Friction velocity        uk    :  0.28245E-01 0.31796E+01
   Dimensionless distance   yplus :  0.14016E+00 0.29726E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        490
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1862   0.45142E-02   0.35059E+00 
c  VelocityY    0.29384E+04    1862   0.45142E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1862   0.45142E-02   0.00000E+00 
c  Pressure     0.41657E+00    7078   0.33500E-01   0.19659E+00 
c  k            0.21352E+04    1516   0.84738E-04   0.14087E+01 
c  omega        0.23067E+08     348   0.31299E-04   0.31795E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1407e-05                         44155


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0021          1.9805      -0.0072363      4.4072e-06
v  Velocity[Y]                  -16.24          34.604          6.7061          20.055
v  Velocity[Z]                 -28.971          28.885         0.07937        0.001648
v  ǁVelocityǁ                   0.0258          34.805          10.516          20.217
v  Pressure                     -401.9          345.05         -57.001          31.635
v  k                        1.8951e-08          56.407           4.218          1.6228
v  omega                         1e-24      3.2658e+07          8350.9          11.857
v  turbulent_viscosity      7.2368e-16          1.2605        0.015836         0.10616
v  CourantNb                    0.0214          2098.2          43.689          1.3771
v  FourierNb                  0.010692           15449          97.121         0.66972
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010811        0.045628


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15506          140.81          2.0468


 TIME FOR THE TIME STEP              281:        0.45954E+02

===============================================================


 INSTANT    0.282000000E+02   TIME STEP NUMBER             282
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.143018105E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29806E+02 0.13751E+02
   Friction velocity        uet   :  0.18930E-02 0.29680E+01
   Friction velocity        uk    :  0.23793E-01 0.29067E+01
   Dimensionless distance   yplus :  0.13372E+00 0.33228E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        448
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1615   0.46652E-02   0.36748E+00 
c  VelocityY    0.29384E+04    1615   0.46652E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1615   0.46652E-02   0.00000E+00 
c  Pressure     0.43828E+00    6990   0.31568E-01   0.20653E+00 
c  k            0.21311E+04    1400   0.82494E-04   0.13999E+01 
c  omega        0.12563E+08     419   0.37325E-04   0.29317E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8382e+05                             1
a  Local Time Step      1.1452e-05                         44210


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2164          2.3202       -0.007851      5.9037e-06
v  Velocity[Y]                 -15.016          34.019          6.7265          20.056
v  Velocity[Z]                 -28.621          29.428        0.053972       0.0025603
v  ǁVelocityǁ                 0.011877          34.526          10.517          20.217
v  Pressure                    -384.28          344.49         -58.395          31.338
v  k                        2.0256e-08          44.883          4.1315          1.6259
v  omega                         1e-24      1.8189e+07          8366.5          11.874
v  turbulent_viscosity      2.1132e-15          1.2508        0.015859         0.10631
v  CourantNb                   0.03232          2100.4          43.561          1.3773
v  FourierNb                  0.010691           15532          98.576         0.67077
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010811        0.045619


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15594          142.14           2.048


 TIME FOR THE TIME STEP              282:        0.42927E+02

===============================================================


 INSTANT    0.283000000E+02   TIME STEP NUMBER             283
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.344519236E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30376E+02 0.21862E+02
   Friction velocity        uet   :  0.18908E-02 0.28554E+01
   Friction velocity        uk    :  0.34129E-01 0.30241E+01
   Dimensionless distance   yplus :  0.12146E+00 0.38374E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    1383   0.45094E-02   0.37041E+00 
c  VelocityY    0.29385E+04    1383   0.45094E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    1383   0.45094E-02   0.00000E+00 
c  Pressure     0.43974E+00    6986   0.28172E-01   0.20773E+00 
c  k            0.21258E+04    1136   0.76986E-04   0.13655E+01 
c  omega        0.10719E+08     309   0.31573E-04   0.18512E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.677e+05                             2
a  Local Time Step      1.1192e-05                         44230


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.3045          2.5756      -0.0065318       8.238e-06
v  Velocity[Y]                 -16.194          32.634          6.7301          20.056
v  Velocity[Z]                 -28.443          29.129        0.037362       0.0035695
v  ǁVelocityǁ                0.0039348          32.795           10.51          20.217
v  Pressure                    -370.74          344.48         -58.606          31.019
v  k                         3.171e-09          39.927          4.0287          1.6288
v  omega                         1e-24      1.1755e+07          8237.7          11.862
v  turbulent_viscosity      1.0899e-13          1.2415        0.015808         0.10646
v  CourantNb                  0.010483          2095.9           43.71          1.3777
v  FourierNb                  0.010692           15623          97.356         0.67047
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010812        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92532           15691          141.07          2.0482


 TIME FOR THE TIME STEP              283:        0.39847E+02

===============================================================


 INSTANT    0.284000000E+02   TIME STEP NUMBER             284
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.493913117E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30454E+02 0.20843E+02
   Friction velocity        uet   :  0.16566E-02 0.26642E+01
   Friction velocity        uk    :  0.26233E-01 0.31814E+01
   Dimensionless distance   yplus :  0.81614E-01 0.29792E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        384
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    1619   0.44459E-02   0.37802E+00 
c  VelocityY    0.29385E+04    1619   0.44459E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    1619   0.44459E-02   0.00000E+00 
c  Pressure     0.41687E+00    6993   0.25703E-01   0.19633E+00 
c  k            0.21207E+04    1226   0.77152E-04   0.14464E+01 
c  omega        0.10330E+08     231   0.32126E-04   0.16525E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0595e+05                             2
a  Local Time Step      1.1591e-05                         44214


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                   -3.29           2.711      -0.0054349      8.7456e-06
v  Velocity[Y]                 -16.127          30.201          6.7632          20.056
v  Velocity[Z]                 -30.729          29.169        0.014522       0.0042621
v  ǁVelocityǁ                 0.017749           36.17          10.507          20.216
v  Pressure                     -352.8          345.38         -56.939          31.135
v  k                         2.368e-09          48.893           3.949          1.6317
v  omega                         1e-24      1.2828e+07          8236.1          11.861
v  turbulent_viscosity      1.7706e-14          1.2335         0.01574         0.10661
v  CourantNb                  0.037811          2112.7          43.864           1.378
v  FourierNb                  0.010693           15760          95.593         0.66998
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14783        0.010812        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9807           15835          139.46           2.048


 TIME FOR THE TIME STEP              284:        0.42403E+02

===============================================================


 INSTANT    0.285000000E+02   TIME STEP NUMBER             285
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.868741608E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30582E+02 0.19871E+02
   Friction velocity        uet   :  0.83089E-03 0.29284E+01
   Friction velocity        uk    :  0.26773E-01 0.32083E+01
   Dimensionless distance   yplus :  0.13035E+00 0.27236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1784   0.44779E-02   0.37967E+00 
c  VelocityY    0.29386E+04    1784   0.44779E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1784   0.44779E-02   0.00000E+00 
c  Pressure     0.41943E+00    7067   0.28374E-01   0.19887E+00 
c  k            0.21176E+04    1489   0.78964E-04   0.15897E+01 
c  omega        0.10325E+08     230   0.31892E-04   0.27691E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.712e+05                             2
a  Local Time Step      1.1161e-05                         44246


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1726           2.983      -0.0052536      9.2008e-06
v  Velocity[Y]                 -14.557          31.017          6.8187          20.056
v  Velocity[Z]                 -31.832           29.02       -0.016735       0.0050438
v  ǁVelocityǁ                0.0096903          36.513           10.53          20.216
v  Pressure                    -381.55          346.85         -54.308          31.422
v  k                         1.149e-09          60.024          3.9067          1.6345
v  omega                         1e-24      2.5751e+07          8080.4          11.831
v  turbulent_viscosity      2.1008e-15          1.2249         0.01569         0.10677
v  CourantNb                  0.083861          2118.3          44.187          1.3782
v  FourierNb                  0.010696           15778          94.134         0.66973
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14808        0.010813        0.045622


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81724           15861          138.32          2.0479


 TIME FOR THE TIME STEP              285:        0.45353E+02

===============================================================


 INSTANT    0.286000000E+02   TIME STEP NUMBER             286
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.196268221E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29947E+02 0.16080E+02
   Friction velocity        uet   :  0.13696E-02 0.30877E+01
   Friction velocity        uk    :  0.25374E-01 0.32014E+01
   Dimensionless distance   yplus :  0.99291E-01 0.26882E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        362
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1836   0.43895E-02   0.38117E+00 
c  VelocityY    0.29386E+04    1836   0.43895E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1836   0.43895E-02   0.00000E+00 
c  Pressure     0.39426E+00    7115   0.33514E-01   0.18580E+00 
c  k            0.21195E+04    1595   0.81558E-04   0.17232E+01 
c  omega        0.11705E+08     230   0.95735E-03   0.90669E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5647e+05                             2
a  Local Time Step      1.1821e-05                         44323


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0262          3.1553      -0.0062353      8.1629e-06
v  Velocity[Y]                 -15.113           33.02          6.8778          20.056
v  Velocity[Z]                 -32.591          29.084       -0.024522       0.0059703
v  ǁVelocityǁ                 0.014334          36.174          10.583          20.215
v  Pressure                     -421.3           347.7         -51.737          31.886
v  k                        5.1593e-10          67.524           3.893          1.6372
v  omega                         1e-24      6.7208e+08          9888.2           11.97
v  turbulent_viscosity      1.0826e-15           1.217        0.015658         0.10692
v  CourantNb                  0.032073          2348.2          44.359           1.378
v  FourierNb                  0.010699           15660          93.321         0.66947
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14883        0.010813        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15746          137.68          2.0474


 TIME FOR THE TIME STEP              286:        0.47710E+02

===============================================================


 INSTANT    0.287000000E+02   TIME STEP NUMBER             287
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.515241936E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30964E+02 0.14445E+02
   Friction velocity        uet   :  0.22939E-02 0.32239E+01
   Friction velocity        uk    :  0.21589E-01 0.29976E+01
   Dimensionless distance   yplus :  0.18946E+00 0.26570E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1759   0.44764E-02   0.38631E+00 
c  VelocityY    0.29389E+04    1759   0.44764E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1759   0.44764E-02   0.00000E+00 
c  Pressure     0.40905E+00    7112   0.36515E-01   0.19214E+00 
c  k            0.21280E+04    1602   0.82154E-04   0.18109E+01 
c  omega        0.27018E+10      36   0.22795E-05   0.24285E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6671e+05                             2
a  Local Time Step       1.109e-05                         44371


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.927          3.2335      -0.0071572       4.896e-06
v  Velocity[Y]                 -18.739          29.937          6.9191          20.056
v  Velocity[Z]                 -32.796          29.041       0.0063992       0.0066083
v  ǁVelocityǁ                0.0068283           34.77          10.619          20.215
v  Pressure                    -438.31          347.32         -50.089          31.994
v  k                        5.3036e-09          67.754          3.9056          1.6398
v  omega                         1e-24      3.3602e+08          9651.8          11.945
v  turbulent_viscosity       7.183e-16          1.2173        0.015634         0.10707
v  CourantNb                  0.033281          2761.6          44.593          1.3776
v  FourierNb                  0.010703           15379          91.947         0.66912
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14929        0.010813        0.045597


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           15465          136.54          2.0468


 TIME FOR THE TIME STEP              287:        0.45019E+02

===============================================================


 INSTANT    0.288000000E+02   TIME STEP NUMBER             288
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.231943062E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31144E+02 0.15025E+02
   Friction velocity        uet   :  0.12021E-02 0.29363E+01
   Friction velocity        uk    :  0.17053E-01 0.31674E+01
   Dimensionless distance   yplus :  0.74493E-01 0.26363E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :       1060
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1693   0.45599E-02   0.37354E+00 
c  VelocityY    0.29390E+04    1693   0.45599E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1693   0.45599E-02   0.00000E+00 
c  Pressure     0.44451E+00    7089   0.35368E-01   0.20909E+00 
c  k            0.21394E+04    1542   0.85695E-04   0.18886E+01 
c  omega        0.67607E+09      53   0.43400E-05   0.66114E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1709e+05                             4
a  Local Time Step      1.1716e-05                         44434


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6126          3.3571      -0.0077328      2.9651e-06
v  Velocity[Y]                  -23.78           29.78          6.9034          20.056
v  Velocity[Z]                 -32.883          28.974        0.040384        0.006854
v  ǁVelocityǁ                0.0017105          33.961          10.616          20.215
v  Pressure                    -436.12          346.81         -48.839          32.249
v  k                        8.2533e-08          57.284          3.9367          1.6421
v  omega                         1e-24      1.6802e+08          9321.6          11.958
v  turbulent_viscosity      1.0256e-14          1.2181        0.015637         0.10722
v  CourantNb                     0.017          2652.9          44.762          1.3773
v  FourierNb                  0.010708           14790           91.48         0.66937
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010814        0.045611


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14873          136.24          2.0467


 TIME FOR THE TIME STEP              288:        0.45307E+02

===============================================================


 INSTANT    0.289000000E+02   TIME STEP NUMBER             289
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.529088219E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31904E+02 0.13587E+02
   Friction velocity        uet   :  0.35758E-02 0.28785E+01
   Friction velocity        uk    :  0.20886E-01 0.28566E+01
   Dimensionless distance   yplus :  0.17090E+00 0.26263E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        444
   Nb of faces within the viscous sub-layer     :       1042
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1673   0.44741E-02   0.34680E+00 
c  VelocityY    0.29392E+04    1673   0.44741E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1673   0.44741E-02   0.00000E+00 
c  Pressure     0.44372E+00    6994   0.31306E-01   0.20960E+00 
c  k            0.21490E+04    1374   0.90175E-04   0.19367E+01 
c  omega        0.16995E+09      95   0.48137E-04   0.22309E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.283e+05                             3
a  Local Time Step      1.1637e-05                         44474


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0745          3.3102      -0.0074722      -2.605e-07
v  Velocity[Y]                 -33.317          29.644          6.8154          20.056
v  Velocity[Z]                 -31.792           28.96        0.065683       0.0067774
v  ǁVelocityǁ                 0.005954          33.656          10.601          20.215
v  Pressure                    -418.92          346.24         -48.682          32.055
v  k                        7.0935e-09          65.175          4.0056          1.6441
v  omega                         1e-24      3.6814e+08           10443          12.022
v  turbulent_viscosity      1.3527e-14          1.2213        0.015646         0.10737
v  CourantNb                  0.039135            2056          44.815           1.377
v  FourierNb                  0.010714           14246          91.567         0.67007
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010816        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14323          136.38          2.0471


 TIME FOR THE TIME STEP              289:        0.44071E+02

===============================================================


 INSTANT    0.290000000E+02   TIME STEP NUMBER             290
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.121231557E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31551E+02 0.22830E+02
   Friction velocity        uet   :  0.22429E-02 0.30454E+01
   Friction velocity        uk    :  0.18946E-01 0.28664E+01
   Dimensionless distance   yplus :  0.11909E+00 0.26171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :       1098
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1594   0.43929E-02   0.32832E+00 
c  VelocityY    0.29393E+04    1594   0.43929E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1594   0.43929E-02   0.00000E+00 
c  Pressure     0.44479E+00    7060   0.29599E-01   0.21086E+00 
c  k            0.21528E+04    1042   0.11642E-03   0.18640E+01 
c  omega        0.53330E+09      62   0.62293E-05   0.57278E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -8.3832e-05                             1
a  omega               -1.6553e+05                             6
a  Local Time Step      1.1578e-05                         44468


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.426          3.0156      -0.0068977      -2.955e-06
v  Velocity[Y]                  -22.24           29.81          6.7121          20.056
v  Velocity[Z]                 -28.556           28.56        0.072573       0.0065095
v  ǁVelocityǁ                0.0039225          33.193          10.622          20.215
v  Pressure                    -406.98          344.74         -50.265          31.815
v  k                        5.3944e-09           107.3          4.1149           1.646
v  omega                         1e-24      1.8422e+08          9399.6           11.96
v  turbulent_viscosity      4.9847e-15          1.2249        0.015683         0.10752
v  CourantNb                  0.036304          2022.1          44.604          1.3767
v  FourierNb                   0.01072           13983          92.795          0.6715
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010817        0.045652


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14045           137.4          2.0482


 TIME FOR THE TIME STEP              290:        0.41551E+02

===============================================================


 INSTANT    0.291000000E+02   TIME STEP NUMBER             291
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.255784098E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30202E+02 0.17281E+02
   Friction velocity        uet   :  0.29710E-02 0.24806E+01
   Friction velocity        uk    :  0.14884E-01 0.36418E+01
   Dimensionless distance   yplus :  0.13221E+00 0.33309E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        436
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1710   0.43974E-02   0.32596E+00 
c  VelocityY    0.29393E+04    1710   0.43974E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1710   0.43974E-02   0.00000E+00 
c  Pressure     0.42141E+00    6979   0.32950E-01   0.19883E+00 
c  k            0.21506E+04    1368   0.15890E-03   0.17298E+01 
c  omega        0.13427E+09     278   0.13507E-04   0.15458E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7955e+05                             3
a  Local Time Step      1.0767e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93149          2.7815      -0.0061908      -4.363e-06
v  Velocity[Y]                 -35.136           30.32          6.6756          20.056
v  Velocity[Z]                 -28.531          28.691        0.094272       0.0060787
v  ǁVelocityǁ                0.0025967          35.348          10.648          20.214
v  Pressure                    -409.93          343.43         -53.134          31.785
v  k                        1.3076e-08          95.073          4.2152          1.6478
v  omega                         1e-24      9.2437e+07          8772.3           11.92
v  turbulent_viscosity       6.749e-15          1.2288        0.015746         0.10767
v  CourantNb                  0.036717          1994.9          44.446          1.3766
v  FourierNb                  0.010726           13977          94.907         0.67352
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1486        0.010817        0.045662


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14036          139.35          2.0501


 TIME FOR THE TIME STEP              291:        0.44680E+02

===============================================================


 INSTANT    0.292000000E+02   TIME STEP NUMBER             292
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.147122261E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37891E+02 0.14233E+02
   Friction velocity        uet   :  0.31401E-02 0.32965E+01
   Friction velocity        uk    :  0.12625E-01 0.35635E+01
   Dimensionless distance   yplus :  0.13678E+00 0.35662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    1743   0.44121E-02   0.32460E+00 
c  VelocityY    0.29394E+04    1743   0.44121E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    1743   0.44121E-02   0.00000E+00 
c  Pressure     0.42219E+00    7115   0.35633E-01   0.19919E+00 
c  k            0.21472E+04    1462   0.13113E-03   0.16434E+01 
c  omega        0.35620E+08     310   0.25129E-04   0.45518E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0756e+05                             2
a  Local Time Step      1.1097e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97099          2.9373      -0.0057733       -4.55e-06
v  Velocity[Y]                 -21.899          30.815          6.6749          20.056
v  Velocity[Z]                 -28.485          28.727          0.1173       0.0055645
v  ǁVelocityǁ                0.0062898          33.668          10.656          20.214
v  Pressure                    -410.81          342.38          -56.13          31.981
v  k                        8.6837e-09          55.504          4.2563          1.6496
v  omega                         1e-24      4.6881e+07          8368.7          11.873
v  turbulent_viscosity      6.4991e-16          1.2322        0.015789         0.10782
v  CourantNb                  0.030987          3001.1          44.591          1.3767
v  FourierNb                  0.010733           14114          95.878         0.67479
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14904        0.010817        0.045681


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           14171          140.47          2.0515


 TIME FOR THE TIME STEP              292:        0.44899E+02

===============================================================


 INSTANT    0.293000000E+02   TIME STEP NUMBER             293
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.120036530E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30726E+02 0.13979E+02
   Friction velocity        uet   :  0.15576E-02 0.26494E+01
   Friction velocity        uk    :  0.16362E-01 0.29440E+01
   Dimensionless distance   yplus :  0.11522E+00 0.26697E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1927   0.45006E-02   0.32932E+00 
c  VelocityY    0.29397E+04    1927   0.45006E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1927   0.45006E-02   0.00000E+00 
c  Pressure     0.42312E+00    7112   0.34465E-01   0.19993E+00 
c  k            0.21463E+04    1525   0.89458E-04   0.14945E+01 
c  omega        0.13715E+08     304   0.43938E-04   0.27112E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.4482e+05                             1
a  Local Time Step      1.1067e-05                         44395


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.256          2.9946      -0.0055319     -7.0285e-06
v  Velocity[Y]                 -17.647          31.785          6.6922          20.056
v  Velocity[Z]                 -28.454          28.901         0.13417       0.0048512
v  ǁVelocityǁ                0.0058895          33.709          10.645          20.214
v  Pressure                    -409.66          341.39         -58.598          31.896
v  k                        2.3774e-08          53.783          4.3023          1.6514
v  omega                         1e-24      2.4773e+07          8260.5           11.87
v  turbulent_viscosity      4.5782e-15          1.2354        0.015816         0.10797
v  CourantNb                  0.042992            2633          44.441          1.3767
v  FourierNb                  0.010741           14300          97.339         0.67564
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010815        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14356          141.78          2.0523


 TIME FOR THE TIME STEP              293:        0.46869E+02

===============================================================


 INSTANT    0.294000000E+02   TIME STEP NUMBER             294
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.574483553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30362E+02 0.13615E+02
   Friction velocity        uet   :  0.45863E-03 0.28944E+01
   Friction velocity        uk    :  0.29645E-01 0.31528E+01
   Dimensionless distance   yplus :  0.15012E+00 0.27976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        539
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1995   0.45100E-02   0.33635E+00 
c  VelocityY    0.29399E+04    1995   0.45100E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1995   0.45100E-02   0.00000E+00 
c  Pressure     0.41919E+00    7073   0.31659E-01   0.19784E+00 
c  k            0.21483E+04    1536   0.98061E-04   0.15782E+01 
c  omega        0.10832E+08     468   0.35573E-04   0.13837E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0332e-05                         44406


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.411          3.0209      -0.0047183     -7.8159e-06
v  Velocity[Y]                  -16.56          33.439          6.7207          20.057
v  Velocity[Z]                 -28.514          28.836         0.13471       0.0040479
v  ǁVelocityǁ                 0.015207          33.819          10.614          20.214
v  Pressure                    -405.71           341.4         -59.724          31.833
v  k                        6.8399e-08          52.043          4.2965          1.6532
v  omega                         1e-24      1.2415e+07          8103.9          11.865
v  turbulent_viscosity      8.1969e-15          1.2401        0.015828         0.10813
v  CourantNb                   0.05081          2029.3          44.225          1.3768
v  FourierNb                  0.010749           14563          99.131          0.6764
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14781        0.010814        0.045661


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14621          143.36          2.0532


 TIME FOR THE TIME STEP              294:        0.47767E+02

===============================================================


 INSTANT    0.295000000E+02   TIME STEP NUMBER             295
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271374293E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30557E+02 0.15160E+02
   Friction velocity        uet   :  0.11092E-02 0.29139E+01
   Friction velocity        uk    :  0.15255E-01 0.31797E+01
   Dimensionless distance   yplus :  0.42231E-01 0.32625E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1890   0.45312E-02   0.35027E+00 
c  VelocityY    0.29401E+04    1890   0.45312E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1890   0.45312E-02   0.00000E+00 
c  Pressure     0.43209E+00    7060   0.31036E-01   0.20398E+00 
c  k            0.21502E+04    1510   0.94025E-04   0.16178E+01 
c  omega        0.10205E+08     448   0.35571E-04   0.12814E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6374e+05                             1
a  Local Time Step      1.0691e-05                         44427


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7355          3.1884      -0.0034297     -6.4677e-06
v  Velocity[Y]                 -15.787          33.631          6.7296          20.057
v  Velocity[Z]                 -28.595          28.921         0.12399       0.0029043
v  ǁVelocityǁ                  0.01001          33.737          10.587          20.214
v  Pressure                    -392.69          340.04         -60.352           31.44
v  k                        7.5575e-08          46.174          4.2154          1.6551
v  omega                         1e-24      1.1701e+07            7990          11.837
v  turbulent_viscosity      6.9934e-14          1.2437        0.015806         0.10829
v  CourantNb                  0.054776          2056.5          44.068           1.377
v  FourierNb                  0.010757           14791          99.817          0.6766
v  total_pressure           1.0093e+05      1.0167e+05      1.0126e+05      1.0136e+05
v  Local Time Step                0.01         0.14814        0.010814        0.045638


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0047           14853          143.89          2.0536


 TIME FOR THE TIME STEP              295:        0.46944E+02

===============================================================


 INSTANT    0.296000000E+02   TIME STEP NUMBER             296
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.210792487E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30394E+02 0.21111E+02
   Friction velocity        uet   :  0.19698E-02 0.28122E+01
   Friction velocity        uk    :  0.15900E-01 0.32479E+01
   Dimensionless distance   yplus :  0.13362E+00 0.40822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        442
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2063   0.42819E-02   0.35705E+00 
c  VelocityY    0.29403E+04    2063   0.42819E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2063   0.42819E-02   0.00000E+00 
c  Pressure     0.44273E+00    7036   0.30323E-01   0.20854E+00 
c  k            0.21521E+04    1442   0.86992E-04   0.15528E+01 
c  omega        0.10198E+08     315   0.10774E-03   0.29188E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7745e+05                             4
a  Local Time Step      1.1276e-05                         44460


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5631          3.4483      -0.0012071     -3.6088e-06
v  Velocity[Y]                 -14.958          32.983          6.7213          20.056
v  Velocity[Z]                 -29.709          28.922         0.10217       0.0014723
v  ǁVelocityǁ                 0.011124            33.2          10.556          20.213
v  Pressure                     -376.8          339.78          -60.02          31.116
v  k                        4.2362e-11          46.581          4.1206           1.657
v  omega                         1e-24      2.9774e+07          8155.1           11.84
v  turbulent_viscosity      9.7243e-14          1.2496        0.015751         0.10846
v  CourantNb                  0.032717          2078.9          44.131          1.3774
v  FourierNb                  0.010765           15084          98.398         0.67615
v  total_pressure           1.0095e+05      1.0166e+05      1.0126e+05      1.0136e+05
v  Local Time Step                0.01         0.14733        0.010813        0.045623


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15154          142.53          2.0535


 TIME FOR THE TIME STEP              296:        0.47740E+02

===============================================================


 INSTANT    0.297000000E+02   TIME STEP NUMBER             297
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.340966959E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30361E+02 0.20838E+02
   Friction velocity        uet   :  0.31269E-02 0.27419E+01
   Friction velocity        uk    :  0.20679E-01 0.32420E+01
   Dimensionless distance   yplus :  0.15513E+00 0.31546E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        416
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2080   0.46175E-02   0.36892E+00 
c  VelocityY    0.29405E+04    2080   0.46175E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2080   0.46175E-02   0.00000E+00 
c  Pressure     0.43779E+00    7047   0.27861E-01   0.20667E+00 
c  k            0.21554E+04    1339   0.84567E-04   0.15940E+01 
c  omega        0.15327E+08     199   0.47952E-04   0.37231E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9142e+05                             1
a  Local Time Step      1.1202e-05                         44466


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9307           3.568       0.0010142     -2.6866e-06
v  Velocity[Y]                 -15.126          30.553           6.746          20.055
v  Velocity[Z]                 -30.158          29.168        0.076894      7.6453e-05
v  ǁVelocityǁ                 0.018851           34.87          10.535          20.211
v  Pressure                    -357.83          341.53         -57.781          31.338
v  k                        2.2513e-10          47.024          4.0256          1.6593
v  omega                         1e-24      2.3497e+07          8199.8           11.84
v  turbulent_viscosity      1.7699e-16           1.271        0.015694         0.10864
v  CourantNb                  0.064843          2094.6          44.433          1.3778
v  FourierNb                  0.010774           15384          97.287         0.67577
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14733        0.010813        0.045608


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15459          141.72          2.0536


 TIME FOR THE TIME STEP              297:        0.47622E+02

===============================================================


 INSTANT    0.298000000E+02   TIME STEP NUMBER             298
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.233005849E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30702E+02 0.19871E+02
   Friction velocity        uet   :  0.25039E-02 0.28741E+01
   Friction velocity        uk    :  0.16443E-01 0.29677E+01
   Dimensionless distance   yplus :  0.18175E+00 0.27165E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    2013   0.45376E-02   0.37728E+00 
c  VelocityY    0.29407E+04    2013   0.45376E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    2013   0.45376E-02   0.00000E+00 
c  Pressure     0.43030E+00    7004   0.27772E-01   0.20314E+00 
c  k            0.21611E+04    1119   0.82805E-04   0.17065E+01 
c  omega        0.12178E+08     214   0.36963E-04   0.16591E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4359e+05                             3
a  Local Time Step      1.1047e-05                         44451


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0722          3.5041       0.0022524     -3.3162e-06
v  Velocity[Y]                 -15.044          30.392          6.7966          20.056
v  Velocity[Z]                 -32.011          29.192         0.04437      -0.0013759
v  ǁVelocityǁ                 0.015735          36.593          10.533          20.212
v  Pressure                    -358.81          343.73         -54.663          31.931
v  k                        3.0603e-10           53.86          3.9735          1.6618
v  omega                         1e-24       1.442e+07          8045.6          11.833
v  turbulent_viscosity      1.1052e-15           1.292         0.01567         0.10883
v  CourantNb                  0.017221            2111          44.692          1.3779
v  FourierNb                  0.010781           15631          95.494         0.67554
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14822        0.010812        0.045578


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15709          140.19          2.0534


 TIME FOR THE TIME STEP              298:        0.46973E+02

===============================================================


 INSTANT    0.299000000E+02   TIME STEP NUMBER             299
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.223482455E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30843E+02 0.14971E+02
   Friction velocity        uet   :  0.34968E-02 0.31127E+01
   Friction velocity        uk    :  0.22929E-01 0.32258E+01
   Dimensionless distance   yplus :  0.11328E+00 0.27043E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        377
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1999   0.44460E-02   0.38165E+00 
c  VelocityY    0.29410E+04    1999   0.44460E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1999   0.44460E-02   0.00000E+00 
c  Pressure     0.44382E+00    7108   0.32172E-01   0.20975E+00 
c  k            0.21716E+04     952   0.85956E-04   0.18465E+01 
c  omega        0.10682E+08     218   0.86580E-04   0.41728E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9166e+05                             3
a  Local Time Step      1.1053e-05                         44421


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0633          3.2529       0.0027335     -2.1608e-06
v  Velocity[Y]                 -15.243          32.812          6.8591          20.056
v  Velocity[Z]                 -33.408          29.288        0.031364      -0.0030081
v  ǁVelocityǁ                 0.010089           36.42           10.57          20.212
v  Pressure                    -412.02          345.47         -51.651          32.328
v  k                         2.844e-09          65.697          3.9659          1.6646
v  omega                         1e-24      3.4896e+07          8224.3          11.849
v  turbulent_viscosity      5.8139e-16          1.3126        0.015691         0.10904
v  CourantNb                  0.020394          2206.1          44.706          1.3776
v  FourierNb                  0.010788           15782           94.38         0.67613
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14923        0.010812        0.045578


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96406           15861          139.09          2.0537


 TIME FOR THE TIME STEP              299:        0.44743E+02

===============================================================


 INSTANT    0.300000000E+02   TIME STEP NUMBER             300
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.438676808E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30444E+02 0.13648E+02
   Friction velocity        uet   :  0.38464E-02 0.32121E+01
   Friction velocity        uk    :  0.19920E-01 0.31423E+01
   Dimensionless distance   yplus :  0.22173E+00 0.27006E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        471
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2025   0.45169E-02   0.38847E+00 
c  VelocityY    0.29412E+04    2025   0.45169E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2025   0.45169E-02   0.00000E+00 
c  Pressure     0.41026E+00    7112   0.36145E-01   0.19353E+00 
c  k            0.21885E+04    1158   0.87560E-04   0.19207E+01 
c  omega        0.11959E+08     183   0.14143E-03   0.10013E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80065                             2
a  Local Time Step      1.1546e-05                         44419


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3166           2.826       0.0023344     -1.8561e-07
v  Velocity[Y]                 -15.813          32.055           6.914          20.057
v  Velocity[Z]                 -32.644          29.009        0.045003       -0.004286
v  ǁVelocityǁ                 0.017113          35.043          10.604          20.213
v  Pressure                    -434.38          346.46         -49.395          32.607
v  k                        4.6785e-08          69.218          3.9807          1.6675
v  omega                         1e-24      6.2605e+07          8440.2           11.87
v  turbulent_viscosity      4.5703e-15          1.3301         0.01574         0.10927
v  CourantNb                  0.030465          2786.2          44.779          1.3771
v  FourierNb                  0.010795           15851          93.316         0.67707
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14917        0.010813        0.045594


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15924           138.1          2.0542


 TIME FOR THE TIME STEP              300:        0.45588E+02

===============================================================


 INSTANT    0.301000000E+02   TIME STEP NUMBER             301
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.214860793E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31281E+02 0.15540E+02
   Friction velocity        uet   :  0.14792E-02 0.31571E+01
   Friction velocity        uk    :  0.18765E-01 0.29197E+01
   Dimensionless distance   yplus :  0.15901E+00 0.26971E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1077
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2070   0.44690E-02   0.38268E+00 
c  VelocityY    0.29413E+04    2070   0.44690E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2070   0.44690E-02   0.00000E+00 
c  Pressure     0.43778E+00    7069   0.36412E-01   0.20733E+00 
c  k            0.22089E+04    1086   0.85865E-04   0.19651E+01 
c  omega        0.20083E+08     164   0.65321E-04   0.11258E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039966                             2
a  omega               -1.7967e+05                             4
a  Local Time Step      1.0928e-05                         44503


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5567          2.2581       0.0011525      1.2179e-06
v  Velocity[Y]                 -22.931          30.031          6.9201          20.056
v  Velocity[Z]                 -33.411          28.798        0.072267      -0.0057665
v  ǁVelocityǁ                0.0047113           34.99          10.596          20.212
v  Pressure                    -436.59          347.11         -48.181          32.506
v  k                        1.6204e-08          61.209          4.0004          1.6705
v  omega                         1e-24      4.9146e+07          8730.2          11.918
v  turbulent_viscosity      9.1582e-14          1.3421        0.015774         0.10951
v  CourantNb                  0.020663            2813           44.82          1.3768
v  FourierNb                  0.010801           15813           92.93         0.67783
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14912        0.010813        0.045608


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15882          137.75          2.0546


 TIME FOR THE TIME STEP              301:        0.45473E+02

===============================================================


 INSTANT    0.302000000E+02   TIME STEP NUMBER             302
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.544900265E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30882E+02 0.13369E+02
   Friction velocity        uet   :  0.12772E-02 0.29558E+01
   Friction velocity        uk    :  0.16568E-01 0.28889E+01
   Dimensionless distance   yplus :  0.14385E+00 0.27001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2030   0.44105E-02   0.35445E+00 
c  VelocityY    0.29414E+04    2030   0.44105E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2030   0.44105E-02   0.00000E+00 
c  Pressure     0.41346E+00    6961   0.33082E-01   0.19567E+00 
c  k            0.22278E+04    1055   0.87108E-04   0.19839E+01 
c  omega        0.16190E+08     171   0.55765E-04   0.68809E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00015987                             1
a  omega               -1.5033e+05                             7
a  Local Time Step      1.1072e-05                         44565


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7631          1.5795     -0.00088283      1.0515e-06
v  Velocity[Y]                 -28.197          29.849          6.8454          20.056
v  Velocity[Z]                 -32.198           28.76        0.091324      -0.0074219
v  ǁVelocityǁ                 0.016138          32.868           10.56          20.213
v  Pressure                    -424.44          347.61         -48.001          32.419
v  k                        1.6049e-07          55.274          4.0454          1.6734
v  omega                         1e-24      2.5796e+07            8573          11.891
v  turbulent_viscosity      3.6742e-14          1.3568        0.015792         0.10977
v  CourantNb                   0.01012          2220.2           44.68          1.3767
v  FourierNb                  0.010807           15768          92.752         0.67873
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14923        0.010814        0.045606


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15835          137.43          2.0554


 TIME FOR THE TIME STEP              302:        0.48085E+02

===============================================================


 INSTANT    0.303000000E+02   TIME STEP NUMBER             303
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.143659964E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30556E+02 0.19728E+02
   Friction velocity        uet   :  0.18349E-02 0.27612E+01
   Friction velocity        uk    :  0.19613E-01 0.30917E+01
   Dimensionless distance   yplus :  0.16468E+00 0.27098E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1952   0.42829E-02   0.33583E+00 
c  VelocityY    0.29414E+04    1952   0.42829E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1952   0.42829E-02   0.00000E+00 
c  Pressure     0.41113E+00    7109   0.31363E-01   0.19403E+00 
c  k            0.22411E+04    1257   0.10248E-03   0.19042E+01 
c  omega        0.12213E+08     260   0.77211E-04   0.38922E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0984e+05                             4
a  Local Time Step      1.1313e-05                         44536


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9199          1.5996        -0.00319      3.2431e-06
v  Velocity[Y]                 -22.907          29.728           6.736          20.056
v  Velocity[Z]                  -29.97          28.496        0.084308      -0.0089313
v  ǁVelocityǁ                0.0038036          33.185          10.578          20.213
v  Pressure                    -405.15          347.26         -49.286          32.069
v  k                        1.6009e-08          87.031           4.149          1.6764
v  omega                         1e-24      9.4169e+07          8675.3          11.927
v  turbulent_viscosity      8.1938e-14          1.3682        0.015829         0.11005
v  CourantNb                  0.026001          2057.9          44.292          1.3764
v  FourierNb                  0.010813           15767          93.879         0.68039
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14761        0.010813        0.045627


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15832          138.17          2.0568


 TIME FOR THE TIME STEP              303:        0.46088E+02

===============================================================


 INSTANT    0.304000000E+02   TIME STEP NUMBER             304
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.669929608E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29576E+02 0.17594E+02
   Friction velocity        uet   :  0.43703E-02 0.25588E+01
   Friction velocity        uk    :  0.11575E-01 0.30040E+01
   Dimensionless distance   yplus :  0.81201E-01 0.29062E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1083
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1854   0.44342E-02   0.32969E+00 
c  VelocityY    0.29413E+04    1854   0.44342E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1854   0.44342E-02   0.00000E+00 
c  Pressure     0.40284E+00    6816   0.33380E-01   0.19030E+00 
c  k            0.22467E+04    1356   0.12000E-03   0.17559E+01 
c  omega        0.10580E+09     244   0.19328E-04   0.24155E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1893e+05                             1
a  Local Time Step      1.1271e-05                         44479


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0901          1.9175      -0.0059894      2.0072e-06
v  Velocity[Y]                 -36.091          30.347          6.6861          20.056
v  Velocity[Z]                 -28.647          28.427        0.088682        -0.01017
v  ǁVelocityǁ                 0.008912          36.676          10.607          20.213
v  Pressure                    -409.77          346.81         -51.615          32.133
v  k                        5.4142e-10           96.18          4.2632          1.6795
v  omega                         1e-24      6.6412e+07          8805.4           11.96
v  turbulent_viscosity      2.9389e-14          1.3764        0.015873         0.11035
v  CourantNb                  0.020734          2054.7          44.086          1.3764
v  FourierNb                  0.010819           15846           96.19         0.68256
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14827        0.010814        0.045641


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15908          140.28          2.0589


 TIME FOR THE TIME STEP              304:        0.44961E+02

===============================================================


 INSTANT    0.305000000E+02   TIME STEP NUMBER             305
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.361090112E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.42284E+02 0.13634E+02
   Friction velocity        uet   :  0.93621E-03 0.33181E+01
   Friction velocity        uk    :  0.15871E-01 0.37120E+01
   Dimensionless distance   yplus :  0.14388E+00 0.36879E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        424
   Nb of faces within the viscous sub-layer     :       1084
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1806   0.43634E-02   0.33007E+00 
c  VelocityY    0.29412E+04    1806   0.43634E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1806   0.43634E-02   0.00000E+00 
c  Pressure     0.40405E+00    6851   0.36122E-01   0.19067E+00 
c  k            0.22481E+04    1356   0.12519E-03   0.16386E+01 
c  omega        0.64400E+08     256   0.15066E-04   0.74825E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2086e+05                             1
a  Local Time Step       1.088e-05                         44498


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1851           2.305      -0.0090497      1.4357e-06
v  Velocity[Y]                 -26.965          30.621          6.6786          20.056
v  Velocity[Z]                 -28.674          28.515        0.098053       -0.011338
v  ǁVelocityǁ                 0.010596          33.692          10.626          20.214
v  Pressure                    -411.72           346.2         -54.648          32.183
v  k                         9.068e-12           44.44          4.3037          1.6826
v  omega                         1e-24      3.3184e+07          8501.1          11.909
v  turbulent_viscosity      1.0002e-15           1.384        0.015927         0.11067
v  CourantNb                  0.093345          2779.5          44.236          1.3766
v  FourierNb                  0.010822           15975          98.215          0.6848
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010814        0.045653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16039          142.45          2.0614


 TIME FOR THE TIME STEP              305:        0.43687E+02

===============================================================


 INSTANT    0.306000000E+02   TIME STEP NUMBER             306
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.902115367E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29827E+02 0.13900E+02
   Friction velocity        uet   :  0.53439E-03 0.28549E+01
   Friction velocity        uk    :  0.30453E-01 0.32184E+01
   Dimensionless distance   yplus :  0.14577E+00 0.27521E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1757   0.46002E-02   0.32872E+00 
c  VelocityY    0.29411E+04    1757   0.46002E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1757   0.46002E-02   0.00000E+00 
c  Pressure     0.43279E+00    7119   0.34510E-01   0.20274E+00 
c  k            0.22484E+04    1271   0.77693E-04   0.14649E+01 
c  omega        0.29125E+08     224   0.27658E-04   0.40722E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4514e+05                             2
a  Local Time Step      1.0612e-05                         44493


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1334          2.5901       -0.011518     -9.8211e-07
v  Velocity[Y]                 -17.705          32.485          6.6952          20.056
v  Velocity[Z]                   -28.6          28.462         0.10213       -0.012444
v  ǁVelocityǁ                 0.013655          33.579          10.615          20.214
v  Pressure                    -411.39          345.76         -56.857          32.169
v  k                        4.6828e-09          53.622          4.3379          1.6857
v  omega                         1e-24      1.6573e+07            8282          11.887
v  turbulent_viscosity      1.6991e-17          1.3885        0.015958           0.111
v  CourantNb                  0.034291            2940          44.322          1.3769
v  FourierNb                  0.010826           16136          98.958         0.68647
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010812        0.045651


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16205          143.28          2.0634


 TIME FOR THE TIME STEP              306:        0.43812E+02

===============================================================


 INSTANT    0.307000000E+02   TIME STEP NUMBER             307
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.367751729E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29922E+02 0.12832E+02
   Friction velocity        uet   :  0.42803E-02 0.29605E+01
   Friction velocity        uk    :  0.11437E-01 0.31461E+01
   Dimensionless distance   yplus :  0.10264E+00 0.27949E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        513
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1998   0.48211E-02   0.33363E+00 
c  VelocityY    0.29411E+04    1998   0.48211E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1998   0.48211E-02   0.00000E+00 
c  Pressure     0.43797E+00    7063   0.32154E-01   0.20564E+00 
c  k            0.22493E+04    1133   0.77978E-04   0.14534E+01 
c  omega        0.16984E+08     338   0.25835E-04   0.29442E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.0019e+05                             1
a  Local Time Step      1.1431e-05                         44472


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.981          2.8316       -0.012056     -1.5929e-06
v  Velocity[Y]                 -16.918          33.684          6.7243          20.056
v  Velocity[Z]                 -28.757          30.035        0.098336       -0.013283
v  ǁVelocityǁ                 0.010639          34.105           10.59          20.214
v  Pressure                    -409.07          345.39          -58.06          32.127
v  k                        5.3735e-09          51.889          4.3185          1.6887
v  omega                         1e-24      1.2904e+07          8113.7          11.863
v  turbulent_viscosity      1.8208e-15          1.3947        0.015969         0.11134
v  CourantNb                  0.056845          2098.7          44.168          1.3772
v  FourierNb                  0.010827           16301          100.33         0.68784
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010812        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16372           144.5           2.065


 TIME FOR THE TIME STEP              307:        0.45993E+02

===============================================================


 INSTANT    0.308000000E+02   TIME STEP NUMBER             308
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.196534805E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29994E+02 0.14581E+02
   Friction velocity        uet   :  0.31777E-02 0.29724E+01
   Friction velocity        uk    :  0.25570E-01 0.29861E+01
   Dimensionless distance   yplus :  0.61647E-01 0.31670E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1822   0.45008E-02   0.35011E+00 
c  VelocityY    0.29410E+04    1822   0.45008E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1822   0.45008E-02   0.00000E+00 
c  Pressure     0.47017E+00    7053   0.30700E-01   0.22251E+00 
c  k            0.22494E+04    1342   0.79709E-04   0.15234E+01 
c  omega        0.12621E+08     438   0.15741E-03   0.16469E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -11865                             1
a  Local Time Step      1.1484e-05                         44507


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7608           3.075       -0.010882     -1.1569e-06
v  Velocity[Y]                 -15.075          33.496          6.7404          20.058
v  Velocity[Z]                  -29.04          29.036        0.071296       -0.013856
v  ǁVelocityǁ                 0.013749          33.908          10.549          20.216
v  Pressure                    -398.37          344.52         -58.781          31.801
v  k                        1.6042e-08          51.956          4.2293          1.6918
v  omega                         1e-24      7.8965e+07          8479.8          11.879
v  turbulent_viscosity      2.9732e-14          1.3969        0.015951         0.11168
v  CourantNb                  0.074758          2095.5          43.992          1.3774
v  FourierNb                  0.010828           16377          101.17         0.68917
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1491        0.010811        0.045622


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99667           16450          145.16          2.0666


 TIME FOR THE TIME STEP              308:        0.44838E+02

===============================================================


 INSTANT    0.309000000E+02   TIME STEP NUMBER             309
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.228724887E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30310E+02 0.14715E+02
   Friction velocity        uet   :  0.64018E-03 0.28479E+01
   Friction velocity        uk    :  0.27382E-01 0.29712E+01
   Dimensionless distance   yplus :  0.82299E-01 0.35488E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :        948
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1884   0.43298E-02   0.35986E+00 
c  VelocityY    0.29408E+04    1884   0.43298E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1884   0.43298E-02   0.00000E+00 
c  Pressure     0.42186E+00    7045   0.30580E-01   0.19860E+00 
c  k            0.22485E+04    1485   0.71856E-04   0.14265E+01 
c  omega        0.32973E+08     255   0.29872E-04   0.49191E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1388e-05                         44523


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5223          3.2277      -0.0084681     -1.0214e-06
v  Velocity[Y]                 -16.143          33.697          6.7255          20.056
v  Velocity[Z]                 -28.641          28.965        0.018217       -0.014429
v  ǁVelocityǁ                 0.011708          34.019          10.522          20.215
v  Pressure                     -386.8          344.23         -58.654          31.106
v  k                        1.2368e-09          41.022           4.132          1.6949
v  omega                         1e-24      4.0258e+07          8224.9          11.857
v  turbulent_viscosity      1.0045e-14          1.3941        0.015897         0.11204
v  CourantNb                  0.062529          2080.1          43.866          1.3776
v  FourierNb                  0.010828           16370          100.67         0.68993
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14816         0.01081        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16446          144.53          2.0675


 TIME FOR THE TIME STEP              309:        0.45498E+02

===============================================================


 INSTANT    0.310000000E+02   TIME STEP NUMBER             310
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.873848157E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31239E+02 0.21055E+02
   Friction velocity        uet   :  0.27644E-03 0.27440E+01
   Friction velocity        uk    :  0.20772E-01 0.34281E+01
   Dimensionless distance   yplus :  0.97142E-01 0.32832E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :        955
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1936   0.45753E-02   0.37226E+00 
c  VelocityY    0.29406E+04    1936   0.45753E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1936   0.45753E-02   0.00000E+00 
c  Pressure     0.40130E+00    7009   0.28616E-01   0.18829E+00 
c  k            0.22488E+04    1531   0.69203E-04   0.14573E+01 
c  omega        0.13091E+08     237   0.47563E-04   0.18103E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0676e-05                         44543


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1755          3.1659      -0.0054983     -2.3556e-06
v  Velocity[Y]                 -16.662          30.674          6.7243          20.055
v  Velocity[Z]                 -29.932          28.913       -0.028811       -0.014561
v  ǁVelocityǁ                 0.017658          34.049          10.503          20.214
v  Pressure                    -369.01          345.44         -57.143          31.093
v  k                        4.7043e-11          41.597          4.0504          1.6982
v  omega                         1e-24      2.1661e+07          8011.2          11.828
v  turbulent_viscosity      1.5262e-15           1.394        0.015855         0.11239
v  CourantNb                  0.026715          2054.4          43.981          1.3779
v  FourierNb                  0.010829           16220          98.796         0.69049
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488        0.010808          0.0456


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16298          142.78          2.0683


 TIME FOR THE TIME STEP              310:        0.45618E+02

===============================================================


 INSTANT    0.311000000E+02   TIME STEP NUMBER             311
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.134726381E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31414E+02 0.20400E+02
   Friction velocity        uet   :  0.16916E-02 0.27640E+01
   Friction velocity        uk    :  0.19201E-01 0.32040E+01
   Dimensionless distance   yplus :  0.53155E-01 0.27200E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1911   0.45508E-02   0.37926E+00 
c  VelocityY    0.29405E+04    1911   0.45508E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1911   0.45508E-02   0.00000E+00 
c  Pressure     0.40561E+00    6719   0.27584E-01   0.18960E+00 
c  k            0.22508E+04    1493   0.67608E-04   0.15702E+01 
c  omega        0.10273E+08     248   0.35997E-04   0.34308E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1385e+05                             1
a  Local Time Step      1.1614e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5924          3.1887      -0.0026898     -3.0955e-06
v  Velocity[Y]                 -14.545          30.619          6.7512          20.056
v  Velocity[Z]                 -31.627          29.047       -0.077476        -0.01426
v  ǁVelocityǁ                 0.023136          37.014          10.499          20.214
v  Pressure                    -352.47          347.82         -54.669          31.471
v  k                        2.7571e-09          54.184          4.0243          1.7015
v  omega                         1e-24      2.3896e+07          7905.4          11.817
v  turbulent_viscosity      1.1821e-16          1.3914        0.015845         0.11274
v  CourantNb                  0.054005          2023.1          44.336          1.3779
v  FourierNb                  0.010829           15988          97.163         0.69153
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14801        0.010808        0.045581


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91733           16065           141.5          2.0695


 TIME FOR THE TIME STEP              311:        0.44138E+02

===============================================================


 INSTANT    0.312000000E+02   TIME STEP NUMBER             312
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.259080772E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30586E+02 0.16688E+02
   Friction velocity        uet   :  0.10463E-02 0.30970E+01
   Friction velocity        uk    :  0.22865E-01 0.29725E+01
   Dimensionless distance   yplus :  0.11260E+00 0.27108E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1847   0.44545E-02   0.38582E+00 
c  VelocityY    0.29404E+04    1847   0.44545E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1847   0.44545E-02   0.00000E+00 
c  Pressure     0.45969E+00    7095   0.30946E-01   0.21504E+00 
c  k            0.22567E+04    1419   0.73209E-04   0.17221E+01 
c  omega        0.11968E+08     198   0.39353E-04   0.47450E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7111e+05                             2
a  Local Time Step      1.1842e-05                         44544


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88257          2.9366     -0.00065322     -3.4741e-06
v  Velocity[Y]                  -15.09          33.615          6.7998          20.056
v  Velocity[Z]                 -32.953          28.746        -0.10686       -0.014149
v  ǁVelocityǁ                 0.014263          36.733          10.528          20.215
v  Pressure                    -407.41          349.94         -52.189          31.746
v  k                        2.0159e-08          66.255          4.0394          1.7049
v  omega                         1e-24      2.7594e+07          8091.7          11.836
v  turbulent_viscosity      1.2121e-14            1.39        0.015865         0.11309
v  CourantNb                  0.021528          2275.3          44.482          1.3777
v  FourierNb                  0.010829           15777          95.856         0.69279
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14724        0.010808        0.045579


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15853          140.34          2.0705


 TIME FOR THE TIME STEP              312:        0.43773E+02

===============================================================


 INSTANT    0.313000000E+02   TIME STEP NUMBER             313
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.168902894E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29998E+02 0.14099E+02
   Friction velocity        uet   :  0.14518E-02 0.33088E+01
   Friction velocity        uk    :  0.23108E-01 0.29556E+01
   Dimensionless distance   yplus :  0.17266E+00 0.26861E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1885   0.46724E-02   0.40075E+00 
c  VelocityY    0.29402E+04    1885   0.46724E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1885   0.46724E-02   0.00000E+00 
c  Pressure     0.44204E+00    7096   0.35685E-01   0.20643E+00 
c  k            0.22683E+04    1353   0.76426E-04   0.18136E+01 
c  omega        0.12110E+08     234   0.52284E-03   0.11448E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2379e+05                             3
a  Local Time Step      1.1072e-05                         44561


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.60793          2.8524      0.00085969     -4.9065e-06
v  Velocity[Y]                 -15.074          32.891          6.8523          20.056
v  Velocity[Z]                 -32.591          28.775       -0.096992        -0.01364
v  ǁVelocityǁ                 0.008478          35.161          10.572          20.215
v  Pressure                    -435.93          351.45         -50.238          32.106
v  k                          3.35e-07          70.754          4.0686          1.7081
v  omega                         1e-24      1.7921e+08           10559          12.015
v  turbulent_viscosity      5.0239e-15          1.3851        0.015899         0.11343
v  CourantNb                  0.057855          2775.1          44.483          1.3773
v  FourierNb                  0.010828           15592           94.69         0.69443
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14751        0.010808        0.045594


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81837           15662          139.17          2.0717


 TIME FOR THE TIME STEP              313:        0.46075E+02

===============================================================


 INSTANT    0.314000000E+02   TIME STEP NUMBER             314
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.376166604E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30793E+02 0.16118E+02
   Friction velocity        uet   :  0.26402E-03 0.32574E+01
   Friction velocity        uk    :  0.19020E-01 0.30276E+01
   Dimensionless distance   yplus :  0.10536E+00 0.27093E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1953   0.45166E-02   0.40861E+00 
c  VelocityY    0.29402E+04    1953   0.45166E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1953   0.45166E-02   0.00000E+00 
c  Pressure     0.45155E+00    7082   0.36380E-01   0.21147E+00 
c  k            0.22835E+04    1251   0.78592E-04   0.18535E+01 
c  omega        0.16524E+09      86   0.17853E-04   0.36823E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00034976                             1
a  omega               -2.0407e+05                             4
a  Local Time Step      1.1062e-05                         44575


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80214            2.97       0.0022439      -4.246e-06
v  Velocity[Y]                 -23.573           30.27          6.8698          20.056
v  Velocity[Z]                 -32.834           28.68        -0.06833       -0.012894
v  ǁVelocityǁ                0.0053893          34.515          10.586          20.215
v  Pressure                    -443.07          351.43         -49.863           31.98
v  k                        7.2706e-07          64.236          4.0837           1.711
v  omega                         1e-24      8.9859e+07          9658.9          11.988
v  turbulent_viscosity      3.7285e-14          1.3803        0.015928         0.11376
v  CourantNb                   0.04435          2853.6          44.516           1.377
v  FourierNb                  0.010826           15462           94.15         0.69612
v  total_pressure           1.0088e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14796        0.010809        0.045585


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15529          138.67          2.0731


 TIME FOR THE TIME STEP              314:        0.45438E+02

===============================================================


 INSTANT    0.315000000E+02   TIME STEP NUMBER             315
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.398977069E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30453E+02 0.14891E+02
   Friction velocity        uet   :  0.19296E-02 0.29389E+01
   Friction velocity        uk    :  0.25728E-01 0.32039E+01
   Dimensionless distance   yplus :  0.13525E+00 0.27166E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1847   0.44030E-02   0.39140E+00 
c  VelocityY    0.29401E+04    1847   0.44030E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1847   0.44030E-02   0.00000E+00 
c  Pressure     0.45062E+00    6882   0.31970E-01   0.21159E+00 
c  k            0.22968E+04    1036   0.77989E-04   0.18761E+01 
c  omega        0.44544E+08     130   0.42910E-04   0.15337E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00094384                             4
a  omega               -2.3969e+05                             8
a  Local Time Step      1.1448e-05                         44559


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0746          3.0082        0.003749     -4.5919e-06
v  Velocity[Y]                 -25.355          30.103          6.8162          20.056
v  Velocity[Z]                 -32.936          28.671       -0.031053       -0.011962
v  ǁVelocityǁ                0.0093484          33.527          10.576          20.215
v  Pressure                    -433.84          351.39          -50.16          31.818
v  k                        1.7492e-09          49.777          4.1083          1.7134
v  omega                         1e-24      4.5461e+07          9251.3           11.95
v  turbulent_viscosity      1.0024e-13          1.3777        0.015938         0.11408
v  CourantNb                  0.030522            2364          44.488          1.3769
v  FourierNb                  0.010824           15324          93.588         0.69776
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14802         0.01081         0.04561


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15389          138.08          2.0747


 TIME FOR THE TIME STEP              315:        0.44748E+02

===============================================================


 INSTANT    0.316000000E+02   TIME STEP NUMBER             316
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.342859879E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29424E+02 0.17327E+02
   Friction velocity        uet   :  0.14001E-02 0.28447E+01
   Friction velocity        uk    :  0.20642E-01 0.27442E+01
   Dimensionless distance   yplus :  0.19747E+00 0.27281E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        435
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1710   0.46124E-02   0.37332E+00 
c  VelocityY    0.29399E+04    1710   0.46124E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1710   0.46124E-02   0.00000E+00 
c  Pressure     0.42992E+00    7062   0.29552E-01   0.20210E+00 
c  k            0.23034E+04     933   0.91260E-04   0.18005E+01 
c  omega        0.13213E+13       3   0.11378E-08   0.62889E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1088e+05                             3
a  Local Time Step      1.1629e-05                         44574


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4178          3.0557       0.0044877      -3.784e-06
v  Velocity[Y]                   -32.6          29.997          6.7163          20.056
v  Velocity[Z]                 -28.634          28.331       -0.014224       -0.010638
v  ǁVelocityǁ                 0.014913          33.289          10.604          20.216
v  Pressure                    -413.03          350.25         -51.529          31.556
v  k                        2.5643e-09          84.192          4.1877          1.7153
v  omega                         1e-24       2.383e+07          8681.9          11.903
v  turbulent_viscosity      2.5435e-16          1.3711        0.015969         0.11438
v  CourantNb                  0.052516          2030.5           44.26          1.3768
v  FourierNb                  0.010823           15235           94.53         0.70034
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14746         0.01081        0.045632


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.71051           15300          138.79          2.0772


 TIME FOR THE TIME STEP              316:        0.41546E+02

===============================================================


 INSTANT    0.317000000E+02   TIME STEP NUMBER             317
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.419159019E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28451E+02 0.21979E+02
   Friction velocity        uet   :  0.11648E-02 0.27191E+01
   Friction velocity        uk    :  0.13810E-01 0.30604E+01
   Dimensionless distance   yplus :  0.12436E+00 0.31909E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :       1001
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1861   0.46170E-02   0.37473E+00 
c  VelocityY    0.29398E+04    1861   0.46170E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1861   0.46170E-02   0.00000E+00 
c  Pressure     0.42458E+00    7030   0.32596E-01   0.19975E+00 
c  k            0.22995E+04    1222   0.11773E-03   0.17666E+01 
c  omega        0.12660E+08     491   0.41568E-04   0.23132E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00039039                             1
a  omega               -1.4151e+05                             2
a  Local Time Step      1.1652e-05                         44553


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6135          3.3304       0.0041641     -3.4994e-06
v  Velocity[Y]                 -36.422           30.18          6.6653          20.056
v  Velocity[Z]                 -28.599          28.283          0.0213      -0.0092806
v  ǁVelocityǁ                 0.013791          39.172          10.649          20.216
v  Pressure                    -417.01          348.51         -53.974          31.604
v  k                        4.5614e-10          107.72          4.3176          1.7168
v  omega                         1e-24      1.4094e+07            8380          11.893
v  turbulent_viscosity       2.356e-16          1.3625        0.015995         0.11464
v  CourantNb                  0.039687          2054.3          44.132          1.3769
v  FourierNb                  0.010822           15295          96.178          0.7034
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1473         0.01081        0.045612


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15361          140.31          2.0803


 TIME FOR THE TIME STEP              317:        0.44749E+02

===============================================================


 INSTANT    0.318000000E+02   TIME STEP NUMBER             318
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.126894898E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52648E+02 0.13823E+02
   Friction velocity        uet   :  0.73438E-03 0.34183E+01
   Friction velocity        uk    :  0.20299E-01 0.50469E+01
   Dimensionless distance   yplus :  0.12535E+00 0.41150E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1943   0.47718E-02   0.38397E+00 
c  VelocityY    0.29398E+04    1943   0.47718E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1943   0.47718E-02   0.00000E+00 
c  Pressure     0.43184E+00    7126   0.36067E-01   0.20235E+00 
c  k            0.22875E+04    1089   0.11828E-03   0.14924E+01 
c  omega        0.10677E+08     440   0.31476E-04   0.14629E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6804e+05                             3
a  Local Time Step      1.1448e-05                         44477


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6202          3.5713       0.0026556     -4.2062e-06
v  Velocity[Y]                 -29.392          30.606          6.6742          20.056
v  Velocity[Z]                  -28.59          28.225        0.059833       -0.007836
v  ǁVelocityǁ                 0.012989          33.675          10.675          20.217
v  Pressure                    -417.77          346.63         -56.877          31.671
v  k                        4.5607e-10          59.144          4.3129           1.718
v  omega                         1e-24      1.1753e+07          8252.8          11.881
v  turbulent_viscosity      6.4309e-16          1.3537        0.016028         0.11491
v  CourantNb                 0.0068924          2148.3          44.182          1.3773
v  FourierNb                  0.010822           15269          97.451          0.7062
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14781        0.010809        0.045597


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15336          141.63          2.0835


 TIME FOR THE TIME STEP              318:        0.45673E+02

===============================================================


 INSTANT    0.319000000E+02   TIME STEP NUMBER             319
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.350587963E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29806E+02 0.13661E+02
   Friction velocity        uet   :  0.16872E-02 0.29067E+01
   Friction velocity        uk    :  0.17086E-01 0.31405E+01
   Dimensionless distance   yplus :  0.13669E+00 0.27033E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1915   0.46437E-02   0.38516E+00 
c  VelocityY    0.29398E+04    1915   0.46437E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1915   0.46437E-02   0.00000E+00 
c  Pressure     0.42126E+00    7122   0.35469E-01   0.19752E+00 
c  k            0.22738E+04    1050   0.83329E-04   0.13371E+01 
c  omega        0.10260E+08     345   0.32692E-04   0.88041E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -69685                             1
a  Local Time Step      1.0391e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0366          3.6769      0.00096386     -3.4516e-06
v  Velocity[Y]                 -17.776          30.863          6.7069          20.057
v  Velocity[Z]                  -28.77          28.532         0.09024      -0.0060699
v  ǁVelocityǁ                0.0092602           33.58          10.671          20.218
v  Pressure                    -416.55          345.46         -58.864          31.706
v  k                        2.3204e-09           50.03          4.3017          1.7186
v  omega                         1e-24      1.1683e+07          8054.2           11.85
v  turbulent_viscosity      5.6109e-16          1.3447        0.016048         0.11515
v  CourantNb                  0.047554          3033.6           44.49          1.3777
v  FourierNb                  0.010821           15306          98.551         0.70873
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1478        0.010809        0.045584


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15373          143.04          2.0864


 TIME FOR THE TIME STEP              319:        0.44351E+02

===============================================================


 INSTANT    0.320000000E+02   TIME STEP NUMBER             320
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.429698226E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30434E+02 0.13556E+02
   Friction velocity        uet   :  0.15193E-02 0.28771E+01
   Friction velocity        uk    :  0.15597E-01 0.32303E+01
   Dimensionless distance   yplus :  0.15290E+00 0.27957E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :        951
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    1968   0.46566E-02   0.39780E+00 
c  VelocityY    0.29396E+04    1968   0.46566E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    1968   0.46566E-02   0.00000E+00 
c  Pressure     0.44810E+00    6984   0.32404E-01   0.21040E+00 
c  k            0.22599E+04    1055   0.78012E-04   0.12573E+01 
c  omega        0.10189E+08     362   0.21071E-03   0.13013E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9753e+05                             2
a  Local Time Step       1.157e-05                         44437


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8277          3.5999      0.00034172      -3.068e-06
v  Velocity[Y]                 -17.182          32.971          6.7461          20.057
v  Velocity[Z]                 -28.585          28.891        0.098627      -0.0043837
v  ǁVelocityǁ                 0.011312          34.007          10.637          20.218
v  Pressure                    -413.36          345.11         -59.203          31.688
v  k                        3.9471e-08          53.325          4.2666          1.7188
v  omega                         1e-24       9.377e+07          8319.9          11.846
v  turbulent_viscosity       2.604e-15          1.3347        0.016042         0.11537
v  CourantNb                  0.037865          2110.9          44.497           1.378
v  FourierNb                  0.010821           15342          99.853         0.71108
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14796        0.010809        0.045619


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15410          144.35          2.0891


 TIME FOR THE TIME STEP              320:        0.45695E+02

===============================================================


 INSTANT    0.321000000E+02   TIME STEP NUMBER             321
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.578588784E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30664E+02 0.13841E+02
   Friction velocity        uet   :  0.33639E-03 0.29383E+01
   Friction velocity        uk    :  0.17807E-01 0.28593E+01
   Dimensionless distance   yplus :  0.93075E-01 0.31197E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        483
   Nb of faces within the viscous sub-layer     :        938
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    1871   0.44669E-02   0.42026E+00 
c  VelocityY    0.29395E+04    1871   0.44669E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    1871   0.44669E-02   0.00000E+00 
c  Pressure     0.45184E+00    7058   0.30216E-01   0.21396E+00 
c  k            0.22461E+04    1100   0.75101E-04   0.13399E+01 
c  omega        0.36061E+08     344   0.80754E-04   0.50504E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -3.312e+05                             2
a  Local Time Step      1.1597e-05                         44449


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0198           3.346      0.00084622     -4.8873e-06
v  Velocity[Y]                 -15.564          33.675          6.7748          20.057
v  Velocity[Z]                 -29.084          28.785         0.07928      -0.0025758
v  ǁVelocityǁ                 0.017584          33.888          10.592          20.217
v  Pressure                    -404.99          345.03         -58.971          31.372
v  k                        2.1288e-07          54.833          4.1591          1.7184
v  omega                         1e-24      1.5279e+08          8566.9          11.873
v  turbulent_viscosity      3.6248e-14          1.3244        0.016001         0.11555
v  CourantNb                 0.0089059          2115.1          44.378          1.3782
v  FourierNb                  0.010821           15358          100.93         0.71282
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14809         0.01081        0.045593


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15427          145.31          2.0911


 TIME FOR THE TIME STEP              321:        0.44305E+02

===============================================================


 INSTANT    0.322000000E+02   TIME STEP NUMBER             322
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.367096138E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31263E+02 0.14637E+02
   Friction velocity        uet   :  0.11256E-02 0.28690E+01
   Friction velocity        uk    :  0.18206E-01 0.29785E+01
   Dimensionless distance   yplus :  0.11979E+00 0.34083E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :        875
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1849   0.46077E-02   0.43888E+00 
c  VelocityY    0.29392E+04    1849   0.46077E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1849   0.46077E-02   0.00000E+00 
c  Pressure     0.44243E+00    7043   0.30262E-01   0.20978E+00 
c  k            0.22306E+04    1015   0.69212E-04   0.12554E+01 
c  omega        0.14025E+09     147   0.12623E-04   0.16077E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.154e-05                         44476


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2645          2.9015       0.0013341     -5.3284e-06
v  Velocity[Y]                 -15.049          33.699          6.7626          20.057
v  Velocity[Z]                 -28.483          29.278         0.03054     -0.00096136
v  ǁVelocityǁ                 0.015915          34.059          10.563          20.217
v  Pressure                    -389.59          345.49         -58.077          30.948
v  k                        6.6026e-07          41.878          4.0506          1.7176
v  omega                         1e-24      7.6381e+07          8360.8          11.833
v  turbulent_viscosity      3.1011e-14          1.3146        0.015918          0.1157
v  CourantNb                  0.052112          2104.8          44.337          1.3785
v  FourierNb                  0.010822           15338           99.27         0.71365
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14861        0.010812         0.04562


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15408          143.61          2.0922


 TIME FOR THE TIME STEP              322:        0.43362E+02

===============================================================


 INSTANT    0.323000000E+02   TIME STEP NUMBER             323
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.238219149E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31513E+02 0.22587E+02
   Friction velocity        uet   :  0.10420E-02 0.27066E+01
   Friction velocity        uk    :  0.22464E-01 0.34589E+01
   Dimensionless distance   yplus :  0.13498E+00 0.38510E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :        909
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1800   0.44418E-02   0.45157E+00 
c  VelocityY    0.29389E+04    1800   0.44418E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1800   0.44418E-02   0.00000E+00 
c  Pressure     0.41990E+00    6735   0.28202E-01   0.19883E+00 
c  k            0.22158E+04    1166   0.65268E-04   0.12592E+01 
c  omega        0.37732E+08     183   0.23058E-04   0.52090E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1375e+05                             1
a  Local Time Step      1.1428e-05                         44494


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5272           2.292        0.001897     -5.1929e-06
v  Velocity[Y]                 -15.134          30.773          6.7507          20.057
v  Velocity[Z]                 -28.622          29.057      -0.0081761      0.00023273
v  ǁVelocityǁ                 0.013584          33.625          10.541          20.217
v  Pressure                    -373.59          347.12         -56.197          30.895
v  k                        3.2817e-07           38.04          3.9778          1.7165
v  omega                         1e-24      3.8166e+07            8284          11.846
v  turbulent_viscosity      6.8296e-14          1.3043         0.01584         0.11581
v  CourantNb                  0.024055          2082.9          44.403          1.3789
v  FourierNb                  0.010824           15284          96.553         0.71405
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010814        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15354          140.96          2.0929


 TIME FOR THE TIME STEP              323:        0.42758E+02

===============================================================


 INSTANT    0.324000000E+02   TIME STEP NUMBER             324
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.153179622E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31816E+02 0.21128E+02
   Friction velocity        uet   :  0.51604E-03 0.26189E+01
   Friction velocity        uk    :  0.28357E-01 0.31953E+01
   Dimensionless distance   yplus :  0.99600E-01 0.30175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1888   0.45531E-02   0.46108E+00 
c  VelocityY    0.29386E+04    1888   0.45531E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1888   0.45531E-02   0.00000E+00 
c  Pressure     0.41573E+00    7070   0.27373E-01   0.19638E+00 
c  k            0.22029E+04    1274   0.63698E-04   0.13690E+01 
c  omega        0.13727E+08     220   0.22508E-03   0.45198E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1634e+05                             4
a  Local Time Step      1.2105e-05                         44498


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7569           1.574       0.0021372     -2.7654e-06
v  Velocity[Y]                 -15.072          30.584          6.7625          20.057
v  Velocity[Z]                 -31.581           29.21       -0.048527       0.0016364
v  ǁVelocityǁ                   0.0183          36.973          10.532          20.217
v  Pressure                    -354.95          350.07          -52.98          31.224
v  k                        9.4907e-08          49.423          3.9518          1.7151
v  omega                         1e-24      3.3082e+08          9365.8          12.003
v  turbulent_viscosity       1.437e-13          1.2939        0.015797         0.11589
v  CourantNb                  0.017394          2056.1          44.805           1.379
v  FourierNb                  0.010827           15250          95.158         0.71469
v  total_pressure           1.0097e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14868        0.010816        0.045641


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15319          139.96          2.0937


 TIME FOR THE TIME STEP              324:        0.45857E+02

===============================================================


 INSTANT    0.325000000E+02   TIME STEP NUMBER             325
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.311769700E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29865E+02 0.18937E+02
   Friction velocity        uet   :  0.20655E-02 0.30385E+01
   Friction velocity        uk    :  0.24353E-01 0.30438E+01
   Dimensionless distance   yplus :  0.15704E+00 0.27498E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1866   0.45724E-02   0.46518E+00 
c  VelocityY    0.29384E+04    1866   0.45724E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1866   0.45724E-02   0.00000E+00 
c  Pressure     0.41389E+00    7048   0.31243E-01   0.19450E+00 
c  k            0.21933E+04    1224   0.69086E-04   0.15306E+01 
c  omega        0.12950E+10      73   0.19950E-05   0.12928E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00049143                             1
a  omega                    -71807                             3
a  Local Time Step      1.1958e-05                         44497


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9522          1.7325       0.0021465       -4.01e-06
v  Velocity[Y]                 -15.124           32.92          6.7938          20.057
v  Velocity[Z]                 -32.018          29.042       -0.075885       0.0032226
v  ǁVelocityǁ                0.0057249          37.285          10.561          20.217
v  Pressure                    -402.27          352.34         -50.135          31.648
v  k                        1.1479e-08          61.741           3.966          1.7135
v  omega                         1e-24      1.6541e+08            9316          11.976
v  turbulent_viscosity      9.5707e-15          1.2836        0.015794         0.11592
v  CourantNb                  0.043099          2046.5           44.96          1.3788
v  FourierNb                  0.010831           15354          93.619         0.71502
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010817        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15422          138.58          2.0938


 TIME FOR THE TIME STEP              325:        0.44821E+02

===============================================================


 INSTANT    0.326000000E+02   TIME STEP NUMBER             326
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.710412727E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29634E+02 0.14185E+02
   Friction velocity        uet   :  0.20670E-02 0.31857E+01
   Friction velocity        uk    :  0.24388E-01 0.32057E+01
   Dimensionless distance   yplus :  0.11169E+00 0.27451E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1813   0.46671E-02   0.47725E+00 
c  VelocityY    0.29381E+04    1813   0.46671E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1813   0.46671E-02   0.00000E+00 
c  Pressure     0.44840E+00    6988   0.36608E-01   0.21158E+00 
c  k            0.21901E+04    1054   0.73313E-04   0.16512E+01 
c  omega        0.32644E+09      64   0.35527E-05   0.35590E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00043346                             2
a  omega               -6.9152e+05                             7
a  Local Time Step       1.169e-05                         44561


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -3.151          2.1046       0.0020793     -3.2469e-06
v  Velocity[Y]                 -15.002          33.904          6.8325          20.056
v  Velocity[Z]                  -32.89          28.932       -0.072972       0.0041628
v  ǁVelocityǁ                 0.013663          35.221          10.599          20.216
v  Pressure                    -435.83          353.26         -47.931          31.851
v  k                         4.957e-08          68.643          3.9995          1.7114
v  omega                         1e-24        8.27e+07          8670.8          11.924
v  turbulent_viscosity      6.0085e-15          1.2736        0.015815         0.11592
v  CourantNb                  0.024724          2696.3          44.886          1.3782
v  FourierNb                  0.010835           15457          92.548         0.71506
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14936        0.010818        0.045665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15524          137.43          2.0933


 TIME FOR THE TIME STEP              326:        0.42770E+02

===============================================================


 INSTANT    0.327000000E+02   TIME STEP NUMBER             327
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.207948040E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31187E+02 0.14766E+02
   Friction velocity        uet   :  0.29696E-02 0.33069E+01
   Friction velocity        uk    :  0.14699E-01 0.30996E+01
   Dimensionless distance   yplus :  0.12543E+00 0.27448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1054
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    1840   0.45354E-02   0.48401E+00 
c  VelocityY    0.29379E+04    1840   0.45354E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    1840   0.45354E-02   0.00000E+00 
c  Pressure     0.43767E+00    7018   0.38244E-01   0.20652E+00 
c  k            0.21924E+04    1262   0.75575E-04   0.17061E+01 
c  omega        0.82991E+08     110   0.30951E-04   0.29330E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0012856                             2
a  omega                    -63070                             2
a  Local Time Step      1.1146e-05                         44589


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2081          2.4346       0.0017021     -2.6703e-06
v  Velocity[Y]                 -21.334          30.353          6.8535          20.057
v  Velocity[Z]                 -32.552          28.752       -0.038484       0.0050101
v  ǁVelocityǁ                  0.01223          34.097          10.616          20.216
v  Pressure                    -445.78          352.69         -47.256          31.956
v  k                        1.0669e-07          64.385          4.0239          1.7088
v  omega                         1e-24      6.9196e+07          8976.6          11.947
v  turbulent_viscosity      5.6037e-14           1.264        0.015858         0.11587
v  CourantNb                   0.02382          2872.8          44.731          1.3777
v  FourierNb                   0.01084           15449          92.661         0.71528
v  total_pressure           1.0088e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947         0.01082        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0107           15514          137.39           2.093


 TIME FOR THE TIME STEP              327:        0.44148E+02

===============================================================


 INSTANT    0.328000000E+02   TIME STEP NUMBER             328
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.310779317E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30387E+02 0.15183E+02
   Friction velocity        uet   :  0.83401E-03 0.29227E+01
   Friction velocity        uk    :  0.26173E-01 0.30815E+01
   Dimensionless distance   yplus :  0.16613E+00 0.27221E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        528
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    1762   0.44965E-02   0.45102E+00 
c  VelocityY    0.29377E+04    1762   0.44965E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    1762   0.44965E-02   0.00000E+00 
c  Pressure     0.44695E+00    7021   0.34447E-01   0.21019E+00 
c  k            0.21953E+04    1382   0.77415E-04   0.17541E+01 
c  omega        0.38664E+08     136   0.34693E-04   0.10417E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011226                             1
a  omega                -1.859e+05                             4
a  Local Time Step      1.1434e-05                         44605


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1179          2.7234      0.00087673     -8.6779e-07
v  Velocity[Y]                 -24.737          30.194          6.8059          20.057
v  Velocity[Z]                 -32.966           28.47       0.0077878       0.0055029
v  ǁVelocityǁ                0.0063259          33.516          10.589          20.216
v  Pressure                    -436.65          351.66         -47.399          31.941
v  k                        6.6548e-07          93.834          4.0469          1.7057
v  omega                         1e-24       3.537e+07          8794.4          11.931
v  turbulent_viscosity      8.7564e-14          1.2547        0.015899         0.11578
v  CourantNb                  0.027873          2517.8          44.656          1.3774
v  FourierNb                  0.010842           15280          93.287         0.71535
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14852         0.01082        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15348          137.94          2.0928


 TIME FOR THE TIME STEP              328:        0.43813E+02

===============================================================


 INSTANT    0.329000000E+02   TIME STEP NUMBER             329
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.327226364E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30265E+02 0.15005E+02
   Friction velocity        uet   :  0.92796E-03 0.28499E+01
   Friction velocity        uk    :  0.16469E-01 0.30083E+01
   Dimensionless distance   yplus :  0.14216E+00 0.27102E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1753   0.45606E-02   0.41907E+00 
c  VelocityY    0.29376E+04    1753   0.45606E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1753   0.45606E-02   0.00000E+00 
c  Pressure     0.42796E+00    7090   0.30798E-01   0.20208E+00 
c  k            0.21943E+04    1405   0.90478E-04   0.17208E+01 
c  omega        0.15890E+08     244   0.46123E-04   0.44940E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74260                             1
a  Local Time Step      1.1246e-05                         44600


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9214          3.0066     -0.00010644      1.5683e-07
v  Velocity[Y]                 -34.632          30.054          6.6993          20.056
v  Velocity[Z]                 -29.215          28.324        0.036837       0.0056873
v  ǁVelocityǁ                 0.010618          34.834          10.594          20.216
v  Pressure                    -413.38          349.64         -48.603          31.739
v  k                        2.7484e-07          115.64          4.0986           1.702
v  omega                         1e-24      1.9183e+07          8502.2          11.931
v  turbulent_viscosity      9.6273e-14          1.2456        0.015931         0.11565
v  CourantNb                  0.031328          2060.1           44.32           1.377
v  FourierNb                  0.010839           15059          94.425         0.71522
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14875         0.01082         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15130          138.75          2.0923


 TIME FOR THE TIME STEP              329:        0.44082E+02

===============================================================


 INSTANT    0.330000000E+02   TIME STEP NUMBER             330
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.462422814E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29091E+02 0.23828E+02
   Friction velocity        uet   :  0.12532E-02 0.30510E+01
   Friction velocity        uk    :  0.27859E-01 0.31524E+01
   Dimensionless distance   yplus :  0.21557E+00 0.27527E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    1820   0.46525E-02   0.40460E+00 
c  VelocityY    0.29375E+04    1820   0.46525E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    1820   0.46525E-02   0.00000E+00 
c  Pressure     0.43951E+00    7031   0.32817E-01   0.20614E+00 
c  k            0.21859E+04    1343   0.11846E-03   0.15856E+01 
c  omega        0.11415E+08     413   0.44066E-04   0.63488E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4364e+05                             1
a  Local Time Step      1.1273e-05                         44577


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.704           3.257      -0.0010691      2.0657e-06
v  Velocity[Y]                  -33.14          30.067          6.6216          20.056
v  Velocity[Z]                 -28.662          28.146        0.068115       0.0059322
v  ǁVelocityǁ                0.0092373          39.705          10.623          20.215
v  Pressure                    -412.01          346.97         -50.824            31.7
v  k                        2.2648e-09          120.79          4.1796           1.698
v  omega                         1e-24      2.6188e+07          8524.8          11.958
v  turbulent_viscosity      4.9515e-14          1.2368        0.015936         0.11548
v  CourantNb                  0.039929          2058.7          44.135          1.3767
v  FourierNb                  0.010836           14856          95.235         0.71495
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010821        0.045638


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14930          139.37          2.0917


 TIME FOR THE TIME STEP              330:        0.45925E+02

===============================================================


 INSTANT    0.331000000E+02   TIME STEP NUMBER             331
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.156796386E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57689E+02 0.13479E+02
   Friction velocity        uet   :  0.20831E-02 0.34360E+01
   Friction velocity        uk    :  0.15738E-01 0.44010E+01
   Dimensionless distance   yplus :  0.13901E+00 0.35824E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        488
   Nb of faces within the viscous sub-layer     :       1049
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    1879   0.45570E-02   0.39566E+00 
c  VelocityY    0.29377E+04    1879   0.45570E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    1879   0.45570E-02   0.00000E+00 
c  Pressure     0.41727E+00    7143   0.37639E-01   0.19646E+00 
c  k            0.21725E+04    1282   0.12581E-03   0.14392E+01 
c  omega        0.13377E+08     501   0.33170E-04   0.23809E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0425e-05                         44546


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5418           3.356      -0.0022182      1.3696e-07
v  Velocity[Y]                 -31.763          30.384          6.6131          20.057
v  Velocity[Z]                  -28.67          28.448         0.10327       0.0057075
v  ǁVelocityǁ                 0.017345          33.581          10.644          20.216
v  Pressure                    -413.88           344.6         -53.663          31.888
v  k                        1.9127e-08          102.26           4.208          1.6936
v  omega                         1e-24      1.3089e+07          8258.5           11.91
v  turbulent_viscosity      3.0764e-14          1.2283        0.015931         0.11527
v  CourantNb                  0.024263          2049.7          44.122          1.3767
v  FourierNb                  0.010834           14766          96.043         0.71438
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010819        0.045573


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14840          140.17          2.0911


 TIME FOR THE TIME STEP              331:        0.46205E+02

===============================================================


 INSTANT    0.332000000E+02   TIME STEP NUMBER             332
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.202143553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30994E+02 0.13721E+02
   Friction velocity        uet   :  0.31385E-02 0.31027E+01
   Friction velocity        uk    :  0.19491E-01 0.35383E+01
   Dimensionless distance   yplus :  0.85599E-01 0.40656E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1892   0.45793E-02   0.38438E+00 
c  VelocityY    0.29376E+04    1892   0.45793E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1892   0.45793E-02   0.00000E+00 
c  Pressure     0.41521E+00    6868   0.38382E-01   0.19679E+00 
c  k            0.21584E+04    1117   0.87991E-04   0.12921E+01 
c  omega        0.10486E+08     385   0.28364E-04   0.11846E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4849e+05                             1
a  Local Time Step      1.1364e-05                         44522


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2287           3.254      -0.0036875     -1.9772e-07
v  Velocity[Y]                 -17.803           30.68          6.6384          20.057
v  Velocity[Z]                 -28.836          28.784         0.12314       0.0051376
v  ǁVelocityǁ                 0.005572          33.428          10.632          20.216
v  Pressure                    -414.32          343.39         -55.753          32.007
v  k                        1.4059e-10          67.591          4.2056           1.689
v  omega                         1e-24      1.1689e+07          7990.5          11.868
v  turbulent_viscosity      1.5193e-14            1.22         0.01592         0.11503
v  CourantNb                  0.032938          3077.4          44.413          1.3768
v  FourierNb                   0.01083           14726          96.497         0.71347
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010818         0.04561


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14797          140.91          2.0902


 TIME FOR THE TIME STEP              332:        0.44357E+02

===============================================================


 INSTANT    0.333000000E+02   TIME STEP NUMBER             333
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.819257546E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31881E+02 0.13789E+02
   Friction velocity        uet   :  0.59809E-03 0.28243E+01
   Friction velocity        uk    :  0.27261E-01 0.34752E+01
   Dimensionless distance   yplus :  0.12027E+00 0.39930E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        473
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    2071   0.46061E-02   0.37926E+00 
c  VelocityY    0.29375E+04    2071   0.46061E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    2071   0.46061E-02   0.00000E+00 
c  Pressure     0.44491E+00    7005   0.34466E-01   0.21057E+00 
c  k            0.21458E+04    1039   0.83833E-04   0.11961E+01 
c  omega        0.10271E+08     384   0.46325E-04   0.18416E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5763e+05                             1
a  Local Time Step       1.132e-05                         44494


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6814          3.1447      -0.0049033     -2.6582e-06
v  Velocity[Y]                 -17.454          32.709          6.6847          20.057
v  Velocity[Z]                 -28.616           29.03         0.11887       0.0041058
v  ǁVelocityǁ                 0.018489          33.969          10.596          20.216
v  Pressure                    -413.05          343.37         -56.535          32.041
v  k                        5.7227e-09          64.577          4.1904          1.6841
v  omega                         1e-24      1.6803e+07          7903.9          11.836
v  turbulent_viscosity      2.2397e-16          1.2121        0.015893         0.11476
v  CourantNb                  0.047544            2336          44.363          1.3769
v  FourierNb                  0.010827           14662          97.091         0.71217
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14831        0.010819        0.045652


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14731          141.45           2.089


 TIME FOR THE TIME STEP              333:        0.46134E+02

===============================================================


 INSTANT    0.334000000E+02   TIME STEP NUMBER             334
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.499996402E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32118E+02 0.14128E+02
   Friction velocity        uet   :  0.13130E-02 0.29374E+01
   Friction velocity        uk    :  0.19979E-01 0.32585E+01
   Dimensionless distance   yplus :  0.12722E+00 0.35463E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        442
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29374E+04    1871   0.44813E-02   0.37553E+00 
c  VelocityY    0.29374E+04    1871   0.44813E-02   0.00000E+00 
c  VelocityZ    0.29374E+04    1871   0.44813E-02   0.00000E+00 
c  Pressure     0.45008E+00    6954   0.31682E-01   0.21322E+00 
c  k            0.21343E+04    1271   0.83035E-04   0.12852E+01 
c  omega        0.10494E+08     486   0.26759E-03   0.23632E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9162e+05                             2
a  Local Time Step      1.1507e-05                         44471


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97091          2.7667      -0.0054929     -2.7628e-06
v  Velocity[Y]                 -15.597          33.381          6.7291          20.056
v  Velocity[Z]                 -28.493          29.235        0.098178       0.0029939
v  ǁVelocityǁ                 0.016574          33.832          10.536          20.216
v  Pressure                    -405.62          343.91         -56.331          32.054
v  k                        3.6429e-09           53.73          4.1148           1.679
v  omega                         1e-24      5.8194e+07          8793.2          11.888
v  turbulent_viscosity      1.1069e-14          1.2229        0.015853         0.11446
v  CourantNb                  0.041877          1997.6           44.29           1.377
v  FourierNb                  0.010824           14645          97.729         0.71083
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14813         0.01082        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14711          142.02          2.0878


 TIME FOR THE TIME STEP              334:        0.44316E+02

===============================================================


 INSTANT    0.335000000E+02   TIME STEP NUMBER             335
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.208130554E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31068E+02 0.14083E+02
   Friction velocity        uet   :  0.26477E-02 0.28751E+01
   Friction velocity        uk    :  0.89873E-02 0.29404E+01
   Dimensionless distance   yplus :  0.62665E-01 0.33376E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        371
   Nb of faces within the viscous sub-layer     :        946
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    1742   0.45398E-02   0.37869E+00 
c  VelocityY    0.29372E+04    1742   0.45398E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    1742   0.45398E-02   0.00000E+00 
c  Pressure     0.45387E+00    7043   0.30507E-01   0.21453E+00 
c  k            0.21216E+04    1346   0.78817E-04   0.12059E+01 
c  omega        0.30236E+08     275   0.65584E-04   0.11974E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6364e+05                             1
a  Local Time Step      1.1222e-05                         44449


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5124          2.8724      -0.0053209     -1.2156e-07
v  Velocity[Y]                 -15.198          33.725          6.7216          20.057
v  Velocity[Z]                 -28.413          29.215        0.057377       0.0018991
v  ǁVelocityǁ                 0.019699          34.119          10.495          20.216
v  Pressure                    -388.01          344.31         -55.952          31.637
v  k                        3.8489e-08           45.86          4.0384          1.6739
v  omega                         1e-24      6.3785e+07          8493.5          11.853
v  turbulent_viscosity      1.7499e-14          1.2365         0.01579         0.11414
v  CourantNb                  0.024165          1981.2          44.207          1.3771
v  FourierNb                  0.010821           14626          96.861         0.70893
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14754         0.01082        0.045757


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14685          141.07           2.086


 TIME FOR THE TIME STEP              335:        0.43923E+02

===============================================================


 INSTANT    0.336000000E+02   TIME STEP NUMBER             336
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.569311027E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31665E+02 0.23127E+02
   Friction velocity        uet   :  0.16700E-02 0.27422E+01
   Friction velocity        uk    :  0.52104E-02 0.32504E+01
   Dimensionless distance   yplus :  0.47313E-01 0.36475E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29371E+04    1823   0.42584E-02   0.37730E+00 
c  VelocityY    0.29371E+04    1823   0.42584E-02   0.00000E+00 
c  VelocityZ    0.29371E+04    1823   0.42584E-02   0.00000E+00 
c  Pressure     0.43262E+00    6722   0.27944E-01   0.20516E+00 
c  k            0.21111E+04    1404   0.68380E-04   0.11568E+01 
c  omega        0.20408E+08     235   0.27026E-03   0.97977E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6497e+05                             2
a  Local Time Step      1.1918e-05                         44439


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9485          2.9673      -0.0042711      5.2622e-06
v  Velocity[Y]                 -15.067          32.101          6.7045          20.055
v  Velocity[Z]                 -28.497          29.236        0.020776      0.00069487
v  ǁVelocityǁ                 0.017822          32.925          10.469          20.214
v  Pressure                    -373.73          345.38         -54.982          31.374
v  k                        7.5906e-07          45.716          3.9961          1.6691
v  omega                         1e-24      2.2456e+08          9609.1          11.944
v  turbulent_viscosity      1.7747e-13          1.2492        0.015743          0.1138
v  CourantNb                  0.010523            1987          44.072          1.3772
v  FourierNb                  0.010818           14690          95.733         0.70683
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869         0.01082        0.045784


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14753          139.81           2.084


 TIME FOR THE TIME STEP              336:        0.43790E+02

===============================================================


 INSTANT    0.337000000E+02   TIME STEP NUMBER             337
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.497937899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31315E+02 0.21574E+02
   Friction velocity        uet   :  0.18239E-02 0.25905E+01
   Friction velocity        uk    :  0.22014E-01 0.30206E+01
   Dimensionless distance   yplus :  0.69439E-01 0.28279E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29371E+04    1913   0.45204E-02   0.37835E+00 
c  VelocityY    0.29371E+04    1913   0.45204E-02   0.00000E+00 
c  VelocityZ    0.29371E+04    1913   0.45204E-02   0.00000E+00 
c  Pressure     0.43290E+00    7039   0.25783E-01   0.20388E+00 
c  k            0.21035E+04    1434   0.68275E-04   0.12418E+01 
c  omega        0.20473E+09      82   0.10659E-04   0.25829E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.624e+05                             2
a  Local Time Step      1.1805e-05                         44453


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2558           3.003      -0.0030762      4.7644e-06
v  Velocity[Y]                 -15.084          30.444          6.7143          20.055
v  Velocity[Z]                 -30.482            29.1       -0.016669      -0.0010834
v  ǁVelocityǁ                 0.010953          36.607          10.472          20.214
v  Pressure                    -363.58          347.86         -52.785          31.564
v  k                        3.1931e-07          46.972          3.9771          1.6645
v  omega                         1e-24      1.1253e+08          8801.7          11.913
v  turbulent_viscosity      7.2201e-14          1.2643        0.015733         0.11345
v  CourantNb                   0.03064          2000.5          44.285          1.3773
v  FourierNb                  0.010816           14866          94.933         0.70509
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14786         0.01082        0.045762


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14928          139.22          2.0824


 TIME FOR THE TIME STEP              337:        0.45063E+02

===============================================================


 INSTANT    0.338000000E+02   TIME STEP NUMBER             338
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.574996008E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30721E+02 0.19965E+02
   Friction velocity        uet   :  0.93775E-03 0.29776E+01
   Friction velocity        uk    :  0.23218E-01 0.28922E+01
   Dimensionless distance   yplus :  0.16234E+00 0.27154E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        470
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29373E+04    1933   0.44767E-02   0.37064E+00 
c  VelocityY    0.29373E+04    1933   0.44767E-02   0.00000E+00 
c  VelocityZ    0.29373E+04    1933   0.44767E-02   0.00000E+00 
c  Pressure     0.40928E+00    6987   0.29000E-01   0.19384E+00 
c  k            0.21004E+04    1409   0.70905E-04   0.13763E+01 
c  omega        0.52807E+08     182   0.20878E-04   0.86833E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -98901                             4
a  Local Time Step      1.1585e-05                         44463


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4929          2.9485      -0.0023578      3.6746e-06
v  Velocity[Y]                 -14.986          30.414          6.7475          20.055
v  Velocity[Z]                 -31.594          28.775        -0.05217      -0.0025019
v  ǁVelocityǁ                 0.013232          36.818          10.512          20.214
v  Pressure                    -390.69          349.34         -50.831           31.85
v  k                        1.2166e-07          59.633          3.9953          1.6602
v  omega                         1e-24      5.6792e+07          8475.8          11.891
v  turbulent_viscosity      3.7947e-14          1.2772         0.01577         0.11308
v  CourantNb                  0.032019          2029.3          44.471          1.3772
v  FourierNb                  0.010813           15112          93.789         0.70361
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14769        0.010819         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15176          138.26          2.0808


 TIME FOR THE TIME STEP              338:        0.45157E+02

===============================================================


 INSTANT    0.339000000E+02   TIME STEP NUMBER             339
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.806495803E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29585E+02 0.13560E+02
   Friction velocity        uet   :  0.80987E-03 0.31181E+01
   Friction velocity        uk    :  0.13970E-01 0.29804E+01
   Dimensionless distance   yplus :  0.15321E+00 0.27230E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29374E+04    1970   0.46239E-02   0.36851E+00 
c  VelocityY    0.29374E+04    1970   0.46239E-02   0.00000E+00 
c  VelocityZ    0.29374E+04    1970   0.46239E-02   0.00000E+00 
c  Pressure     0.42426E+00    7004   0.33396E-01   0.19936E+00 
c  k            0.21048E+04    1177   0.74784E-04   0.14966E+01 
c  omega        0.17186E+08     246   0.36399E-04   0.35704E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8401e+05                             1
a  Local Time Step      1.1405e-05                         44412


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6785          3.0524      -0.0021481      2.0833e-06
v  Velocity[Y]                 -15.112          31.185           6.805          20.056
v  Velocity[Z]                 -32.847           28.68       -0.053931      -0.0039584
v  ǁVelocityǁ                 0.012857          35.525          10.587          20.215
v  Pressure                    -431.13           349.3         -49.506          32.081
v  k                        6.2047e-09           67.67          4.0347          1.6563
v  omega                         1e-24       2.946e+07          8199.8          11.856
v  turbulent_viscosity      1.2267e-14          1.2868        0.015812         0.11272
v  CourantNb                  0.014866          2444.1          44.477           1.377
v  FourierNb                  0.010812           15271          93.039         0.70202
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010819          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15336          137.52           2.079


 TIME FOR THE TIME STEP              339:        0.45173E+02

===============================================================


 INSTANT    0.340000000E+02   TIME STEP NUMBER             340
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.335872883E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30229E+02 0.14108E+02
   Friction velocity        uet   :  0.26217E-04 0.31281E+01
   Friction velocity        uk    :  0.18771E-01 0.30364E+01
   Dimensionless distance   yplus :  0.13692E+00 0.27074E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :       1075
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    2002   0.45348E-02   0.37324E+00 
c  VelocityY    0.29376E+04    2002   0.45348E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    2002   0.45348E-02   0.00000E+00 
c  Pressure     0.44266E+00    6812   0.36776E-01   0.21077E+00 
c  k            0.21165E+04    1057   0.77175E-04   0.15573E+01 
c  omega        0.11134E+08     225   0.34529E-03   0.41335E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62225                             1
a  Local Time Step      1.1089e-05                         44257


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.736          3.2834      -0.0016826      1.5514e-06
v  Velocity[Y]                 -21.232          30.162          6.8563          20.056
v  Velocity[Z]                  -31.83           28.44       -0.019576      -0.0052129
v  ǁVelocityǁ                  0.01117          33.596          10.649          20.215
v  Pressure                    -446.68          347.45         -49.349          32.069
v  k                         6.093e-09          66.016          4.0777          1.6528
v  omega                         1e-24      7.4919e+07          9548.3          11.942
v  turbulent_viscosity      5.9827e-15          1.2957        0.015862         0.11235
v  CourantNb                  0.032402          2747.9          44.481          1.3767
v  FourierNb                  0.010811           15317          92.823         0.70013
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14843         0.01082        0.045659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90995           15383           137.3          2.0768


 TIME FOR THE TIME STEP              340:        0.44953E+02

===============================================================


 INSTANT    0.341000000E+02   TIME STEP NUMBER             341
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.647757598E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29981E+02 0.13302E+02
   Friction velocity        uet   :  0.48017E-03 0.28847E+01
   Friction velocity        uk    :  0.16813E-01 0.31745E+01
   Dimensionless distance   yplus :  0.79949E-01 0.27007E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    2003   0.44130E-02   0.35092E+00 
c  VelocityY    0.29375E+04    2003   0.44130E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    2003   0.44130E-02   0.00000E+00 
c  Pressure     0.44035E+00    7014   0.36589E-01   0.20891E+00 
c  k            0.21306E+04    1263   0.79349E-04   0.16246E+01 
c  omega        0.45176E+08     234   0.59585E-04   0.12633E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2354e+05                             2
a  Local Time Step       1.167e-05                         44180


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7678          3.3865     -0.00072082     -2.5888e-06
v  Velocity[Y]                 -23.528          29.982          6.8531          20.056
v  Velocity[Z]                 -32.172          28.346        0.038743      -0.0063538
v  ǁVelocityǁ                 0.012872          33.484          10.652          20.215
v  Pressure                    -440.85          345.32         -49.932          31.989
v  k                        5.4443e-09          54.779          4.1031          1.6495
v  omega                         1e-24      3.8112e+07          8958.7          11.935
v  turbulent_viscosity      5.5076e-15          1.3047         0.01591         0.11199
v  CourantNb                    0.0336          2528.5          44.528          1.3767
v  FourierNb                  0.010811           15296          94.026         0.69849
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010821        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15368          138.55          2.0752


 TIME FOR THE TIME STEP              341:        0.45291E+02

===============================================================


 INSTANT    0.342000000E+02   TIME STEP NUMBER             342
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.113139283E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29825E+02 0.14512E+02
   Friction velocity        uet   :  0.77678E-03 0.28457E+01
   Friction velocity        uk    :  0.25497E-01 0.28172E+01
   Dimensionless distance   yplus :  0.11512E+00 0.26672E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29374E+04    1994   0.45133E-02   0.31237E+00 
c  VelocityY    0.29374E+04    1994   0.45133E-02   0.00000E+00 
c  VelocityZ    0.29374E+04    1994   0.45133E-02   0.00000E+00 
c  Pressure     0.43094E+00    7077   0.32725E-01   0.20300E+00 
c  k            0.21422E+04    1217   0.83577E-04   0.16440E+01 
c  omega        0.15926E+08     181   0.73815E-04   0.59444E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -64715                             1
a  Local Time Step      1.1414e-05                         44178


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2802          3.3031     -0.00014872     -5.6637e-06
v  Velocity[Y]                 -34.019            29.8          6.7713          20.056
v  Velocity[Z]                 -30.591          28.237        0.083559      -0.0073313
v  ǁVelocityǁ                0.0076622          34.097          10.636          20.216
v  Pressure                    -420.39           343.1         -50.973          31.884
v  k                         6.943e-09          67.658           4.133          1.6464
v  omega                         1e-24      2.3354e+07          8613.3          11.899
v  turbulent_viscosity      4.2478e-15          1.3126        0.015935         0.11164
v  CourantNb                  0.068652            2093          44.395          1.3767
v  FourierNb                  0.010812           15237          93.983         0.69645
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010822         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15310          138.38          2.0731


 TIME FOR THE TIME STEP              342:        0.45095E+02

===============================================================


 INSTANT    0.343000000E+02   TIME STEP NUMBER             343
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.802744903E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30301E+02 0.23514E+02
   Friction velocity        uet   :  0.28634E-02 0.30410E+01
   Friction velocity        uk    :  0.18434E-01 0.28928E+01
   Dimensionless distance   yplus :  0.58661E-01 0.26504E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29374E+04    1976   0.46562E-02   0.29039E+00 
c  VelocityY    0.29374E+04    1976   0.46562E-02   0.00000E+00 
c  VelocityZ    0.29374E+04    1976   0.46562E-02   0.00000E+00 
c  Pressure     0.45011E+00    7049   0.30262E-01   0.21180E+00 
c  k            0.21468E+04    1079   0.10609E-03   0.15243E+01 
c  omega        0.11392E+08     347   0.50047E-04   0.24231E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.501e+05                             1
a  Local Time Step      1.1212e-05                         44216


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -3.112          3.0255      0.00035115     -5.0239e-06
v  Velocity[Y]                   -24.3          29.882          6.6853          20.056
v  Velocity[Z]                 -28.558          28.421         0.11722      -0.0083695
v  ǁVelocityǁ                 0.005501          33.386          10.639          20.216
v  Pressure                    -408.16          340.95         -52.755          31.667
v  k                        7.6779e-08          95.476          4.1987          1.6438
v  omega                         1e-24      1.4427e+07          8237.7          11.879
v  turbulent_viscosity      3.1234e-14          1.3181        0.015942          0.1113
v  CourantNb                   0.05116          2091.9          44.252          1.3766
v  FourierNb                  0.010813           15208          94.743         0.69459
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947         0.01082        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15279             139          2.0712


 TIME FOR THE TIME STEP              343:        0.45752E+02

===============================================================


 INSTANT    0.344000000E+02   TIME STEP NUMBER             344
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.248620581E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43726E+02 0.15437E+02
   Friction velocity        uet   :  0.69377E-03 0.29244E+01
   Friction velocity        uk    :  0.18073E-01 0.40762E+01
   Dimensionless distance   yplus :  0.14020E+00 0.32592E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        435
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29373E+04    1976   0.46968E-02   0.28253E+00 
c  VelocityY    0.29373E+04    1976   0.46968E-02   0.00000E+00 
c  VelocityZ    0.29373E+04    1976   0.46968E-02   0.00000E+00 
c  Pressure     0.44041E+00    7105   0.33913E-01   0.20710E+00 
c  k            0.21457E+04    1201   0.11455E-03   0.13659E+01 
c  omega        0.10332E+08     491   0.59563E-04   0.34044E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3405e+05                             1
a  Local Time Step      1.0877e-05                         44271


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7346          2.5523       0.0010575     -5.0551e-06
v  Velocity[Y]                  -36.32          30.053          6.6594          20.056
v  Velocity[Z]                 -28.424          28.497         0.14645      -0.0091139
v  ǁVelocityǁ                 0.013048          36.995          10.627          20.216
v  Pressure                    -410.84          340.22         -54.587          31.819
v  k                        5.7442e-10          77.851          4.2189          1.6416
v  omega                         1e-24      2.0362e+07          8136.5          11.868
v  turbulent_viscosity      2.6778e-14          1.3201        0.015946         0.11097
v  CourantNb                  0.016781          2080.4          44.284          1.3767
v  FourierNb                  0.010814           15255           96.77         0.69336
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010819        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15324          141.05            2.07


 TIME FOR THE TIME STEP              344:        0.46929E+02

===============================================================


 INSTANT    0.345000000E+02   TIME STEP NUMBER             345
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.852225987E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37618E+02 0.14534E+02
   Friction velocity        uet   :  0.15554E-02 0.34486E+01
   Friction velocity        uk    :  0.26139E-01 0.34130E+01
   Dimensionless distance   yplus :  0.10774E+00 0.32203E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29373E+04    2024   0.44264E-02   0.27948E+00 
c  VelocityY    0.29373E+04    2024   0.44264E-02   0.00000E+00 
c  VelocityZ    0.29373E+04    2024   0.44264E-02   0.00000E+00 
c  Pressure     0.43950E+00    7112   0.37684E-01   0.20698E+00 
c  k            0.21432E+04    1424   0.96505E-04   0.12663E+01 
c  omega        0.15576E+08     340   0.19725E-04   0.13226E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.1088e+05                             1
a  Local Time Step      1.1063e-05                         44259


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7978          1.9184       0.0018893     -4.9405e-06
v  Velocity[Y]                 -19.913          30.776          6.6699          20.057
v  Velocity[Z]                 -28.393          28.857         0.15308      -0.0091114
v  ǁVelocityǁ                 0.015886          33.588          10.596          20.217
v  Pressure                    -412.15          340.67          -56.19          32.089
v  k                        3.4764e-09          44.186          4.1867          1.6399
v  omega                         1e-24      1.1707e+07            7931          11.845
v  turbulent_viscosity      2.6314e-16          1.3224         0.01593         0.11066
v  CourantNb                  0.029966          3107.8          44.654          1.3769
v  FourierNb                  0.010817           15331          96.594          0.6915
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010819        0.045764


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15396          141.25          2.0684


 TIME FOR THE TIME STEP              345:        0.47999E+02

===============================================================


 INSTANT    0.346000000E+02   TIME STEP NUMBER             346
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.502215554E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31250E+02 0.13635E+02
   Friction velocity        uet   :  0.72997E-03 0.27383E+01
   Friction velocity        uk    :  0.18097E-01 0.29654E+01
   Dimensionless distance   yplus :  0.87143E-01 0.26478E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        430
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29372E+04    2062   0.47151E-02   0.28034E+00 
c  VelocityY    0.29372E+04    2062   0.47151E-02   0.00000E+00 
c  VelocityZ    0.29372E+04    2062   0.47151E-02   0.00000E+00 
c  Pressure     0.43234E+00    7034   0.36233E-01   0.20396E+00 
c  k            0.21415E+04    1545   0.71871E-04   0.11242E+01 
c  omega        0.11456E+08     250   0.39169E-04   0.29391E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0914e-05                         44230


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9473           2.009       0.0022538     -3.1501e-06
v  Velocity[Y]                 -17.419          32.303          6.6988          20.056
v  Velocity[Z]                 -28.354          28.886         0.12887      -0.0093575
v  ǁVelocityǁ                  0.01505          33.951          10.548          20.216
v  Pressure                    -412.39          342.05         -56.704          32.213
v  k                        7.7065e-09          49.949          4.1802          1.6386
v  omega                         1e-24      1.6419e+07          8006.2          11.852
v  turbulent_viscosity      1.6749e-15          1.3257        0.015889         0.11037
v  CourantNb                  0.025227          2489.9          44.609          1.3769
v  FourierNb                  0.010819           15452          95.525         0.68911
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14899        0.010819        0.045774


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15515          140.13           2.066


 TIME FOR THE TIME STEP              346:        0.48555E+02

===============================================================


 INSTANT    0.347000000E+02   TIME STEP NUMBER             347
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.416203701E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31328E+02 0.13391E+02
   Friction velocity        uet   :  0.65143E-03 0.29220E+01
   Friction velocity        uk    :  0.23260E-01 0.32229E+01
   Dimensionless distance   yplus :  0.57691E-01 0.27640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29373E+04    2051   0.45297E-02   0.29414E+00 
c  VelocityY    0.29373E+04    2051   0.45297E-02   0.00000E+00 
c  VelocityZ    0.29373E+04    2051   0.45297E-02   0.00000E+00 
c  Pressure     0.47395E+00    7053   0.34695E-01   0.22449E+00 
c  k            0.21416E+04    1571   0.74986E-04   0.11657E+01 
c  omega        0.10836E+08     349   0.38174E-03   0.56898E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5409e+05                             1
a  Local Time Step      1.1021e-05                         44219


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1411          2.3506       0.0021389     -3.2479e-06
v  Velocity[Y]                 -16.395           33.46          6.7323          20.056
v  Velocity[Z]                 -28.351          29.297        0.080389       -0.009393
v  ǁVelocityǁ                 0.017858          33.672          10.511          20.216
v  Pressure                    -409.88          343.93         -56.375          32.157
v  k                        1.1895e-08          53.115          4.1586          1.6377
v  omega                         1e-24      1.3538e+08          9147.3          11.929
v  turbulent_viscosity      3.0034e-15          1.3267        0.015875         0.11011
v  CourantNb                  0.044017          2027.2          44.289          1.3768
v  FourierNb                  0.010821           15700          95.652         0.68738
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010818        0.045784


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15761          139.94          2.0642


 TIME FOR THE TIME STEP              347:        0.47061E+02

===============================================================


 INSTANT    0.348000000E+02   TIME STEP NUMBER             348
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.502762362E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31372E+02 0.15834E+02
   Friction velocity        uet   :  0.17507E-03 0.29142E+01
   Friction velocity        uk    :  0.20650E-01 0.31819E+01
   Dimensionless distance   yplus :  0.14563E+00 0.32210E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29373E+04    2099   0.45990E-02   0.31501E+00 
c  VelocityY    0.29373E+04    2099   0.45990E-02   0.00000E+00 
c  VelocityZ    0.29373E+04    2099   0.45990E-02   0.00000E+00 
c  Pressure     0.47736E+00    7006   0.31466E-01   0.22548E+00 
c  k            0.21420E+04    1533   0.76567E-04   0.11977E+01 
c  omega        0.11454E+09     194   0.16877E-03   0.99850E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1458e-05                         44243


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.3411          2.6739       0.0017462     -1.5733e-06
v  Velocity[Y]                 -16.072           33.25          6.7524          20.056
v  Velocity[Z]                 -28.412          29.291        0.017998      -0.0091263
v  ǁVelocityǁ                 0.021117          33.683          10.484          20.216
v  Pressure                    -396.51          344.62         -56.508          31.583
v  k                        3.2749e-07          44.434          4.1063          1.6373
v  omega                         1e-24      7.3466e+08           13516          12.337
v  turbulent_viscosity       3.579e-14          1.3261        0.015864         0.10987
v  CourantNb                  0.067555            2063          44.055          1.3766
v  FourierNb                  0.010823           15895          96.527         0.68634
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14798        0.010817        0.045769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15953          140.58           2.063


 TIME FOR THE TIME STEP              348:        0.47202E+02

===============================================================


 INSTANT    0.349000000E+02   TIME STEP NUMBER             349
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.701185620E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28741E+02 0.21958E+02
   Friction velocity        uet   :  0.13039E-02 0.27471E+01
   Friction velocity        uk    :  0.22492E-01 0.31866E+01
   Dimensionless distance   yplus :  0.14406E+00 0.40051E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :        956
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29375E+04    2155   0.45273E-02   0.31892E+00 
c  VelocityY    0.29375E+04    2155   0.45273E-02   0.00000E+00 
c  VelocityZ    0.29375E+04    2155   0.45273E-02   0.00000E+00 
c  Pressure     0.45638E+00    6999   0.29459E-01   0.21554E+00 
c  k            0.21422E+04    1422   0.69110E-04   0.11474E+01 
c  omega        0.21594E+10     121   0.29139E-05   0.25310E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1611e-05                         44267


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.4152          2.9525       0.0013166     -7.5456e-07
v  Velocity[Y]                 -15.786          32.075          6.7355          20.056
v  Velocity[Z]                 -28.355           29.32       -0.038238      -0.0084939
v  ǁVelocityǁ                 0.011104          33.196           10.46          20.216
v  Pressure                    -378.32          345.56         -56.046          31.311
v  k                        5.7433e-07          37.783          4.0534          1.6372
v  omega                         1e-24      3.6738e+08           10918          12.104
v  turbulent_viscosity      2.5962e-13           1.325        0.015834         0.10965
v  CourantNb                  0.047765          2087.2          44.078          1.3767
v  FourierNb                  0.010824           16148          96.176         0.68481
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010817        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16208          140.25          2.0616


 TIME FOR THE TIME STEP              349:        0.47242E+02

===============================================================


 INSTANT    0.350000000E+02   TIME STEP NUMBER             350
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.813193319E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28317E+02 0.20991E+02
   Friction velocity        uet   :  0.26118E-02 0.25990E+01
   Friction velocity        uk    :  0.31617E-01 0.31674E+01
   Dimensionless distance   yplus :  0.99549E-01 0.29672E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        524
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    2139   0.43711E-02   0.32949E+00 
c  VelocityY    0.29376E+04    2139   0.43711E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    2139   0.43711E-02   0.00000E+00 
c  Pressure     0.41494E+00    7001   0.26479E-01   0.19513E+00 
c  k            0.21428E+04    1104   0.66987E-04   0.11717E+01 
c  omega        0.54012E+09      56   0.56794E-05   0.64690E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.112e-05                         44264


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.3732          3.0301      0.00099279     -2.8033e-06
v  Velocity[Y]                 -14.943          30.612          6.7341          20.056
v  Velocity[Z]                  -30.34          28.842       -0.081177      -0.0078726
v  ǁVelocityǁ                 0.019006          35.621          10.442          20.215
v  Pressure                    -362.62          346.69         -54.612          31.307
v  k                        3.0954e-08          43.064          4.0272          1.6377
v  omega                         1e-24      1.8382e+08          9489.5          11.967
v  turbulent_viscosity      6.4004e-14          1.3201        0.015811         0.10947
v  CourantNb                  0.037958          2105.4          44.155          1.3769
v  FourierNb                  0.010826           16365          95.191          0.6835
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010818        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16432          139.35          2.0604


 TIME FOR THE TIME STEP              350:        0.46906E+02

===============================================================


 INSTANT    0.351000000E+02   TIME STEP NUMBER             351
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.753930461E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29681E+02 0.20024E+02
   Friction velocity        uet   :  0.27346E-02 0.29340E+01
   Friction velocity        uk    :  0.31127E-01 0.29917E+01
   Dimensionless distance   yplus :  0.17872E+00 0.27645E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        563
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2169   0.44945E-02   0.33208E+00 
c  VelocityY    0.29378E+04    2169   0.44945E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2169   0.44945E-02   0.00000E+00 
c  Pressure     0.42716E+00    6970   0.27941E-01   0.20140E+00 
c  k            0.21445E+04    1437   0.68212E-04   0.12789E+01 
c  omega        0.13580E+09      97   0.11765E-04   0.17772E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.114e-05                         44226


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2328          3.2687      0.00073345      1.0923e-06
v  Velocity[Y]                 -15.114          31.236          6.7561          20.056
v  Velocity[Z]                 -32.426          28.841        -0.12505      -0.0068364
v  ǁVelocityǁ                 0.018162          37.009          10.449          20.215
v  Pressure                    -372.02          347.49         -52.919          31.502
v  k                         1.636e-07          54.707          4.0393          1.6385
v  omega                         1e-24      9.2214e+07          8731.4          11.887
v  turbulent_viscosity      1.7025e-14           1.315        0.015818         0.10932
v  CourantNb                  0.033052          2111.8          44.276           1.377
v  FourierNb                  0.010829           16467          94.353         0.68291
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14758        0.010817        0.045666


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16541          138.63          2.0599


 TIME FOR THE TIME STEP              351:        0.48046E+02

===============================================================


 INSTANT    0.352000000E+02   TIME STEP NUMBER             352
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.745916735E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29850E+02 0.16374E+02
   Friction velocity        uet   :  0.11128E-02 0.31421E+01
   Friction velocity        uk    :  0.14609E-01 0.31207E+01
   Dimensionless distance   yplus :  0.11776E+00 0.27354E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        516
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2151   0.44038E-02   0.33852E+00 
c  VelocityY    0.29380E+04    2151   0.44038E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2151   0.44038E-02   0.00000E+00 
c  Pressure     0.43471E+00    7017   0.32176E-01   0.20507E+00 
c  k            0.21496E+04    1618   0.75430E-04   0.14108E+01 
c  omega        0.35972E+08     155   0.26248E-04   0.50892E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5153e+05                             1
a  Local Time Step      1.1212e-05                         44183


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1703          3.4821      0.00047441      3.3407e-06
v  Velocity[Y]                 -14.949          32.929          6.7923          20.056
v  Velocity[Z]                 -33.823            28.5        -0.13945      -0.0056119
v  ǁVelocityǁ                 0.013046          36.414          10.499          20.216
v  Pressure                    -427.52          347.12         -51.694          31.575
v  k                        6.3425e-09          65.038          4.0634          1.6397
v  omega                         1e-24      4.6747e+07          8308.5          11.845
v  turbulent_viscosity      3.0262e-14          1.3119        0.015837         0.10919
v  CourantNb                  0.037958          2358.3          44.136          1.3766
v  FourierNb                  0.010831           16359           93.38         0.68203
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14725        0.010817        0.045639


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16437          137.52          2.0587


 TIME FOR THE TIME STEP              352:        0.48293E+02

===============================================================


 INSTANT    0.353000000E+02   TIME STEP NUMBER             353
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.259448483E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29683E+02 0.13720E+02
   Friction velocity        uet   :  0.58586E-03 0.32257E+01
   Friction velocity        uk    :  0.17222E-01 0.30260E+01
   Dimensionless distance   yplus :  0.15097E+00 0.27034E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2118   0.44303E-02   0.34732E+00 
c  VelocityY    0.29384E+04    2118   0.44303E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2118   0.44303E-02   0.00000E+00 
c  Pressure     0.41754E+00    7012   0.35667E-01   0.19844E+00 
c  k            0.21595E+04    1696   0.76739E-04   0.14753E+01 
c  omega        0.59137E+10      33   0.50182E-06   0.20230E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0932e-05                         44153


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1106          3.5128      0.00019092      2.6133e-06
v  Velocity[Y]                 -16.105          30.796          6.8312          20.057
v  Velocity[Z]                 -33.323          28.383         -0.1061      -0.0046471
v  ǁVelocityǁ                0.0096571           35.28          10.559          20.216
v  Pressure                    -451.98          345.76         -51.184          31.658
v  k                        9.5009e-09          67.216          4.0849          1.6411
v  omega                         1e-24       7.279e+07          8773.5          11.882
v  turbulent_viscosity      6.2483e-16          1.3074        0.015869          0.1091
v  CourantNb                  0.033099          2776.6          44.069          1.3763
v  FourierNb                  0.010833           16146           93.14         0.68183
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14824        0.010816        0.045592


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           0.979           16226          137.21          2.0582


 TIME FOR THE TIME STEP              353:        0.48327E+02

===============================================================


 INSTANT    0.354000000E+02   TIME STEP NUMBER             354
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271520382E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28839E+02 0.13723E+02
   Friction velocity        uet   :  0.24756E-02 0.30548E+01
   Friction velocity        uk    :  0.71909E-02 0.30007E+01
   Dimensionless distance   yplus :  0.58904E-01 0.26504E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        466
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2074   0.44881E-02   0.33802E+00 
c  VelocityY    0.29385E+04    2074   0.44881E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2074   0.44881E-02   0.00000E+00 
c  Pressure     0.40876E+00    7002   0.35348E-01   0.19368E+00 
c  k            0.21709E+04    1704   0.78120E-04   0.15039E+01 
c  omega        0.32298E+08     175   0.35670E-04   0.69698E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1609e-05                         44196


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8301          3.4591        2.17e-05      1.9344e-06
v  Velocity[Y]                 -24.359          30.113          6.8353          20.057
v  Velocity[Z]                 -31.334          28.431       -0.048912      -0.0031246
v  ǁVelocityǁ                 0.015476          32.633          10.581          20.216
v  Pressure                     -453.7          343.89         -51.489          31.667
v  k                        3.5455e-08          58.702            4.09          1.6426
v  omega                         1e-24      3.7105e+07          8536.2          11.892
v  turbulent_viscosity      2.3372e-15          1.2999        0.015904         0.10904
v  CourantNb                   0.04233          2726.8          44.124          1.3762
v  FourierNb                  0.010835           15570          93.681         0.68239
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869        0.010817        0.045601


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87534           15651          137.81          2.0586


 TIME FOR THE TIME STEP              354:        0.47906E+02

===============================================================


 INSTANT    0.355000000E+02   TIME STEP NUMBER             355
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.698557005E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31210E+02 0.13595E+02
   Friction velocity        uet   :  0.70469E-03 0.27562E+01
   Friction velocity        uk    :  0.20873E-01 0.29382E+01
   Dimensionless distance   yplus :  0.15579E+00 0.26237E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    2048   0.45881E-02   0.31258E+00 
c  VelocityY    0.29387E+04    2048   0.45881E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    2048   0.45881E-02   0.00000E+00 
c  Pressure     0.43402E+00    6968   0.32859E-01   0.20479E+00 
c  k            0.21796E+04    1595   0.80736E-04   0.15200E+01 
c  omega        0.13657E+08     211   0.87365E-04   0.77933E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1033e-05                         44244


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3189          3.5642      -0.0001153      7.5239e-07
v  Velocity[Y]                  -29.04          29.966          6.7763          20.057
v  Velocity[Z]                 -31.889          28.413        0.013203      -0.0017457
v  ǁVelocityǁ                 0.020064          33.081           10.58          20.216
v  Pressure                    -437.58          342.87         -52.291           31.53
v  k                        7.3238e-08          57.255          4.1047           1.644
v  omega                         1e-24      3.7936e+07          8700.3          11.921
v  turbulent_viscosity      2.8136e-15          1.2963        0.015914           0.109
v  CourantNb                 0.0078079          2166.2          44.161          1.3763
v  FourierNb                  0.010838           15075          93.181         0.68262
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14771        0.010818         0.04558


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15154          137.34          2.0589


 TIME FOR THE TIME STEP              355:        0.47019E+02

===============================================================


 INSTANT    0.356000000E+02   TIME STEP NUMBER             356
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.451644850E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30878E+02 0.20427E+02
   Friction velocity        uet   :  0.22644E-02 0.27808E+01
   Friction velocity        uk    :  0.65253E-02 0.32349E+01
   Dimensionless distance   yplus :  0.95635E-01 0.25701E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1982   0.45522E-02   0.29540E+00 
c  VelocityY    0.29386E+04    1982   0.45522E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1982   0.45522E-02   0.00000E+00 
c  Pressure     0.44129E+00    6992   0.30457E-01   0.20766E+00 
c  k            0.21819E+04    1377   0.10247E-03   0.14342E+01 
c  omega        0.12802E+08     278   0.71421E-04   0.43250E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8163e+05                             1
a  Local Time Step      1.1379e-05                         44294


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6217           3.333     -6.6374e-05      -7.645e-07
v  Velocity[Y]                 -29.682          29.824          6.6823          20.057
v  Velocity[Z]                 -30.327          28.805        0.051739     -0.00038763
v  ǁVelocityǁ                 0.011537          33.273          10.608          20.216
v  Pressure                    -413.29          342.52         -53.763            31.4
v  k                        5.4136e-08          93.729          4.1658          1.6455
v  omega                         1e-24      2.0618e+07          8398.7          11.895
v  turbulent_viscosity      1.4639e-13          1.2904        0.015919           0.109
v  CourantNb                  0.031207          2032.1          44.039          1.3762
v  FourierNb                  0.010841           14763          94.422         0.68326
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14774        0.010816        0.045619


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14839          138.46          2.0595


 TIME FOR THE TIME STEP              356:        0.46229E+02

===============================================================


 INSTANT    0.357000000E+02   TIME STEP NUMBER             357
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.399218275E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31398E+02 0.21356E+02
   Friction velocity        uet   :  0.19097E-02 0.25550E+01
   Friction velocity        uk    :  0.71215E-02 0.34883E+01
   Dimensionless distance   yplus :  0.10400E+00 0.35088E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        402
   Nb of faces within the viscous sub-layer     :        994
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    1924   0.45209E-02   0.29273E+00 
c  VelocityY    0.29385E+04    1924   0.45209E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    1924   0.45209E-02   0.00000E+00 
c  Pressure     0.45534E+00    6985   0.33545E-01   0.21635E+00 
c  k            0.21770E+04    1234   0.13330E-03   0.12855E+01 
c  omega        0.10721E+08     503   0.38479E-04   0.20562E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66089                             1
a  Local Time Step      1.1261e-05                         44316


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0973          2.9025     -0.00012344      -1.952e-06
v  Velocity[Y]                 -35.092          30.315          6.6484          20.057
v  Velocity[Z]                 -28.499          28.592        0.093647       0.0012475
v  ǁVelocityǁ                 0.019011          35.787          10.629          20.216
v  Pressure                    -414.83          342.89         -55.765          31.532
v  k                        1.2765e-08          99.465          4.2157          1.6471
v  omega                         1e-24       1.332e+07          8132.9          11.871
v  turbulent_viscosity      1.4267e-14          1.2819        0.015909         0.10901
v  CourantNb                  0.033771          1998.7          44.068          1.3764
v  FourierNb                  0.010843           14630          96.437         0.68453
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14762        0.010817        0.045656


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14701           140.5          2.0609


 TIME FOR THE TIME STEP              357:        0.45581E+02

===============================================================


 INSTANT    0.358000000E+02   TIME STEP NUMBER             358
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.155786167E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40217E+02 0.13305E+02
   Friction velocity        uet   :  0.11171E-02 0.32722E+01
   Friction velocity        uk    :  0.71186E-02 0.48605E+01
   Dimensionless distance   yplus :  0.90158E-01 0.42577E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1939   0.42836E-02   0.29992E+00 
c  VelocityY    0.29384E+04    1939   0.42836E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1939   0.42836E-02   0.00000E+00 
c  Pressure     0.45215E+00    6998   0.37655E-01   0.21474E+00 
c  k            0.21686E+04    1339   0.12242E-03   0.11817E+01 
c  omega        0.10328E+08     458   0.28905E-04   0.10334E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5914e+05                             1
a  Local Time Step      1.1272e-05                         44296


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3559          3.0495      -0.0003583     -4.1591e-07
v  Velocity[Y]                 -25.346          30.735          6.6644          20.056
v  Velocity[Z]                 -28.353          29.079         0.11473       0.0023026
v  ǁVelocityǁ                 0.010754          33.724          10.622          20.215
v  Pressure                    -414.83           343.7         -57.743          31.628
v  k                        1.1832e-09          51.076          4.1706          1.6486
v  omega                         1e-24      1.1736e+07          7920.4          11.848
v  turbulent_viscosity       1.597e-14           1.276        0.015883         0.10906
v  CourantNb                  0.077018          2940.9          44.367          1.3766
v  FourierNb                  0.010845           14693          96.381         0.68523
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14758        0.010816        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14753          140.75          2.0619


 TIME FOR THE TIME STEP              358:        0.45702E+02

===============================================================


 INSTANT    0.359000000E+02   TIME STEP NUMBER             359
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.710466752E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31051E+02 0.13778E+02
   Friction velocity        uet   :  0.11733E-02 0.27265E+01
   Friction velocity        uk    :  0.16486E-01 0.31703E+01
   Dimensionless distance   yplus :  0.17490E+00 0.26275E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        417
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1954   0.44398E-02   0.30968E+00 
c  VelocityY    0.29383E+04    1954   0.44398E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1954   0.44398E-02   0.00000E+00 
c  Pressure     0.42323E+00    6993   0.36098E-01   0.20004E+00 
c  k            0.21596E+04    1432   0.73321E-04   0.10108E+01 
c  omega        0.10241E+08     296   0.37480E-04   0.13276E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2134e+05                             1
a  Local Time Step      1.0295e-05                         44265


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4476          3.1248     -0.00019221      1.9019e-06
v  Velocity[Y]                 -17.855          31.031          6.6993          20.056
v  Velocity[Z]                 -28.323          29.054         0.11026       0.0036353
v  ǁVelocityǁ                0.0044765          33.784          10.589          20.215
v  Pressure                    -414.34          345.01         -58.646          31.677
v  k                        3.0228e-08          50.779          4.1593          1.6502
v  omega                         1e-24      1.3342e+07          7879.1           11.82
v  turbulent_viscosity      2.0044e-15          1.2688        0.015833         0.10911
v  CourantNb                  0.032978          2811.7          44.564          1.3768
v  FourierNb                  0.010846           14782          95.503         0.68515
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14789        0.010817        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14839          140.07          2.0619


 TIME FOR THE TIME STEP              359:        0.45493E+02

===============================================================


 INSTANT    0.360000000E+02   TIME STEP NUMBER             360
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.176139145E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30932E+02 0.14045E+02
   Friction velocity        uet   :  0.14440E-02 0.28621E+01
   Friction velocity        uk    :  0.14014E-01 0.31572E+01
   Dimensionless distance   yplus :  0.97002E-01 0.28513E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2046   0.44866E-02   0.32842E+00 
c  VelocityY    0.29383E+04    2046   0.44866E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2046   0.44866E-02   0.00000E+00 
c  Pressure     0.43079E+00    6994   0.32329E-01   0.20371E+00 
c  k            0.21521E+04    1457   0.76601E-04   0.10035E+01 
c  omega        0.10472E+08     428   0.23509E-03   0.22980E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4234e+05                             1
a  Local Time Step      1.1023e-05                         44280


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6212           3.093      0.00036869      2.0032e-06
v  Velocity[Y]                 -16.671          32.892          6.7321          20.056
v  Velocity[Z]                 -28.268           29.31        0.080639       0.0048712
v  ǁVelocityǁ                 0.017216          33.642          10.541          20.214
v  Pressure                     -413.7          345.94         -58.369          31.637
v  k                        1.3006e-07          53.244          4.1499          1.6517
v  omega                         1e-24      5.8561e+07          9097.5          11.917
v  turbulent_viscosity      2.0454e-14            1.26        0.015808         0.10919
v  CourantNb                  0.040896          2040.9          44.488          1.3768
v  FourierNb                  0.010847           14889          96.708         0.68545
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010817        0.045703


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14947           141.2          2.0622


 TIME FOR THE TIME STEP              360:        0.47225E+02

===============================================================


 INSTANT    0.361000000E+02   TIME STEP NUMBER             361
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.410114105E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30201E+02 0.14493E+02
   Friction velocity        uet   :  0.40308E-02 0.29247E+01
   Friction velocity        uk    :  0.18842E-01 0.30178E+01
   Dimensionless distance   yplus :  0.10497E+00 0.32178E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1996   0.43199E-02   0.35161E+00 
c  VelocityY    0.29382E+04    1996   0.43199E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1996   0.43199E-02   0.00000E+00 
c  Pressure     0.42915E+00    7043   0.29921E-01   0.20383E+00 
c  k            0.21439E+04    1414   0.72850E-04   0.10796E+01 
c  omega        0.25297E+08     377   0.47158E-04   0.83541E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66642                             1
a  Local Time Step      1.0912e-05                         44312


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5813           3.112       0.0012477      4.0528e-06
v  Velocity[Y]                 -15.049          33.257          6.7416          20.056
v  Velocity[Z]                 -28.369          29.117        0.035127       0.0056128
v  ǁVelocityǁ                 0.019591          33.725          10.502          20.214
v  Pressure                    -403.98          345.18         -58.208          31.329
v  k                        2.5471e-08          48.629             4.1           1.653
v  omega                         1e-24      3.0315e+07          8703.1          11.906
v  turbulent_viscosity      2.0487e-13          1.2534        0.015783         0.10927
v  CourantNb                   0.03353          2064.1          44.401          1.3768
v  FourierNb                  0.010849           14948          98.114         0.68598
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14899        0.010816        0.045674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15011          142.52          2.0627


 TIME FOR THE TIME STEP              361:        0.47630E+02

===============================================================


 INSTANT    0.362000000E+02   TIME STEP NUMBER             362
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.272810858E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29841E+02 0.16435E+02
   Friction velocity        uet   :  0.32098E-02 0.28313E+01
   Friction velocity        uk    :  0.16371E-01 0.31549E+01
   Dimensionless distance   yplus :  0.16227E+00 0.36920E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :        931
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    2018   0.43623E-02   0.36474E+00 
c  VelocityY    0.29382E+04    2018   0.43623E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    2018   0.43623E-02   0.00000E+00 
c  Pressure     0.43996E+00    7034   0.29721E-01   0.20815E+00 
c  k            0.21351E+04    1277   0.64282E-04   0.10078E+01 
c  omega        0.12827E+08     294   0.50997E-04   0.41120E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.224e+05                             1
a  Local Time Step      1.1558e-05                         44328


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6383          3.3696       0.0024916      4.0014e-06
v  Velocity[Y]                 -15.059          34.308          6.7215          20.056
v  Velocity[Z]                 -28.587           29.22       -0.017669       0.0061603
v  ǁVelocityǁ                 0.017075          34.451          10.481          20.214
v  Pressure                    -386.84          343.76         -57.936          30.936
v  k                        4.5202e-08          39.386          4.0575          1.6543
v  omega                         1e-24      1.7173e+07          8496.3          11.879
v  turbulent_viscosity      3.6996e-15          1.2468        0.015743         0.10937
v  CourantNb                  0.031304          2089.2          44.306          1.3768
v  FourierNb                   0.01085           15066          97.445         0.68605
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14887        0.010817        0.045659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15134          141.75          2.0628


 TIME FOR THE TIME STEP              362:        0.46448E+02

===============================================================


 INSTANT    0.363000000E+02   TIME STEP NUMBER             363
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.195715482E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30175E+02 0.20529E+02
   Friction velocity        uet   :  0.19677E-02 0.27293E+01
   Friction velocity        uk    :  0.18466E-01 0.33318E+01
   Dimensionless distance   yplus :  0.65645E-01 0.30887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        483
   Nb of faces within the viscous sub-layer     :        951
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2029   0.47639E-02   0.38050E+00 
c  VelocityY    0.29380E+04    2029   0.47639E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2029   0.47639E-02   0.00000E+00 
c  Pressure     0.42043E+00    6791   0.27501E-01   0.19857E+00 
c  k            0.21278E+04    1059   0.63505E-04   0.10383E+01 
c  omega        0.10882E+08     217   0.17582E-03   0.10920E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1467e-05                         44357


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5843           3.537       0.0029525      5.1663e-06
v  Velocity[Y]                 -15.055          30.718          6.7201          20.056
v  Velocity[Z]                 -30.292          28.974       -0.062382        0.006472
v  ǁVelocityǁ                 0.010927          34.879          10.476          20.214
v  Pressure                    -370.41          343.21         -56.811          30.877
v  k                        1.8283e-08          40.247          4.0184          1.6554
v  omega                         1e-24      8.5771e+07          8401.9          11.858
v  turbulent_viscosity      3.2909e-15          1.2398        0.015708         0.10947
v  CourantNb                  0.021567          2107.4          44.348           1.377
v  FourierNb                  0.010851           15207          96.379         0.68596
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14815        0.010817        0.045653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15282          140.73           2.063


 TIME FOR THE TIME STEP              363:        0.46269E+02

===============================================================


 INSTANT    0.364000000E+02   TIME STEP NUMBER             364
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.249189053E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30331E+02 0.20392E+02
   Friction velocity        uet   :  0.92644E-03 0.28085E+01
   Friction velocity        uk    :  0.17064E-01 0.32614E+01
   Dimensionless distance   yplus :  0.14165E+00 0.27051E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        525
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    2021   0.47120E-02   0.38779E+00 
c  VelocityY    0.29379E+04    2021   0.47120E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    2021   0.47120E-02   0.00000E+00 
c  Pressure     0.44233E+00    6965   0.27443E-01   0.20946E+00 
c  k            0.21230E+04    1128   0.63490E-04   0.11455E+01 
c  omega        0.30915E+08     153   0.34351E-04   0.35533E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.0591e+05                             2
a  Local Time Step      1.2036e-05                         44380


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4739          3.5696       0.0029318      3.8368e-06
v  Velocity[Y]                 -14.973          30.553          6.7476          20.056
v  Velocity[Z]                 -31.822          28.936        -0.10499       0.0065105
v  ǁVelocityǁ                0.0064822          36.407          10.488          20.213
v  Pressure                    -354.84          343.54         -55.007           31.12
v  k                        3.3474e-09          51.122          4.0141          1.6565
v  omega                         1e-24       4.356e+07          8165.1          11.826
v  turbulent_viscosity      3.1472e-14          1.2355          0.0157         0.10956
v  CourantNb                  0.014006          2124.7          44.413           1.377
v  FourierNb                  0.010852           15299          94.735         0.68597
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010818        0.045649


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75451           15378          139.15           2.063


 TIME FOR THE TIME STEP              364:        0.47266E+02

===============================================================


 INSTANT    0.365000000E+02   TIME STEP NUMBER             365
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.202336550E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30646E+02 0.16323E+02
   Friction velocity        uet   :  0.10371E-02 0.30706E+01
   Friction velocity        uk    :  0.11217E-01 0.29855E+01
   Dimensionless distance   yplus :  0.96248E-01 0.26812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        470
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    1983   0.45295E-02   0.39230E+00 
c  VelocityY    0.29378E+04    1983   0.45295E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    1983   0.45295E-02   0.00000E+00 
c  Pressure     0.44985E+00    7106   0.31517E-01   0.21391E+00 
c  k            0.21227E+04    1319   0.69611E-04   0.12921E+01 
c  omega        0.17714E+08     180   0.32471E-04   0.11358E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1608e-05                         44397


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3974          3.4437       0.0028171      3.2044e-06
v  Velocity[Y]                 -15.268          31.398          6.7967          20.057
v  Velocity[Z]                 -33.077          28.806        -0.11512       0.0068232
v  ǁVelocityǁ                0.0032227          36.348          10.547          20.214
v  Pressure                     -412.2          343.59         -53.462          31.358
v  k                        1.8776e-08          63.222          4.0374          1.6575
v  omega                         1e-24      2.3146e+07          8011.4          11.807
v  turbulent_viscosity      9.0572e-17          1.2311        0.015721         0.10966
v  CourantNb                  0.022168          2160.8           44.27          1.3766
v  FourierNb                  0.010852           15305          93.092           0.686
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1479        0.010818        0.045652


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15385          137.36          2.0626


 TIME FOR THE TIME STEP              365:        0.46797E+02

===============================================================


 INSTANT    0.366000000E+02   TIME STEP NUMBER             366
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.868559330E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31356E+02 0.13143E+02
   Friction velocity        uet   :  0.24419E-02 0.31346E+01
   Friction velocity        uk    :  0.12342E-01 0.31784E+01
   Dimensionless distance   yplus :  0.10142E+00 0.26341E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1906   0.43665E-02   0.39980E+00 
c  VelocityY    0.29376E+04    1906   0.43665E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1906   0.43665E-02   0.00000E+00 
c  Pressure     0.42371E+00    7127   0.35588E-01   0.20053E+00 
c  k            0.21291E+04    1393   0.72837E-04   0.13695E+01 
c  omega        0.12113E+08     203   0.46638E-04   0.84923E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.192e-05                         44444


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2936          3.2118       0.0025536      2.6091e-06
v  Velocity[Y]                 -15.037          31.399          6.8535          20.056
v  Velocity[Z]                 -33.187          28.549       -0.081584       0.0065516
v  ǁVelocityǁ                0.0097721           35.19          10.616          20.213
v  Pressure                    -442.89          343.33         -52.378          31.456
v  k                        1.1136e-07          68.175          4.0642          1.6582
v  omega                         1e-24      1.4227e+07          7963.1          11.817
v  turbulent_viscosity      1.9774e-14          1.2281         0.01577         0.10975
v  CourantNb                  0.026707          2699.8          44.227          1.3763
v  FourierNb                  0.010852           15266          92.731         0.68654
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14739        0.010817        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9971           15344          136.96          2.0628


 TIME FOR THE TIME STEP              366:        0.47038E+02

===============================================================


 INSTANT    0.367000000E+02   TIME STEP NUMBER             367
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.459856999E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31177E+02 0.13692E+02
   Friction velocity        uet   :  0.15985E-02 0.31180E+01
   Friction velocity        uk    :  0.15747E-01 0.30328E+01
   Dimensionless distance   yplus :  0.13072E+00 0.26169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    1928   0.45285E-02   0.39364E+00 
c  VelocityY    0.29376E+04    1928   0.45285E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    1928   0.45285E-02   0.00000E+00 
c  Pressure     0.42179E+00    7044   0.36735E-01   0.19924E+00 
c  k            0.21399E+04    1308   0.75377E-04   0.14049E+01 
c  omega        0.10682E+08     234   0.19117E-03   0.12105E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3919e+05                             1
a  Local Time Step      1.0949e-05                         44474


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4777          2.8568       0.0021412     -1.6757e-06
v  Velocity[Y]                  -23.71          30.182          6.8806          20.056
v  Velocity[Z]                 -32.474          28.825       -0.018304       0.0062763
v  ǁVelocityǁ                 0.024724          33.903          10.647          20.213
v  Pressure                    -448.63           343.6         -52.162          31.547
v  k                        2.7269e-08          61.801          4.0659          1.6585
v  omega                         1e-24      6.7043e+07          8359.8           11.88
v  turbulent_viscosity      6.7858e-14          1.2259        0.015804         0.10984
v  CourantNb                  0.017904          2748.9          44.318          1.3762
v  FourierNb                  0.010852           15192          93.377         0.68717
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14774        0.010818         0.04569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95613           15264           137.7          2.0633


 TIME FOR THE TIME STEP              367:        0.47034E+02

===============================================================


 INSTANT    0.368000000E+02   TIME STEP NUMBER             368
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.136495786E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30949E+02 0.13884E+02
   Friction velocity        uet   :  0.61286E-03 0.28867E+01
   Friction velocity        uk    :  0.18235E-01 0.29108E+01
   Dimensionless distance   yplus :  0.11935E+00 0.26056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    1955   0.44538E-02   0.35908E+00 
c  VelocityY    0.29378E+04    1955   0.44538E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    1955   0.44538E-02   0.00000E+00 
c  Pressure     0.42915E+00    6904   0.33940E-01   0.20405E+00 
c  k            0.21502E+04     942   0.78160E-04   0.14246E+01 
c  omega        0.25449E+08     157   0.55393E-04   0.11741E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4895e+05                             1
a  Local Time Step      1.0908e-05                         44459


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7342          2.4037       0.0018849     -2.1317e-06
v  Velocity[Y]                 -26.061           30.01          6.8356          20.056
v  Velocity[Z]                 -31.822          28.617         0.05515        0.005908
v  ǁVelocityǁ                 0.018474          32.689          10.628          20.212
v  Pressure                    -434.63             345          -52.23          31.725
v  k                        1.5525e-07          50.448           4.066          1.6585
v  omega                         1e-24      3.4325e+07          8564.9          11.903
v  turbulent_viscosity       4.914e-15          1.2243         0.01579         0.10992
v  CourantNb                 0.0098499          2252.6          44.445          1.3762
v  FourierNb                  0.010852           15100          92.881         0.68714
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010818         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15166          137.33          2.0634


 TIME FOR THE TIME STEP              368:        0.45430E+02

===============================================================


 INSTANT    0.369000000E+02   TIME STEP NUMBER             369
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.112507945E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31683E+02 0.17685E+02
   Friction velocity        uet   :  0.21939E-02 0.27578E+01
   Friction velocity        uk    :  0.17314E-01 0.28099E+01
   Dimensionless distance   yplus :  0.10598E+00 0.26175E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        374
   Nb of faces within the viscous sub-layer     :        973
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2007   0.46734E-02   0.33457E+00 
c  VelocityY    0.29378E+04    2007   0.46734E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2007   0.46734E-02   0.00000E+00 
c  Pressure     0.43091E+00    6990   0.30252E-01   0.20410E+00 
c  k            0.21548E+04    1263   0.96105E-04   0.13536E+01 
c  omega        0.17184E+08     209   0.47432E-04   0.13792E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4322e+05                             1
a  Local Time Step      1.1208e-05                         44437


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9746          1.8772       0.0019842     -8.6447e-07
v  Velocity[Y]                 -29.459          29.858          6.7473          20.056
v  Velocity[Z]                 -30.353          28.857        0.094078       0.0051897
v  ǁVelocityǁ                 0.014163          33.216          10.639          20.212
v  Pressure                    -407.97          346.43         -52.716          31.751
v  k                        4.0689e-07          80.008           4.097          1.6581
v  omega                         1e-24      4.7287e+07          8412.5          11.912
v  turbulent_viscosity      2.7974e-14          1.2319        0.015753         0.10999
v  CourantNb                   0.01865          2094.9          44.333          1.3762
v  FourierNb                  0.010852           15046          94.292         0.68742
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010818        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15103          138.63          2.0636


 TIME FOR THE TIME STEP              369:        0.46634E+02

===============================================================


 INSTANT    0.370000000E+02   TIME STEP NUMBER             370
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.114546449E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30991E+02 0.19879E+02
   Friction velocity        uet   :  0.19548E-02 0.25955E+01
   Friction velocity        uk    :  0.22960E-01 0.29252E+01
   Dimensionless distance   yplus :  0.17499E+00 0.29487E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    2033   0.46203E-02   0.32637E+00 
c  VelocityY    0.29379E+04    2033   0.46203E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    2033   0.46203E-02   0.00000E+00 
c  Pressure     0.44582E+00    6985   0.32116E-01   0.21154E+00 
c  k            0.21515E+04    1408   0.11260E-03   0.12082E+01 
c  omega        0.28542E+08     350   0.18693E-04   0.54931E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6544e+05                             1
a  Local Time Step      1.0803e-05                         44390


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2019           1.599       0.0019396      1.0649e-06
v  Velocity[Y]                 -38.661          30.165          6.7085          20.056
v  Velocity[Z]                  -28.43          29.005         0.12705       0.0045276
v  ǁVelocityǁ                0.0075907          40.111          10.651          20.212
v  Pressure                    -411.28          347.91         -53.668          31.978
v  k                        3.2797e-08          94.234           4.138          1.6575
v  omega                         1e-24       2.363e+07          8279.3          11.914
v  turbulent_viscosity      1.1053e-13          1.2417         0.01569         0.11005
v  CourantNb                  0.048029          2067.2          44.444          1.3763
v  FourierNb                  0.010853           15100          95.162         0.68799
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14771        0.010819        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15155          139.61          2.0643


 TIME FOR THE TIME STEP              370:        0.48156E+02

===============================================================


 INSTANT    0.371000000E+02   TIME STEP NUMBER             371
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.179384373E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.51677E+02 0.14128E+02
   Friction velocity        uet   :  0.17566E-02 0.35385E+01
   Friction velocity        uk    :  0.16888E-01 0.44630E+01
   Dimensionless distance   yplus :  0.49039E-01 0.39051E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2122   0.46639E-02   0.32008E+00 
c  VelocityY    0.29380E+04    2122   0.46639E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2122   0.46639E-02   0.00000E+00 
c  Pressure     0.42431E+00    6770   0.36981E-01   0.20205E+00 
c  k            0.21442E+04    1423   0.11397E-03   0.10614E+01 
c  omega        0.12316E+08     433   0.44709E-04   0.35440E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9097e+05                             2
a  Local Time Step      1.1344e-05                         44331


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3855           1.744       0.0014148     -6.3435e-07
v  Velocity[Y]                 -29.001          30.562          6.7122          20.056
v  Velocity[Z]                 -28.469          28.767          0.1426       0.0036432
v  ǁVelocityǁ                0.0082097          33.644          10.641          20.212
v  Pressure                    -412.23           349.2          -54.88          32.253
v  k                        1.6044e-09          43.758          4.1109          1.6567
v  omega                         1e-24      1.3965e+07          8176.6           11.91
v  turbulent_viscosity      4.6111e-15          1.2534        0.015632          0.1101
v  CourantNb                  0.034778          2472.8          44.804          1.3765
v  FourierNb                  0.010852           15156          94.617         0.68805
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14751        0.010819        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15211          139.42          2.0646


 TIME FOR THE TIME STEP              371:        0.49828E+02

===============================================================


 INSTANT    0.372000000E+02   TIME STEP NUMBER             372
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.428540901E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30642E+02 0.14087E+02
   Friction velocity        uet   :  0.63899E-03 0.29789E+01
   Friction velocity        uk    :  0.13275E-01 0.31606E+01
   Dimensionless distance   yplus :  0.10165E+00 0.27325E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2210   0.44603E-02   0.31572E+00 
c  VelocityY    0.29383E+04    2210   0.44603E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2210   0.44603E-02   0.00000E+00 
c  Pressure     0.42245E+00    7001   0.37050E-01   0.20081E+00 
c  k            0.21368E+04    1393   0.67949E-04   0.90120E+00 
c  omega        0.14588E+08     310   0.80289E-04   0.48328E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8539e+05                             2
a  Local Time Step        1.15e-05                         44290


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5043          1.8121      0.00070702      1.7761e-06
v  Velocity[Y]                 -17.682          31.859          6.7288          20.056
v  Velocity[Z]                 -28.565          28.781         0.13263       0.0024879
v  ǁVelocityǁ                 0.010374          33.537          10.603          20.212
v  Pressure                    -412.37          349.55         -55.657          32.511
v  k                        2.0936e-10          51.072          4.1043          1.6558
v  omega                         1e-24        2.71e+07          8199.5          11.887
v  turbulent_viscosity       1.829e-15           1.266        0.015576         0.11015
v  CourantNb                 0.0035788          3085.6          45.093          1.3766
v  FourierNb                  0.010852           15229          93.406         0.68725
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14852        0.010819        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15290           138.5          2.0639


 TIME FOR THE TIME STEP              372:        0.49634E+02

===============================================================


 INSTANT    0.373000000E+02   TIME STEP NUMBER             373
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.664564349E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30470E+02 0.13874E+02
   Friction velocity        uet   :  0.34710E-03 0.29542E+01
   Friction velocity        uk    :  0.13183E-01 0.33169E+01
   Dimensionless distance   yplus :  0.85179E-01 0.28236E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    2230   0.44734E-02   0.32530E+00 
c  VelocityY    0.29386E+04    2230   0.44734E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    2230   0.44734E-02   0.00000E+00 
c  Pressure     0.43243E+00    7006   0.33748E-01   0.20373E+00 
c  k            0.21305E+04    1232   0.64854E-04   0.84094E+00 
c  omega        0.12403E+08     282   0.26348E-03   0.24525E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -21775                             1
a  Local Time Step      1.1669e-05                         44300


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4889           1.734       0.0002227      1.9776e-06
v  Velocity[Y]                 -17.165          33.596          6.7476          20.056
v  Velocity[Z]                 -28.669          28.878        0.096587       0.0011831
v  ǁVelocityǁ                  0.01554          34.114          10.562          20.212
v  Pressure                    -411.29          348.98         -55.766          32.398
v  k                        1.0633e-09          50.878          4.1234          1.6549
v  omega                         1e-24      6.6394e+07            8882          11.909
v  turbulent_viscosity      3.5135e-16          1.2782         0.01557         0.11018
v  CourantNb                  0.047138          2013.9            44.9          1.3765
v  FourierNb                   0.01085           15377           94.25         0.68715
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14858         0.01082        0.045666


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15439          139.15          2.0637


 TIME FOR THE TIME STEP              373:        0.48261E+02

===============================================================


 INSTANT    0.374000000E+02   TIME STEP NUMBER             374
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.445912943E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30293E+02 0.15404E+02
   Friction velocity        uet   :  0.50740E-03 0.29919E+01
   Friction velocity        uk    :  0.17520E-01 0.29526E+01
   Dimensionless distance   yplus :  0.76200E-01 0.32405E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        542
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    2233   0.44256E-02   0.34032E+00 
c  VelocityY    0.29388E+04    2233   0.44256E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    2233   0.44256E-02   0.00000E+00 
c  Pressure     0.42090E+00    7045   0.31840E-01   0.19811E+00 
c  k            0.21255E+04    1195   0.66812E-04   0.93938E+00 
c  omega        0.31049E+08     331   0.45028E-04   0.13449E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2338e+05                             1
a  Local Time Step      1.1412e-05                         44314


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3637          1.5263      0.00018422       2.092e-06
v  Velocity[Y]                 -15.384          33.769          6.7629          20.057
v  Velocity[Z]                 -28.669          28.571        0.041829     -0.00021518
v  ǁVelocityǁ                0.0079951          34.122          10.521          20.212
v  Pressure                    -402.62           346.9         -56.144          32.054
v  k                        1.5837e-08          50.812          4.0929          1.6539
v  omega                         1e-24      3.4253e+07          8641.4          11.927
v  turbulent_viscosity      5.3139e-15          1.2866        0.015596          0.1102
v  CourantNb                  0.029746          2012.7          44.563          1.3764
v  FourierNb                  0.010848           15481          96.309         0.68792
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010819        0.045666


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15546          140.87          2.0643


 TIME FOR THE TIME STEP              374:        0.48130E+02

===============================================================


 INSTANT    0.375000000E+02   TIME STEP NUMBER             375
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.366518353E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29820E+02 0.14085E+02
   Friction velocity        uet   :  0.49428E-03 0.29035E+01
   Friction velocity        uk    :  0.16792E-01 0.29693E+01
   Dimensionless distance   yplus :  0.11352E+00 0.35232E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    2193   0.44529E-02   0.35447E+00 
c  VelocityY    0.29389E+04    2193   0.44529E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    2193   0.44529E-02   0.00000E+00 
c  Pressure     0.43272E+00    7022   0.30612E-01   0.20393E+00 
c  k            0.21202E+04    1376   0.63886E-04   0.86554E+00 
c  omega        0.19143E+08     295   0.15527E-03   0.19313E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1428e+05                             1
a  Local Time Step      1.0965e-05                         44375


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1558          1.4093      8.6479e-06     -6.1636e-07
v  Velocity[Y]                 -15.113          34.268          6.7405          20.057
v  Velocity[Z]                 -29.022          28.543       -0.025439       -0.001532
v  ǁVelocityǁ                0.0074565          34.695          10.507          20.213
v  Pressure                    -389.29          344.96         -56.584           31.51
v  k                        7.1994e-09           42.92          4.0555           1.653
v  omega                         1e-24      7.7213e+07          8961.9          11.958
v  turbulent_viscosity      2.8256e-14          1.2957         0.01561         0.11022
v  CourantNb                  0.018139            2006          44.425          1.3764
v  FourierNb                  0.010847           15538          96.545         0.68828
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010818        0.045654


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15608          140.97          2.0647


 TIME FOR THE TIME STEP              375:        0.47847E+02

===============================================================


 INSTANT    0.376000000E+02   TIME STEP NUMBER             376
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.903737791E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30660E+02 0.20351E+02
   Friction velocity        uet   :  0.31675E-03 0.27696E+01
   Friction velocity        uk    :  0.14632E-01 0.32328E+01
   Dimensionless distance   yplus :  0.88929E-01 0.35331E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    2155   0.42444E-02   0.36082E+00 
c  VelocityY    0.29390E+04    2155   0.42444E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    2155   0.42444E-02   0.00000E+00 
c  Pressure     0.46214E+00    6682   0.28984E-01   0.22021E+00 
c  k            0.21164E+04    1429   0.61833E-04   0.88109E+00 
c  omega        0.30708E+08     193   0.20198E-03   0.85107E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                     -7812                             1
a  Local Time Step      1.1493e-05                         44403


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9211          1.3839     -4.2332e-05     -9.2415e-07
v  Velocity[Y]                 -14.957          31.289          6.7239          20.056
v  Velocity[Z]                 -28.681          28.645       -0.075837      -0.0027276
v  ǁVelocityǁ                 0.016595           33.46          10.503          20.212
v  Pressure                    -375.15          343.72         -56.394          31.279
v  k                        9.3075e-09           42.58          4.0358          1.6523
v  omega                         1e-24      2.2107e+08          9590.3          11.991
v  turbulent_viscosity      1.7548e-14          1.3062        0.015623         0.11023
v  CourantNb                 0.0073681          1993.3          44.257          1.3765
v  FourierNb                  0.010845           15504          95.648         0.68811
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010817        0.045663


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15577           139.9          2.0646


 TIME FOR THE TIME STEP              376:        0.46305E+02

===============================================================


 INSTANT    0.377000000E+02   TIME STEP NUMBER             377
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.222076806E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30886E+02 0.20493E+02
   Friction velocity        uet   :  0.10465E-02 0.27072E+01
   Friction velocity        uk    :  0.14590E-01 0.30202E+01
   Dimensionless distance   yplus :  0.14843E+00 0.29432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    2097   0.45472E-02   0.36942E+00 
c  VelocityY    0.29389E+04    2097   0.45472E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    2097   0.45472E-02   0.00000E+00 
c  Pressure     0.42816E+00    7000   0.27122E-01   0.20237E+00 
c  k            0.21153E+04    1431   0.62211E-04   0.98948E+00 
c  omega        0.19328E+09      81   0.14460E-04   0.33890E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8316e+05                             1
a  Local Time Step      1.1443e-05                         44402


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6691          1.3695     -0.00015221     -3.0913e-06
v  Velocity[Y]                 -15.083          30.802          6.7362          20.056
v  Velocity[Z]                 -31.714          28.603        -0.12038      -0.0042175
v  ǁVelocityǁ                 0.012328           36.45          10.511          20.212
v  Pressure                     -366.9          344.08         -55.014          31.368
v  k                        8.6442e-09          53.085          4.0523          1.6519
v  omega                         1e-24      1.1077e+08          9183.3          11.927
v  turbulent_viscosity      1.1033e-14          1.3141        0.015639         0.11024
v  CourantNb                  0.040999          1981.9          44.378          1.3766
v  FourierNb                  0.010844           15388          94.486         0.68769
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.149        0.010817         0.04569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91317           15462          138.86          2.0643


 TIME FOR THE TIME STEP              377:        0.47381E+02

===============================================================


 INSTANT    0.378000000E+02   TIME STEP NUMBER             378
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.314523847E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31068E+02 0.18821E+02
   Friction velocity        uet   :  0.80808E-03 0.30709E+01
   Friction velocity        uk    :  0.73985E-02 0.30944E+01
   Dimensionless distance   yplus :  0.61047E-01 0.26859E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        474
   Nb of faces within the viscous sub-layer     :       1068
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    2008   0.44654E-02   0.37079E+00 
c  VelocityY    0.29390E+04    2008   0.44654E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    2008   0.44654E-02   0.00000E+00 
c  Pressure     0.43035E+00    6877   0.30958E-01   0.20309E+00 
c  k            0.21186E+04    1366   0.67148E-04   0.11453E+01 
c  omega        0.53482E+08     129   0.27444E-04   0.10432E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80796                             1
a  Local Time Step      1.1798e-05                         44416


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3859          1.3552     -0.00015271     -4.0007e-06
v  Velocity[Y]                 -15.047          33.006          6.7748          20.057
v  Velocity[Z]                  -32.54          28.441        -0.15002       -0.005232
v  ǁVelocityǁ                0.0065398          36.687          10.551          20.213
v  Pressure                    -407.94           344.1          -54.09          31.472
v  k                        1.6312e-09          64.557          4.0885          1.6517
v  omega                         1e-24      5.5905e+07          8612.5          11.866
v  turbulent_viscosity      9.5246e-15          1.3196        0.015696         0.11024
v  CourantNb                  0.026433          2125.3           44.31          1.3765
v  FourierNb                  0.010843           15143          93.348         0.68753
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010816        0.045674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15217          137.66           2.064


 TIME FOR THE TIME STEP              378:        0.46051E+02

===============================================================


 INSTANT    0.379000000E+02   TIME STEP NUMBER             379
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.111066393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31651E+02 0.17346E+02
   Friction velocity        uet   :  0.17499E-02 0.32234E+01
   Friction velocity        uk    :  0.18526E-01 0.32128E+01
   Dimensionless distance   yplus :  0.12183E+00 0.26614E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        417
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1891   0.43406E-02   0.38266E+00 
c  VelocityY    0.29391E+04    1891   0.43406E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1891   0.43406E-02   0.00000E+00 
c  Pressure     0.44151E+00    7020   0.36076E-01   0.20794E+00 
c  k            0.21289E+04    1232   0.72995E-04   0.12650E+01 
c  omega        0.17935E+08     276   0.99735E-04   0.11756E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4921e+05                             1
a  Local Time Step      1.0913e-05                         44483


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1479          1.3482      0.00033752      -3.027e-06
v  Velocity[Y]                 -15.213          32.126           6.829          20.057
v  Velocity[Z]                 -32.954          28.664        -0.13463      -0.0060937
v  ǁVelocityǁ                0.0078253          34.627          10.611          20.213
v  Pressure                    -440.13          344.52         -53.235           31.57
v  k                        4.7671e-08          69.964           4.119          1.6518
v  omega                         1e-24      6.4052e+07            8497          11.881
v  turbulent_viscosity       2.127e-15          1.3238        0.015764         0.11025
v  CourantNb                  0.014292          2637.9          44.215          1.3763
v  FourierNb                  0.010841           15049          93.264         0.68744
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010815        0.045658


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15116          137.48          2.0637


 TIME FOR THE TIME STEP              379:        0.45534E+02

===============================================================


 INSTANT    0.380000000E+02   TIME STEP NUMBER             380
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.542015457E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30769E+02 0.17113E+02
   Friction velocity        uet   :  0.15016E-02 0.31960E+01
   Friction velocity        uk    :  0.14990E-01 0.31753E+01
   Dimensionless distance   yplus :  0.16641E+00 0.26473E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        410
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1796   0.43671E-02   0.38722E+00 
c  VelocityY    0.29391E+04    1796   0.43671E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1796   0.43671E-02   0.00000E+00 
c  Pressure     0.39233E+00    7010   0.38403E-01   0.18523E+00 
c  k            0.21443E+04    1168   0.76087E-04   0.13237E+01 
c  omega        0.21326E+08     168   0.10393E-03   0.14788E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -95336                             1
a  Local Time Step      1.1804e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2119          1.3599       0.0013377     -8.1631e-07
v  Velocity[Y]                 -20.583          30.276          6.8658          20.056
v  Velocity[Z]                 -33.202          28.649       -0.079409      -0.0071412
v  ǁVelocityǁ                0.0043804          34.702          10.641          20.213
v  Pressure                    -449.01          344.52         -53.201          31.522
v  k                        8.5359e-08          65.137          4.1196          1.6519
v  omega                         1e-24      7.6067e+07          8573.8          11.886
v  turbulent_viscosity      5.5312e-15          1.3295        0.015805         0.11026
v  CourantNb                  0.034552          2778.6          44.181          1.3762
v  FourierNb                  0.010841           15068          92.966          0.6871
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14841        0.010816        0.045643


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98159           15127          137.15          2.0632


 TIME FOR THE TIME STEP              380:        0.44696E+02

===============================================================


 INSTANT    0.381000000E+02   TIME STEP NUMBER             381
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.513794883E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31056E+02 0.15980E+02
   Friction velocity        uet   :  0.15078E-02 0.29555E+01
   Friction velocity        uk    :  0.10011E-01 0.29034E+01
   Dimensionless distance   yplus :  0.10723E+00 0.26502E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1841   0.44628E-02   0.36415E+00 
c  VelocityY    0.29390E+04    1841   0.44628E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1841   0.44628E-02   0.00000E+00 
c  Pressure     0.40849E+00    7013   0.36331E-01   0.19290E+00 
c  k            0.21601E+04    1368   0.79811E-04   0.13603E+01 
c  omega        0.27526E+08     150   0.49165E-04   0.89073E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7893e+05                             1
a  Local Time Step      1.1497e-05                         44519


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2242          1.3856       0.0015429      -3.517e-08
v  Velocity[Y]                 -24.318          30.112          6.8451          20.057
v  Velocity[Z]                 -33.204          28.962       -0.011309      -0.0075977
v  ǁVelocityǁ                0.0016412          34.043          10.631          20.213
v  Pressure                     -439.7          345.66         -53.371          31.621
v  k                        2.5326e-07          51.596          4.1122           1.652
v  omega                         1e-24      3.8758e+07          8653.4          11.899
v  turbulent_viscosity      5.4157e-14          1.3317        0.015812         0.11027
v  CourantNb                  0.046736          2444.2          44.207          1.3762
v  FourierNb                  0.010841           15126          93.198          0.6869
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14831        0.010816         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98663           15181           137.4          2.0631


 TIME FOR THE TIME STEP              381:        0.45899E+02

===============================================================


 INSTANT    0.382000000E+02   TIME STEP NUMBER             382
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.184790685E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30999E+02 0.15719E+02
   Friction velocity        uet   :  0.11707E-02 0.28996E+01
   Friction velocity        uk    :  0.90031E-02 0.30438E+01
   Dimensionless distance   yplus :  0.12244E+00 0.26988E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1879   0.44903E-02   0.34223E+00 
c  VelocityY    0.29389E+04    1879   0.44903E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1879   0.44903E-02   0.00000E+00 
c  Pressure     0.42645E+00    7057   0.32422E-01   0.20227E+00 
c  k            0.21711E+04    1480   0.88862E-04   0.13274E+01 
c  omega        0.13285E+08     237   0.56273E-04   0.40679E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -76733                             1
a  Local Time Step      1.1424e-05                         44519


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1688          1.4173      0.00077857      6.3653e-07
v  Velocity[Y]                 -37.036          30.003          6.7636          20.057
v  Velocity[Z]                 -30.972           28.74        0.033311      -0.0077999
v  ǁVelocityǁ                0.0082888          37.196          10.629          20.213
v  Pressure                    -414.92          347.08         -53.631          31.626
v  k                        3.4099e-08          78.548          4.1285          1.6522
v  omega                         1e-24      2.0761e+07          8347.2          11.882
v  turbulent_viscosity      4.5626e-14          1.3324        0.015789         0.11028
v  CourantNb                  0.031522          2007.1          44.258          1.3763
v  FourierNb                  0.010841           15264          94.021         0.68679
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010817        0.045703


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15316          138.28          2.0631


 TIME FOR THE TIME STEP              382:        0.46359E+02

===============================================================


 INSTANT    0.383000000E+02   TIME STEP NUMBER             383
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.117363529E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30737E+02 0.25216E+02
   Friction velocity        uet   :  0.42987E-03 0.31679E+01
   Friction velocity        uk    :  0.12422E-01 0.28857E+01
   Dimensionless distance   yplus :  0.12545E+00 0.29466E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        400
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1776   0.43454E-02   0.33769E+00 
c  VelocityY    0.29389E+04    1776   0.43454E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1776   0.43454E-02   0.00000E+00 
c  Pressure     0.44552E+00    6976   0.33398E-01   0.21110E+00 
c  k            0.21743E+04    1493   0.12081E-03   0.11753E+01 
c  omega        0.10679E+08     415   0.37668E-04   0.23179E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.428e+05                             1
a  Local Time Step      1.1427e-05                         44483


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1611          1.4349     -0.00019935     -6.7309e-07
v  Velocity[Y]                 -38.429          30.193          6.7049          20.056
v  Velocity[Z]                 -28.556          28.745        0.066656      -0.0082841
v  ǁVelocityǁ                 0.011221          42.109          10.642          20.213
v  Pressure                    -415.23          347.83         -54.528          31.666
v  k                        1.4325e-09          102.82          4.1607          1.6526
v  omega                         1e-24      1.2845e+07          8122.5          11.876
v  turbulent_viscosity      1.0822e-13          1.3302        0.015746         0.11031
v  CourantNb                  0.056218          2084.6          44.418          1.3765
v  FourierNb                  0.010841           15382          94.615         0.68693
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14859        0.010817        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89485           15440          139.03          2.0634


 TIME FOR THE TIME STEP              383:        0.45344E+02

===============================================================


 INSTANT    0.384000000E+02   TIME STEP NUMBER             384
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.108931216E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57277E+02 0.14298E+02
   Friction velocity        uet   :  0.43374E-03 0.36730E+01
   Friction velocity        uk    :  0.21246E-01 0.46596E+01
   Dimensionless distance   yplus :  0.12452E+00 0.38850E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :       1036
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1817   0.45576E-02   0.33748E+00 
c  VelocityY    0.29388E+04    1817   0.45576E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1817   0.45576E-02   0.00000E+00 
c  Pressure     0.42854E+00    7009   0.38140E-01   0.20303E+00 
c  k            0.21717E+04    1439   0.12297E-03   0.10230E+01 
c  omega        0.10368E+08     499   0.23039E-03   0.12762E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -4491.5                             1
a  Local Time Step       1.121e-05                         44440


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.146          1.4456     -0.00033918     -1.2137e-06
v  Velocity[Y]                  -32.28          30.435          6.7063          20.056
v  Velocity[Z]                 -28.912          28.627         0.08734      -0.0082872
v  ǁVelocityǁ                 0.015763          33.615          10.634          20.213
v  Pressure                    -415.54          347.81         -55.837          32.076
v  k                        1.1617e-10           62.61          4.1474          1.6533
v  omega                         1e-24      2.0662e+08            8727          11.945
v  turbulent_viscosity      5.2405e-15          1.3309        0.015694         0.11034
v  CourantNb                  0.026128          1990.8          44.671          1.3768
v  FourierNb                  0.010841           15462          94.446         0.68697
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010817        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15526          139.12          2.0638


 TIME FOR THE TIME STEP              384:        0.46554E+02

===============================================================


 INSTANT    0.385000000E+02   TIME STEP NUMBER             385
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.414759940E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30305E+02 0.14261E+02
   Friction velocity        uet   :  0.56447E-03 0.30830E+01
   Friction velocity        uk    :  0.14186E-01 0.32339E+01
   Dimensionless distance   yplus :  0.12761E+00 0.29011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1841   0.43504E-02   0.33705E+00 
c  VelocityY    0.29388E+04    1841   0.43504E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1841   0.43504E-02   0.00000E+00 
c  Pressure     0.42542E+00    7008   0.39290E-01   0.20105E+00 
c  k            0.21677E+04    1263   0.75073E-04   0.88859E+00 
c  omega        0.37232E+09      86   0.49225E-05   0.46153E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5348e+05                             1
a  Local Time Step      1.1549e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0053          1.4441      0.00045933     -4.2942e-07
v  Velocity[Y]                 -17.706          30.859          6.7308          20.056
v  Velocity[Z]                 -28.589          28.537        0.087741      -0.0079266
v  ǁVelocityǁ                0.0047191          33.622          10.607          20.214
v  Pressure                    -415.38          347.31         -56.723          32.266
v  k                        1.0886e-09           48.51          4.1329          1.6541
v  omega                         1e-24       1.033e+08          8753.2          11.923
v  turbulent_viscosity      2.2088e-16          1.3302        0.015665         0.11038
v  CourantNb                  0.034492          3077.1          45.011          1.3771
v  FourierNb                  0.010842           15598          93.565         0.68692
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010816        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15668          138.58           2.064


 TIME FOR THE TIME STEP              385:        0.44829E+02

===============================================================


 INSTANT    0.386000000E+02   TIME STEP NUMBER             386
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.237850789E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30142E+02 0.13536E+02
   Friction velocity        uet   :  0.21416E-02 0.27772E+01
   Friction velocity        uk    :  0.20791E-01 0.29431E+01
   Dimensionless distance   yplus :  0.61944E-01 0.27488E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1850   0.44804E-02   0.35144E+00 
c  VelocityY    0.29387E+04    1850   0.44804E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1850   0.44804E-02   0.00000E+00 
c  Pressure     0.45802E+00    7003   0.35056E-01   0.21749E+00 
c  k            0.21645E+04     971   0.63772E-04   0.78775E+00 
c  omega        0.99407E+08     146   0.31617E-04   0.44295E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1561e-05                         44413


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2466          1.6331       0.0011158     -4.1987e-07
v  Velocity[Y]                 -17.428          32.454          6.7558          20.056
v  Velocity[Z]                 -28.547          28.703        0.059057      -0.0079368
v  ǁVelocityǁ                 0.016519          34.134           10.57          20.214
v  Pressure                    -414.37          346.92         -56.724          32.224
v  k                        3.6566e-09          51.111          4.1567           1.655
v  omega                         1e-24      6.6342e+07          9467.3          11.954
v  turbulent_viscosity       2.367e-15          1.3277        0.015673         0.11043
v  CourantNb                  0.020557          2215.9          44.874           1.377
v  FourierNb                  0.010843           15736          94.322         0.68742
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14928        0.010814        0.045748


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15810           139.2          2.0645


 TIME FOR THE TIME STEP              386:        0.43820E+02

===============================================================


 INSTANT    0.387000000E+02   TIME STEP NUMBER             387
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.935107168E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30232E+02 0.13733E+02
   Friction velocity        uet   :  0.20731E-02 0.29187E+01
   Friction velocity        uk    :  0.11397E-01 0.32102E+01
   Dimensionless distance   yplus :  0.90536E-01 0.30803E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        523
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1782   0.45321E-02   0.37389E+00 
c  VelocityY    0.29387E+04    1782   0.45321E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1782   0.45321E-02   0.00000E+00 
c  Pressure     0.43648E+00    6988   0.31760E-01   0.20681E+00 
c  k            0.21619E+04    1311   0.64658E-04   0.86847E+00 
c  omega        0.48338E+08     314   0.31397E-04   0.14680E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4627e+05                             1
a  Local Time Step      1.1559e-05                         44439


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3314          1.8072      0.00089419     -2.0086e-06
v  Velocity[Y]                 -15.825          33.415          6.7777          20.056
v  Velocity[Z]                 -28.567          28.569        0.014572      -0.0074694
v  ǁVelocityǁ                 0.017979          33.918           10.54          20.214
v  Pressure                    -408.96          346.34         -56.475          32.017
v  k                        6.9917e-09          54.687           4.133           1.656
v  omega                         1e-24      3.4069e+07          8955.5          11.919
v  turbulent_viscosity      8.2264e-15          1.3241        0.015678         0.11049
v  CourantNb                  0.040641          2069.3          44.532           1.377
v  FourierNb                  0.010844           15821          96.133         0.68823
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010815         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15898          140.66          2.0652


 TIME FOR THE TIME STEP              387:        0.45322E+02

===============================================================


 INSTANT    0.388000000E+02   TIME STEP NUMBER             388
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.334433622E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30729E+02 0.14802E+02
   Friction velocity        uet   :  0.11253E-02 0.28904E+01
   Friction velocity        uk    :  0.82067E-02 0.33388E+01
   Dimensionless distance   yplus :  0.11402E+00 0.34500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1649   0.45099E-02   0.39667E+00 
c  VelocityY    0.29387E+04    1649   0.45099E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1649   0.45099E-02   0.00000E+00 
c  Pressure     0.42091E+00    6912   0.31489E-01   0.19913E+00 
c  k            0.21575E+04    1467   0.65289E-04   0.83249E+00 
c  omega        0.20647E+08     308   0.51319E-04   0.92144E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.595e+05                             1
a  Local Time Step      1.1251e-05                         44453


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4996          1.9042      0.00011494     -2.5572e-06
v  Velocity[Y]                 -15.013          33.551          6.7591          20.056
v  Velocity[Z]                  -28.75          28.676       -0.044398      -0.0069795
v  ǁVelocityǁ                0.0065715          33.854          10.532          20.214
v  Pressure                    -392.41          344.83         -56.815            31.4
v  k                        1.0492e-07           43.07          4.0901           1.657
v  omega                         1e-24      4.3599e+07          8707.5          11.908
v  turbulent_viscosity      1.1567e-14          1.3196        0.015651         0.11056
v  CourantNb                  0.051934          2089.2          44.409          1.3771
v  FourierNb                  0.010845           15838          96.552         0.68894
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14755        0.010815        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15916          140.96          2.0661


 TIME FOR THE TIME STEP              388:        0.43742E+02

===============================================================


 INSTANT    0.389000000E+02   TIME STEP NUMBER             389
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.283510083E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31028E+02 0.23129E+02
   Friction velocity        uet   :  0.27666E-02 0.28048E+01
   Friction velocity        uk    :  0.17998E-01 0.31499E+01
   Dimensionless distance   yplus :  0.10440E+00 0.37267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        500
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1602   0.43979E-02   0.41176E+00 
c  VelocityY    0.29388E+04    1602   0.43979E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1602   0.43979E-02   0.00000E+00 
c  Pressure     0.43303E+00    6938   0.30525E-01   0.20605E+00 
c  k            0.21526E+04    1466   0.59314E-04   0.80533E+00 
c  omega        0.17159E+08     253   0.30001E-04   0.25938E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1248e+05                             1
a  Local Time Step      1.1591e-05                         44469


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5681          1.9046     -0.00087559       -3.91e-06
v  Velocity[Y]                 -14.774          32.804          6.7359          20.056
v  Velocity[Z]                 -28.713          28.966        -0.08661      -0.0063436
v  ǁVelocityǁ                 0.010807          33.034          10.533          20.214
v  Pressure                    -380.69          344.68           -56.3          31.168
v  k                        1.0399e-08          36.154          4.0671          1.6581
v  omega                         1e-24      2.1994e+07          8301.9          11.846
v  turbulent_viscosity      8.0242e-14          1.3161         0.01561         0.11064
v  CourantNb                  0.043139          2102.5           44.26          1.3774
v  FourierNb                  0.010846           15752          95.784         0.68925
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14872        0.010815        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15826          140.04          2.0667


 TIME FOR THE TIME STEP              389:        0.42538E+02

===============================================================


 INSTANT    0.390000000E+02   TIME STEP NUMBER             390
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.327935919E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31197E+02 0.21364E+02
   Friction velocity        uet   :  0.74682E-03 0.26110E+01
   Friction velocity        uk    :  0.19490E-01 0.29194E+01
   Dimensionless distance   yplus :  0.12097E+00 0.30222E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :        957
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1557   0.45037E-02   0.42874E+00 
c  VelocityY    0.29388E+04    1557   0.45037E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1557   0.45037E-02   0.00000E+00 
c  Pressure     0.41768E+00    6973   0.28647E-01   0.19824E+00 
c  k            0.21488E+04    1358   0.59744E-04   0.88605E+00 
c  omega        0.11309E+08     219   0.27077E-04   0.99119E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7221e+05                             1
a  Local Time Step      1.1429e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7154          1.7944      -0.0014433     -4.7056e-06
v  Velocity[Y]                 -15.151           30.61          6.7343          20.056
v  Velocity[Z]                  -31.02           28.65        -0.12044      -0.0055323
v  ǁVelocityǁ                 0.012148          36.502          10.541          20.214
v  Pressure                    -358.75          345.99         -54.593           31.26
v  k                        6.8637e-08          47.132           4.067          1.6593
v  omega                         1e-24      1.1715e+07          8057.5          11.817
v  turbulent_viscosity      6.0029e-14           1.313        0.015582         0.11073
v  CourantNb                  0.022859            2103           44.38          1.3777
v  FourierNb                  0.010846           15646          94.764         0.68966
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1481        0.010815        0.045669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80249           15716          139.14          2.0674


 TIME FOR THE TIME STEP              390:        0.42600E+02

===============================================================


 INSTANT    0.391000000E+02   TIME STEP NUMBER             391
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.261568291E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31714E+02 0.19495E+02
   Friction velocity        uet   :  0.20254E-02 0.30022E+01
   Friction velocity        uk    :  0.78935E-02 0.30229E+01
   Dimensionless distance   yplus :  0.65523E-01 0.26849E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1660   0.44828E-02   0.43424E+00 
c  VelocityY    0.29387E+04    1660   0.44828E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1660   0.44828E-02   0.00000E+00 
c  Pressure     0.39815E+00    7063   0.31032E-01   0.18839E+00 
c  k            0.21473E+04    1156   0.62354E-04   0.10214E+01 
c  omega        0.10567E+08     212   0.24891E-04   0.62072E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -81397                             1
a  Local Time Step      1.1345e-05                         44456


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8732          1.5642      -0.0014861     -6.1768e-07
v  Velocity[Y]                 -14.505          30.995          6.7539          20.056
v  Velocity[Z]                 -32.311          28.695         -0.1402      -0.0047052
v  ǁVelocityǁ                0.0013758          37.029          10.576          20.214
v  Pressure                    -398.08          347.35         -52.951          31.455
v  k                        1.5036e-08          58.364          4.0874          1.6606
v  omega                         1e-24      1.1712e+07          7989.7          11.799
v  turbulent_viscosity      5.2808e-14          1.3073        0.015596         0.11083
v  CourantNb                  0.059053          2093.3          44.402          1.3777
v  FourierNb                  0.010847           15528          93.355         0.69038
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010816         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15592          137.76           2.068


 TIME FOR THE TIME STEP              391:        0.42537E+02

===============================================================


 INSTANT    0.392000000E+02   TIME STEP NUMBER             392
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.348280228E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31920E+02 0.14908E+02
   Friction velocity        uet   :  0.15565E-02 0.31131E+01
   Friction velocity        uk    :  0.13516E-01 0.32029E+01
   Dimensionless distance   yplus :  0.65266E-01 0.26693E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :        923
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1789   0.43086E-02   0.44214E+00 
c  VelocityY    0.29387E+04    1789   0.43086E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1789   0.43086E-02   0.00000E+00 
c  Pressure     0.41867E+00    7023   0.35975E-01   0.19844E+00 
c  k            0.21503E+04    1030   0.69755E-04   0.11504E+01 
c  omega        0.10325E+08     236   0.56361E-04   0.11585E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8879e+05                             3
a  Local Time Step      1.1454e-05                         44462


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9244          1.2196      -0.0011732      1.1918e-06
v  Velocity[Y]                 -15.122          32.958          6.7869          20.056
v  Velocity[Z]                 -32.913          28.782        -0.12396      -0.0036984
v  ǁVelocityǁ                 0.012715          35.637          10.624          20.215
v  Pressure                    -440.91          348.48         -51.572          31.677
v  k                        2.6104e-08          66.561          4.1061          1.6619
v  omega                         1e-24      1.1923e+07          7962.8          11.802
v  turbulent_viscosity      6.5765e-14          1.3023        0.015648         0.11093
v  CourantNb                  0.044408          2456.2          44.287          1.3774
v  FourierNb                  0.010847           15432          93.805          0.6917
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010816        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15492          138.09          2.0691


 TIME FOR THE TIME STEP              392:        0.43684E+02

===============================================================


 INSTANT    0.393000000E+02   TIME STEP NUMBER             393
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.360279839E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30143E+02 0.15261E+02
   Friction velocity        uet   :  0.21508E-02 0.32025E+01
   Friction velocity        uk    :  0.17587E-01 0.29089E+01
   Dimensionless distance   yplus :  0.15679E+00 0.26599E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :        921
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1857   0.45360E-02   0.45181E+00 
c  VelocityY    0.29387E+04    1857   0.45360E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1857   0.45360E-02   0.00000E+00 
c  Pressure     0.43908E+00    7005   0.38446E-01   0.20657E+00 
c  k            0.21572E+04    1100   0.73205E-04   0.12110E+01 
c  omega        0.12488E+08     204   0.21099E-03   0.18979E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -57986                             1
a  Local Time Step      1.1104e-05                         44477


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9837          1.0648     -0.00036469      1.9165e-06
v  Velocity[Y]                 -19.064          30.386          6.8159          20.056
v  Velocity[Z]                 -33.077          28.729       -0.066964      -0.0025167
v  ǁVelocityǁ                 0.021723          34.975          10.653          20.215
v  Pressure                    -457.16          349.26         -51.138          31.574
v  k                        7.8616e-09          65.653          4.1059           1.663
v  omega                         1e-24      8.1428e+07          8379.8          11.838
v  turbulent_viscosity      1.3199e-14          1.2968        0.015715         0.11104
v  CourantNb                  0.025804            2778          44.219          1.3773
v  FourierNb                  0.010848           15317          93.935         0.69325
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010816        0.045673


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15376          138.15          2.0705


 TIME FOR THE TIME STEP              393:        0.44680E+02

===============================================================


 INSTANT    0.394000000E+02   TIME STEP NUMBER             394
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.614305740E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30921E+02 0.15437E+02
   Friction velocity        uet   :  0.94397E-03 0.30124E+01
   Friction velocity        uk    :  0.21861E-01 0.29204E+01
   Dimensionless distance   yplus :  0.11961E+00 0.26743E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :        910
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1924   0.43239E-02   0.42903E+00 
c  VelocityY    0.29387E+04    1924   0.43239E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1924   0.43239E-02   0.00000E+00 
c  Pressure     0.43372E+00    7007   0.36635E-01   0.20538E+00 
c  k            0.21648E+04    1147   0.74454E-04   0.12514E+01 
c  omega        0.28389E+10      43   0.48920E-06   0.83677E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9275e+05                             1
a  Local Time Step      1.0985e-05                         44476


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1645          1.0963        0.000672      2.8743e-06
v  Velocity[Y]                 -23.796          30.223          6.7952          20.057
v  Velocity[Z]                 -33.054          28.568      -0.0036087      -0.0014648
v  ǁVelocityǁ                 0.016563          34.218          10.628          20.215
v  Pressure                    -451.18          349.51         -51.155          31.645
v  k                        9.9066e-08           53.88          4.0813          1.6639
v  omega                         1e-24      4.1385e+07          8388.5          11.861
v  turbulent_viscosity      1.4163e-15          1.2893        0.015754         0.11115
v  CourantNb                  0.062183          2545.6          44.298          1.3773
v  FourierNb                  0.010849           15209          94.816         0.69485
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.149        0.010816        0.045644


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15273          139.11          2.0722


 TIME FOR THE TIME STEP              394:        0.44680E+02

===============================================================


 INSTANT    0.395000000E+02   TIME STEP NUMBER             395
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.201446438E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30864E+02 0.14002E+02
   Friction velocity        uet   :  0.12239E-02 0.28864E+01
   Friction velocity        uk    :  0.19651E-01 0.28629E+01
   Dimensionless distance   yplus :  0.10339E+00 0.27018E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :        947
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    2015   0.42450E-02   0.39910E+00 
c  VelocityY    0.29387E+04    2015   0.42450E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    2015   0.42450E-02   0.00000E+00 
c  Pressure     0.42542E+00    7023   0.32049E-01   0.20092E+00 
c  k            0.21690E+04    1170   0.85539E-04   0.12377E+01 
c  omega        0.14480E+08     243   0.82708E-04   0.66963E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -36680                             1
a  Local Time Step      1.0899e-05                         44488


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4331          1.2367       0.0014281      2.7454e-06
v  Velocity[Y]                 -33.833          30.064          6.7121          20.056
v  Velocity[Z]                 -29.855          28.637        0.042395     -0.00035675
v  ǁVelocityǁ                0.0033634          34.128          10.602          20.216
v  Pressure                     -429.6          349.21         -51.496          31.509
v  k                        1.6312e-08          68.928          4.0668          1.6644
v  omega                         1e-24      3.6839e+07          8352.8          11.883
v  turbulent_viscosity       2.454e-14          1.2808        0.015732         0.11125
v  CourantNb                  0.053417          2010.7          44.274          1.3774
v  FourierNb                  0.010849           15235           95.37         0.69601
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14875        0.010818        0.045667


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15291          139.64          2.0734


 TIME FOR THE TIME STEP              395:        0.45683E+02

===============================================================


 INSTANT    0.396000000E+02   TIME STEP NUMBER             396
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.295175332E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30186E+02 0.23411E+02
   Friction velocity        uet   :  0.10345E-02 0.29985E+01
   Friction velocity        uk    :  0.16985E-01 0.31029E+01
   Dimensionless distance   yplus :  0.17784E+00 0.27267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        357
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    2003   0.45338E-02   0.37689E+00 
c  VelocityY    0.29386E+04    2003   0.45338E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    2003   0.45338E-02   0.00000E+00 
c  Pressure     0.39852E+00    6980   0.31779E-01   0.18752E+00 
c  k            0.21658E+04    1154   0.10560E-03   0.11149E+01 
c  omega        0.12137E+08     348   0.50272E-04   0.36504E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1914e+05                             1
a  Local Time Step       1.063e-05                         44492


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5846          1.3229       0.0018045      1.9882e-06
v  Velocity[Y]                 -24.455          30.072          6.6313          20.056
v  Velocity[Z]                 -28.536          28.726        0.064774      0.00044733
v  ǁVelocityǁ                 0.011362          33.899          10.611          20.215
v  Pressure                    -417.14          347.52         -52.578          31.379
v  k                        9.5106e-07          96.761          4.0929          1.6647
v  omega                         1e-24      2.0085e+07          8188.3          11.916
v  turbulent_viscosity      2.1313e-14          1.2732        0.015688         0.11135
v  CourantNb                  0.022979          2013.8          44.279          1.3774
v  FourierNb                  0.010848           15188          95.191         0.69691
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1491        0.010819        0.045664


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15248          139.47          2.0743


 TIME FOR THE TIME STEP              396:        0.45998E+02

===============================================================


 INSTANT    0.397000000E+02   TIME STEP NUMBER             397
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.441982520E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45128E+02 0.15904E+02
   Friction velocity        uet   :  0.86297E-03 0.29203E+01
   Friction velocity        uk    :  0.17586E-01 0.39886E+01
   Dimensionless distance   yplus :  0.18255E+00 0.32923E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        354
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2037   0.45362E-02   0.36360E+00 
c  VelocityY    0.29385E+04    2037   0.45362E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2037   0.45362E-02   0.00000E+00 
c  Pressure     0.40080E+00    6987   0.36646E-01   0.18948E+00 
c  k            0.21562E+04    1228   0.11502E-03   0.95664E+00 
c  omega        0.10503E+08     511   0.41594E-04   0.23886E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -67273                             1
a  Local Time Step      1.0622e-05                         44482


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6246          1.3526       0.0018482      1.4453e-06
v  Velocity[Y]                 -35.668          30.342          6.6227          20.056
v  Velocity[Z]                 -28.579          28.453        0.083793       0.0012316
v  ǁVelocityǁ                0.0085279          36.661          10.604          20.215
v  Pressure                    -418.27          346.26          -53.93          31.771
v  k                         2.731e-09          116.43          4.1084          1.6648
v  omega                         1e-24      1.3118e+07          8151.7          11.927
v  turbulent_viscosity      1.9652e-13          1.2643        0.015643         0.11145
v  CourantNb                  0.021261          2014.7          44.526          1.3775
v  FourierNb                  0.010848           15108          94.745         0.69773
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14852         0.01082        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78498           15169          139.27          2.0752


 TIME FOR THE TIME STEP              397:        0.45903E+02

===============================================================


 INSTANT    0.398000000E+02   TIME STEP NUMBER             398
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.859358931E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38140E+02 0.14705E+02
   Friction velocity        uet   :  0.13090E-02 0.34139E+01
   Friction velocity        uk    :  0.22476E-01 0.35835E+01
   Dimensionless distance   yplus :  0.19090E+00 0.34153E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        388
   Nb of faces within the viscous sub-layer     :       1061
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2045   0.43848E-02   0.34947E+00 
c  VelocityY    0.29383E+04    2045   0.43848E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2045   0.43848E-02   0.00000E+00 
c  Pressure     0.41573E+00    7078   0.39777E-01   0.19701E+00 
c  k            0.21449E+04    1240   0.91289E-04   0.85302E+00 
c  omega        0.10313E+08     386   0.72636E-04   0.43677E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4054e+05                             2
a  Local Time Step      1.0678e-05                         44433


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5972          1.3293       0.0019354      2.5002e-06
v  Velocity[Y]                 -20.057          30.934          6.6409          20.057
v  Velocity[Z]                 -29.066          28.543        0.080757       0.0018108
v  ǁVelocityǁ                 0.012185          33.773          10.572          20.216
v  Pressure                    -418.47          344.94         -55.366          31.867
v  k                        2.2014e-09          131.33          4.0963          1.6647
v  omega                         1e-24      2.5433e+07          8259.2           11.92
v  turbulent_viscosity      1.2033e-15          1.2566        0.015639         0.11153
v  CourantNb                 0.0052563          3155.7          44.974          1.3775
v  FourierNb                  0.010849           15052          94.094         0.69852
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14849        0.010823        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7917           15116          139.07           2.076


 TIME FOR THE TIME STEP              398:        0.47835E+02

===============================================================


 INSTANT    0.399000000E+02   TIME STEP NUMBER             399
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.184280587E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30644E+02 0.13754E+02
   Friction velocity        uet   :  0.13251E-02 0.27902E+01
   Friction velocity        uk    :  0.23168E-01 0.32931E+01
   Dimensionless distance   yplus :  0.10372E+00 0.32533E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        432
   Nb of faces within the viscous sub-layer     :       1086
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    2055   0.44575E-02   0.34530E+00 
c  VelocityY    0.29381E+04    2055   0.44575E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    2055   0.44575E-02   0.00000E+00 
c  Pressure     0.43456E+00    7057   0.36260E-01   0.20532E+00 
c  k            0.21347E+04    1280   0.63523E-04   0.71994E+00 
c  omega        0.11401E+08     272   0.22443E-03   0.22893E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8724e+05                             1
a  Local Time Step      1.0904e-05                         44386


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.557          1.2732       0.0022092      2.0796e-06
v  Velocity[Y]                 -17.714          32.958          6.6681          20.056
v  Velocity[Z]                 -28.717          28.614        0.052223       0.0024939
v  ǁVelocityǁ                 0.014589          34.132          10.534          20.216
v  Pressure                    -417.86          343.77         -56.066          31.774
v  k                        6.7918e-10          109.56          4.1253          1.6643
v  omega                         1e-24      4.9875e+07          9143.6          11.961
v  turbulent_viscosity      2.6997e-15           1.249        0.015656          0.1116
v  CourantNb                  0.053976          2555.5          44.828          1.3773
v  FourierNb                  0.010849           15049          94.102         0.69922
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14861        0.010825        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91938           15115          138.93          2.0765


 TIME FOR THE TIME STEP              399:        0.47836E+02

===============================================================


 INSTANT    0.400000000E+02   TIME STEP NUMBER             400
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.573514296E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31210E+02 0.13540E+02
   Friction velocity        uet   :  0.11396E-02 0.29787E+01
   Friction velocity        uk    :  0.20039E-01 0.35117E+01
   Dimensionless distance   yplus :  0.11627E+00 0.40350E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        557
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    2059   0.44783E-02   0.34534E+00 
c  VelocityY    0.29381E+04    2059   0.44783E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    2059   0.44783E-02   0.00000E+00 
c  Pressure     0.42443E+00    6985   0.33497E-01   0.20121E+00 
c  k            0.21258E+04    1268   0.67124E-04   0.77832E+00 
c  omega        0.24143E+08     345   0.19653E-03   0.55856E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8364e+05                             2
a  Local Time Step      1.1236e-05                         44373


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5798          1.2324       0.0024486      2.5619e-06
v  Velocity[Y]                 -16.376          34.053          6.7004          20.056
v  Velocity[Z]                 -28.533          29.093       0.0084419       0.0028458
v  ǁVelocityǁ                 0.012655          34.216          10.494          20.216
v  Pressure                    -413.65          342.49         -56.404          31.612
v  k                        7.3642e-10          69.458          4.1204          1.6636
v  omega                         1e-24      1.2998e+08          9523.9          11.946
v  turbulent_viscosity      1.3163e-15          1.2412        0.015701         0.11165
v  CourantNb                  0.025327          2025.1          44.463          1.3771
v  FourierNb                  0.010848           15015          95.772         0.70037
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14878        0.010825         0.04575


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15082          140.24          2.0775


 TIME FOR THE TIME STEP              400:        0.48420E+02

===============================================================


 INSTANT    0.401000000E+02   TIME STEP NUMBER             401
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.234692316E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31927E+02 0.16517E+02
   Friction velocity        uet   :  0.89365E-03 0.29559E+01
   Friction velocity        uk    :  0.16295E-01 0.36967E+01
   Dimensionless distance   yplus :  0.20076E+00 0.42476E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        522
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2021   0.44177E-02   0.35623E+00 
c  VelocityY    0.29380E+04    2021   0.44177E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2021   0.44177E-02   0.00000E+00 
c  Pressure     0.43479E+00    6981   0.31846E-01   0.20676E+00 
c  k            0.21163E+04    1154   0.67319E-04   0.77432E+00 
c  omega        0.95148E+08     207   0.22697E-04   0.14971E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -17563                             1
a  Local Time Step      1.1374e-05                         44330


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5974          1.2091        0.002687      2.7327e-06
v  Velocity[Y]                 -15.247          33.819          6.7028          20.056
v  Velocity[Z]                 -28.696          28.784       -0.037799        0.002844
v  ǁVelocityǁ                0.0086498          34.398          10.471          20.216
v  Pressure                    -397.95          341.26         -56.736          31.284
v  k                         2.109e-08          45.085          4.0935          1.6626
v  omega                         1e-24       6.535e+07          8759.6          11.889
v  turbulent_viscosity        1.77e-15          1.2338        0.015737         0.11168
v  CourantNb                  0.030479          2028.1          44.233           1.377
v  FourierNb                  0.010848           14967          97.209         0.70156
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14929        0.010825        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15036          141.44          2.0785


 TIME FOR THE TIME STEP              401:        0.46357E+02

===============================================================


 INSTANT    0.402000000E+02   TIME STEP NUMBER             402
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.258044832E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32108E+02 0.23721E+02
   Friction velocity        uet   :  0.46558E-03 0.27710E+01
   Friction velocity        uk    :  0.82200E-02 0.32189E+01
   Dimensionless distance   yplus :  0.73927E-01 0.40458E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        568
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2052   0.44267E-02   0.35830E+00 
c  VelocityY    0.29378E+04    2052   0.44267E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2052   0.44267E-02   0.00000E+00 
c  Pressure     0.41084E+00    6974   0.30443E-01   0.19570E+00 
c  k            0.21066E+04    1281   0.58838E-04   0.72397E+00 
c  omega        0.26910E+08     248   0.40348E-04   0.49961E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0855e-05                         44337


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5214          1.1895       0.0024288      1.9491e-06
v  Velocity[Y]                  -15.08          32.542          6.6839          20.056
v  Velocity[Z]                 -28.416          29.061       -0.073438       0.0027657
v  ǁVelocityǁ                 0.013488          33.105           10.46          20.215
v  Pressure                    -384.41          340.81          -56.82          30.856
v  k                        3.0333e-08          40.206           4.084          1.6614
v  omega                         1e-24      3.3411e+07          8420.1          11.875
v  turbulent_viscosity      1.3611e-14          1.2276        0.015748         0.11169
v  CourantNb                  0.027957          2032.2          43.984           1.377
v  FourierNb                  0.010847           14880          96.923         0.70195
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010825        0.045769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14950          140.91          2.0789


 TIME FOR THE TIME STEP              402:        0.46239E+02

===============================================================


 INSTANT    0.403000000E+02   TIME STEP NUMBER             403
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.107995187E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31432E+02 0.21255E+02
   Friction velocity        uet   :  0.19371E-02 0.26556E+01
   Friction velocity        uk    :  0.13701E-01 0.30592E+01
   Dimensionless distance   yplus :  0.96011E-01 0.30974E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        527
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    2042   0.44387E-02   0.36612E+00 
c  VelocityY    0.29377E+04    2042   0.44387E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    2042   0.44387E-02   0.00000E+00 
c  Pressure     0.41248E+00    7027   0.28465E-01   0.19711E+00 
c  k            0.20983E+04    1446   0.59056E-04   0.79455E+00 
c  omega        0.12669E+08     210   0.11261E-03   0.63961E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4008e+05                             1
a  Local Time Step      1.0779e-05                         44351


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3466          1.2194       0.0021818      2.6587e-06
v  Velocity[Y]                 -14.446          30.527          6.6931          20.056
v  Velocity[Z]                 -30.385          28.936       -0.088424       0.0023335
v  ǁVelocityǁ                 0.018383          35.381          10.472          20.215
v  Pressure                    -364.35          342.71         -55.705           30.81
v  k                        7.3989e-08          44.674            4.09            1.66
v  omega                         1e-24      4.5663e+07          8313.1          11.854
v  turbulent_viscosity        1.07e-15          1.2221        0.015772         0.11167
v  CourantNb                  0.031218          2035.6          43.892           1.377
v  FourierNb                  0.010847           14867          96.202         0.70215
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010826         0.04575


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14936          140.09          2.0792


 TIME FOR THE TIME STEP              403:        0.45119E+02

===============================================================


 INSTANT    0.404000000E+02   TIME STEP NUMBER             404
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.320774851E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31422E+02 0.20433E+02
   Friction velocity        uet   :  0.27007E-02 0.29412E+01
   Friction velocity        uk    :  0.10770E-01 0.31619E+01
   Dimensionless distance   yplus :  0.10079E+00 0.26501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        461
   Nb of faces within the viscous sub-layer     :        990
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29376E+04    2097   0.43711E-02   0.36208E+00 
c  VelocityY    0.29376E+04    2097   0.43711E-02   0.00000E+00 
c  VelocityZ    0.29376E+04    2097   0.43711E-02   0.00000E+00 
c  Pressure     0.45004E+00    7047   0.29594E-01   0.21443E+00 
c  k            0.20928E+04    1506   0.60925E-04   0.93794E+00 
c  omega        0.18935E+28       2   0.46197E-23   0.17334E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1394e-05                         44345


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0713          1.2452        0.002417      1.2413e-08
v  Velocity[Y]                 -15.033          30.514          6.7284          20.056
v  Velocity[Z]                 -32.363          28.907        -0.09915       0.0021654
v  ǁVelocityǁ                 0.010759          36.944          10.505          20.215
v  Pressure                    -379.81           345.1         -54.249          31.005
v  k                        4.5788e-08          55.955          4.1119          1.6585
v  omega                         1e-24      9.7212e+07          8474.5          11.835
v  turbulent_viscosity      3.4096e-14          1.2167        0.015824         0.11163
v  CourantNb                  0.058256          2036.8          44.036          1.3769
v  FourierNb                  0.010846           14935          95.142          0.7022
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14912        0.010826        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88934           15003          139.18          2.0791


 TIME FOR THE TIME STEP              404:        0.46172E+02

===============================================================


 INSTANT    0.405000000E+02   TIME STEP NUMBER             405
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.383053693E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30592E+02 0.14953E+02
   Friction velocity        uet   :  0.12799E-02 0.31398E+01
   Friction velocity        uk    :  0.13462E-01 0.29233E+01
   Dimensionless distance   yplus :  0.11712E+00 0.26909E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1050
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29377E+04    2157   0.45237E-02   0.35714E+00 
c  VelocityY    0.29377E+04    2157   0.45237E-02   0.00000E+00 
c  VelocityZ    0.29377E+04    2157   0.45237E-02   0.00000E+00 
c  Pressure     0.41340E+00    7094   0.32927E-01   0.19473E+00 
c  k            0.20935E+04    1546   0.70925E-04   0.11318E+01 
c  omega        0.39410E+08     220   0.32423E-04   0.48260E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66883                             1
a  Local Time Step      1.1126e-05                         44309


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7273          1.2766       0.0030817     -1.8753e-06
v  Velocity[Y]                 -15.127          30.355          6.7875          20.056
v  Velocity[Z]                 -33.177          29.101       -0.079332       0.0017583
v  ǁVelocityǁ                0.0088839          35.654          10.575          20.215
v  Pressure                    -431.25           346.9         -52.889          31.261
v  k                        5.1905e-11          65.243          4.1321          1.6569
v  omega                         1e-24      4.9192e+07          8213.4          11.853
v  turbulent_viscosity      7.3764e-14          1.2133        0.015871         0.11157
v  CourantNb                  0.021628          2202.9          44.042          1.3766
v  FourierNb                  0.010845           15326          95.036         0.70211
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14893        0.010827        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76184           15380          139.08          2.0787


 TIME FOR THE TIME STEP              405:        0.48996E+02

===============================================================


 INSTANT    0.406000000E+02   TIME STEP NUMBER             406
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.236255952E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31029E+02 0.14098E+02
   Friction velocity        uet   :  0.14545E-02 0.30736E+01
   Friction velocity        uk    :  0.96973E-02 0.29399E+01
   Dimensionless distance   yplus :  0.14602E+00 0.27080E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1069
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2198   0.43308E-02   0.36090E+00 
c  VelocityY    0.29378E+04    2198   0.43308E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2198   0.43308E-02   0.00000E+00 
c  Pressure     0.46991E+00    7047   0.36952E-01   0.22284E+00 
c  k            0.21026E+04    1418   0.73706E-04   0.11691E+01 
c  omega        0.14384E+08     200   0.17675E-03   0.17932E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7001e+05                             1
a  Local Time Step      1.0863e-05                         44308


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3582          1.2923        0.003306     -1.7472e-06
v  Velocity[Y]                 -19.328          30.197          6.8512          20.056
v  Velocity[Z]                 -32.584          28.934       -0.027287       0.0012832
v  ǁVelocityǁ                 0.006538          34.553          10.635          20.215
v  Pressure                    -450.94          347.74         -51.808           31.63
v  k                        1.4846e-08          68.021          4.1176           1.655
v  omega                         1e-24      6.9344e+07          8679.4          11.886
v  turbulent_viscosity      1.5211e-16          1.2122        0.015904         0.11149
v  CourantNb                  0.034485          2633.7          44.139          1.3765
v  FourierNb                  0.010845           15524          94.855         0.70174
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010826        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15581          138.99          2.0782


 TIME FOR THE TIME STEP              406:        0.49278E+02

===============================================================


 INSTANT    0.407000000E+02   TIME STEP NUMBER             407
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.512636913E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30183E+02 0.14132E+02
   Friction velocity        uet   :  0.13107E-02 0.29780E+01
   Friction velocity        uk    :  0.19474E-01 0.32010E+01
   Dimensionless distance   yplus :  0.13182E+00 0.27177E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        414
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2240   0.44682E-02   0.35169E+00 
c  VelocityY    0.29378E+04    2240   0.44682E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2240   0.44682E-02   0.00000E+00 
c  Pressure     0.43134E+00    7070   0.37566E-01   0.20318E+00 
c  k            0.21144E+04    1246   0.78355E-04   0.12004E+01 
c  omega        0.30438E+08     160   0.43766E-04   0.67199E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1037e+05                             3
a  Local Time Step      1.1254e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5016          1.3292       0.0025169     -3.4141e-06
v  Velocity[Y]                 -25.769          30.006          6.8805          20.056
v  Velocity[Z]                 -31.041          28.762        0.037094      0.00083261
v  ǁVelocityǁ                0.0070568            32.3          10.645          20.215
v  Pressure                    -449.49          347.62         -51.411          31.543
v  k                        2.3754e-08          59.499            4.09          1.6529
v  omega                         1e-24      3.5429e+07          8391.5          11.873
v  turbulent_viscosity       4.343e-14          1.2171        0.015924         0.11139
v  CourantNb                  0.027288          2591.1          44.286          1.3765
v  FourierNb                  0.010844           15629          95.489         0.70143
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14851        0.010826        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15691          139.78          2.0779


 TIME FOR THE TIME STEP              407:        0.47322E+02

===============================================================


 INSTANT    0.408000000E+02   TIME STEP NUMBER             408
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.389377886E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30372E+02 0.13762E+02
   Friction velocity        uet   :  0.12413E-02 0.27318E+01
   Friction velocity        uk    :  0.11014E-01 0.29412E+01
   Dimensionless distance   yplus :  0.13314E+00 0.26913E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        344
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2210   0.45505E-02   0.31501E+00 
c  VelocityY    0.29380E+04    2210   0.45505E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2210   0.45505E-02   0.00000E+00 
c  Pressure     0.40941E+00    7093   0.35039E-01   0.19341E+00 
c  k            0.21236E+04    1197   0.77091E-04   0.12115E+01 
c  omega        0.16574E+08     216   0.66158E-04   0.71082E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6705e+05                             1
a  Local Time Step      1.1364e-05                         44402


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.503          1.5864       0.0021961     -2.9729e-06
v  Velocity[Y]                 -29.341          29.837          6.8342          20.057
v  Velocity[Z]                 -31.267          28.579        0.093128     -2.2929e-05
v  ǁVelocityǁ                 0.012766          33.025          10.611          20.216
v  Pressure                    -430.83          347.54         -50.925          31.769
v  k                        9.6111e-09          55.178          4.0621          1.6505
v  omega                         1e-24      3.3694e+07          8519.7          11.887
v  turbulent_viscosity      3.0576e-14          1.2247        0.015894         0.11126
v  CourantNb                 0.0071032          2024.4          44.504          1.3766
v  FourierNb                  0.010844           15685          95.647         0.70057
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14787        0.010825        0.045669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15756          140.15          2.0772


 TIME FOR THE TIME STEP              408:        0.46829E+02

===============================================================


 INSTANT    0.409000000E+02   TIME STEP NUMBER             409
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.690272957E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30101E+02 0.20778E+02
   Friction velocity        uet   :  0.22686E-02 0.27501E+01
   Friction velocity        uk    :  0.13615E-01 0.29227E+01
   Dimensionless distance   yplus :  0.11692E+00 0.26864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        323
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2184   0.45136E-02   0.29228E+00 
c  VelocityY    0.29380E+04    2184   0.45136E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2184   0.45136E-02   0.00000E+00 
c  Pressure     0.43037E+00    6853   0.31793E-01   0.20411E+00 
c  k            0.21253E+04    1236   0.93241E-04   0.11079E+01 
c  omega        0.13821E+08     262   0.39844E-04   0.34248E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -94899                             1
a  Local Time Step      1.1337e-05                         44386


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3478          1.7659       0.0022955     -8.6931e-07
v  Velocity[Y]                  -23.48          29.762          6.7478          20.057
v  Velocity[Z]                 -29.429          28.728         0.11606     -0.00087464
v  ǁVelocityǁ                 0.015742          33.178          10.603          20.216
v  Pressure                    -407.44           346.2         -51.309          31.764
v  k                        1.3341e-08          85.103          4.0836          1.6479
v  omega                         1e-24      1.7139e+07          8189.1          11.864
v  turbulent_viscosity      2.8719e-14          1.2328        0.015842         0.11111
v  CourantNb                 0.0069261          2014.1          44.573          1.3765
v  FourierNb                  0.010844           15720          95.083         0.69956
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010824        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15784          139.66          2.0761


 TIME FOR THE TIME STEP              409:        0.45761E+02

===============================================================


 INSTANT    0.410000000E+02   TIME STEP NUMBER             410
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.112376283E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29937E+02 0.18235E+02
   Friction velocity        uet   :  0.28481E-03 0.25172E+01
   Friction velocity        uk    :  0.17854E-01 0.36781E+01
   Dimensionless distance   yplus :  0.10105E+00 0.33303E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        363
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29379E+04    2121   0.44329E-02   0.28425E+00 
c  VelocityY    0.29379E+04    2121   0.44329E-02   0.00000E+00 
c  VelocityZ    0.29379E+04    2121   0.44329E-02   0.00000E+00 
c  Pressure     0.42788E+00    7050   0.33412E-01   0.20226E+00 
c  k            0.21197E+04    1359   0.11058E-03   0.95221E+00 
c  omega        0.10833E+08     451   0.31626E-04   0.16818E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2455e+05                             1
a  Local Time Step      1.0758e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.255          1.8271       0.0020272      1.2148e-06
v  Velocity[Y]                 -39.189          30.224          6.7177          20.057
v  Velocity[Z]                 -28.792          28.507         0.13304      -0.0015735
v  ǁVelocityǁ                 0.011302           39.41          10.585          20.216
v  Pressure                    -409.49          345.28         -52.192          31.896
v  k                        6.7282e-09           88.58          4.1024          1.6453
v  omega                         1e-24      1.1809e+07          8022.4          11.869
v  turbulent_viscosity      7.7203e-14          1.2387        0.015795         0.11095
v  CourantNb                  0.020306          2010.7          44.743          1.3766
v  FourierNb                  0.010843           15730          94.508          0.6986
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010825        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15795          139.25          2.0752


 TIME FOR THE TIME STEP              410:        0.47180E+02

===============================================================


 INSTANT    0.411000000E+02   TIME STEP NUMBER             411
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.622791562E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45142E+02 0.13578E+02
   Friction velocity        uet   :  0.82618E-03 0.36343E+01
   Friction velocity        uk    :  0.20727E-01 0.42301E+01
   Dimensionless distance   yplus :  0.11862E+00 0.38481E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        375
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29378E+04    2092   0.45193E-02   0.27875E+00 
c  VelocityY    0.29378E+04    2092   0.45193E-02   0.00000E+00 
c  VelocityZ    0.29378E+04    2092   0.45193E-02   0.00000E+00 
c  Pressure     0.41948E+00    7021   0.37089E-01   0.19763E+00 
c  k            0.21114E+04    1398   0.10493E-03   0.84992E+00 
c  omega        0.10310E+08     375   0.12932E-03   0.57304E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -47988                             1
a  Local Time Step      1.0445e-05                         44330


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2014          1.8357       0.0015445      3.5294e-06
v  Velocity[Y]                 -25.947          30.663          6.7196          20.055
v  Velocity[Z]                 -28.658          28.504         0.13023      -0.0022774
v  ǁVelocityǁ                0.0080102          33.629          10.557          20.215
v  Pressure                     -410.2          344.78          -53.25          32.018
v  k                        8.2142e-09          42.209          4.0623          1.6428
v  omega                         1e-24      5.3023e+07          8230.9           11.89
v  turbulent_viscosity       8.966e-15          1.2463        0.015764         0.11078
v  CourantNb                  0.040804            3140          45.146          1.3767
v  FourierNb                  0.010844           15738          93.557         0.69737
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010825        0.045775


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15816           138.7          2.0741


 TIME FOR THE TIME STEP              411:        0.45984E+02

===============================================================


 INSTANT    0.412000000E+02   TIME STEP NUMBER             412
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.105417370E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30832E+02 0.14445E+02
   Friction velocity        uet   :  0.14130E-02 0.28996E+01
   Friction velocity        uk    :  0.23993E-01 0.31612E+01
   Dimensionless distance   yplus :  0.13525E+00 0.27102E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2018   0.45601E-02   0.27824E+00 
c  VelocityY    0.29380E+04    2018   0.45601E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2018   0.45601E-02   0.00000E+00 
c  Pressure     0.44601E+00    7124   0.36855E-01   0.21199E+00 
c  k            0.21038E+04    1369   0.60186E-04   0.69299E+00 
c  omega        0.15247E+08     237   0.47204E-04   0.66646E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7949e+05                             1
a  Local Time Step      1.1031e-05                         44311


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4977          1.6419       0.0011004      3.0243e-06
v  Velocity[Y]                 -17.523          31.494          6.7256          20.056
v  Velocity[Z]                 -28.536          28.709        0.098933      -0.0029662
v  ǁVelocityǁ                0.0036423          33.689          10.521          20.216
v  Pressure                     -410.1          344.38         -53.838           32.23
v  k                        1.3732e-08          45.701          4.0714          1.6403
v  omega                         1e-24      2.7649e+07          8457.5          11.928
v  turbulent_viscosity      4.8834e-15          1.2559        0.015742         0.11059
v  CourantNb                  0.049437          2852.9          45.077          1.3766
v  FourierNb                  0.010845           15714          92.476         0.69569
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14907        0.010823        0.045745


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15786          137.55          2.0723


 TIME FOR THE TIME STEP              412:        0.45587E+02

===============================================================


 INSTANT    0.413000000E+02   TIME STEP NUMBER             413
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.728135991E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31718E+02 0.14376E+02
   Friction velocity        uet   :  0.19773E-02 0.29200E+01
   Friction velocity        uk    :  0.26075E-01 0.29733E+01
   Dimensionless distance   yplus :  0.10099E+00 0.28394E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        572
   Nb of faces within the viscous sub-layer     :       1060
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1920   0.44978E-02   0.29394E+00 
c  VelocityY    0.29382E+04    1920   0.44978E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1920   0.44978E-02   0.00000E+00 
c  Pressure     0.43608E+00    7038   0.34195E-01   0.20733E+00 
c  k            0.20979E+04    1252   0.61231E-04   0.66935E+00 
c  omega        0.11642E+08     247   0.22714E-03   0.26962E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -9648.7                             1
a  Local Time Step      1.0986e-05                         44302


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5628           1.337      0.00087066      2.8192e-06
v  Velocity[Y]                 -16.933          33.185          6.7417          20.056
v  Velocity[Z]                 -28.488          28.689        0.044794      -0.0038699
v  ǁVelocityǁ                 0.014028           33.72          10.496          20.216
v  Pressure                    -407.48          344.81         -53.772          32.073
v  k                        1.0416e-07          51.151          4.1041           1.638
v  omega                         1e-24       6.464e+07          9265.2          11.957
v  turbulent_viscosity      1.2438e-14          1.2637         0.01576          0.1104
v  CourantNb                  0.050304          2052.4          44.649          1.3764
v  FourierNb                  0.010845           15654           92.92         0.69475
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010821        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15719          137.57          2.0711


 TIME FOR THE TIME STEP              413:        0.43825E+02

===============================================================


 INSTANT    0.414000000E+02   TIME STEP NUMBER             414
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.116461538E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31631E+02 0.14560E+02
   Friction velocity        uet   :  0.45979E-03 0.29266E+01
   Friction velocity        uk    :  0.24449E-01 0.29296E+01
   Dimensionless distance   yplus :  0.96486E-01 0.32123E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        532
   Nb of faces within the viscous sub-layer     :       1050
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1857   0.45657E-02   0.31669E+00 
c  VelocityY    0.29382E+04    1857   0.45657E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1857   0.45657E-02   0.00000E+00 
c  Pressure     0.42084E+00    6921   0.32431E-01   0.19929E+00 
c  k            0.20931E+04    1025   0.65982E-04   0.74547E+00 
c  omega        0.30982E+08     279   0.37604E-04   0.82100E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0932e-05                         44310


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.598          1.2025      0.00074139      7.5974e-07
v  Velocity[Y]                 -15.151          32.968          6.7643          20.056
v  Velocity[Z]                 -28.409          29.138       -0.018134      -0.0045439
v  ǁVelocityǁ                0.0098791          33.771          10.487          20.216
v  Pressure                    -396.28           343.6         -54.365            31.7
v  k                        1.4741e-08          48.372          4.0964          1.6359
v  omega                         1e-24      3.3247e+07          8664.9          11.912
v  turbulent_viscosity      1.6692e-13          1.2704        0.015795         0.11019
v  CourantNb                  0.028662          2049.7          44.153          1.3762
v  FourierNb                  0.010846           15585          94.842         0.69465
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14901        0.010821        0.045744


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15643          138.99          2.0708


 TIME FOR THE TIME STEP              414:        0.42614E+02

===============================================================


 INSTANT    0.415000000E+02   TIME STEP NUMBER             415
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.295415314E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31154E+02 0.16476E+02
   Friction velocity        uet   :  0.55002E-03 0.28079E+01
   Friction velocity        uk    :  0.11875E-01 0.32040E+01
   Dimensionless distance   yplus :  0.86217E-01 0.36252E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        528
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    1843   0.46522E-02   0.33611E+00 
c  VelocityY    0.29380E+04    1843   0.46522E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    1843   0.46522E-02   0.00000E+00 
c  Pressure     0.46808E+00    6957   0.30398E-01   0.21987E+00 
c  k            0.20886E+04    1221   0.64904E-04   0.70076E+00 
c  omega        0.13391E+08     322   0.65656E-04   0.42022E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6264e+05                             2
a  Local Time Step      1.1429e-05                         44343


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5556          1.0924      0.00091983      9.9987e-07
v  Velocity[Y]                 -15.242          32.551          6.7507          20.056
v  Velocity[Z]                 -28.507          28.961       -0.075147      -0.0054438
v  ǁVelocityǁ                  0.01533           33.32          10.489          20.216
v  Pressure                    -379.72           343.7         -54.879          31.167
v  k                        2.1321e-09          41.071          4.0797           1.634
v  omega                         1e-24      2.5109e+07          8480.6          11.881
v  turbulent_viscosity      2.7499e-14          1.2759        0.015814         0.10999
v  CourantNb                   0.05105          2040.1          44.014          1.3762
v  FourierNb                  0.010846           15543          95.098         0.69404
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14806        0.010822         0.04579


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15598          139.11          2.0703


 TIME FOR THE TIME STEP              415:        0.42672E+02

===============================================================


 INSTANT    0.416000000E+02   TIME STEP NUMBER             416
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.424637986E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30146E+02 0.20329E+02
   Friction velocity        uet   :  0.12382E-02 0.26621E+01
   Friction velocity        uk    :  0.14246E-01 0.31466E+01
   Dimensionless distance   yplus :  0.97230E-01 0.31925E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1961   0.46642E-02   0.34696E+00 
c  VelocityY    0.29381E+04    1961   0.46642E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1961   0.46642E-02   0.00000E+00 
c  Pressure     0.44524E+00    7006   0.29021E-01   0.21104E+00 
c  k            0.20852E+04    1394   0.58106E-04   0.74070E+00 
c  omega        0.11344E+08     235   0.61185E-03   0.13214E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0822e-05                         44344


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6148          1.0931       0.0010979     -2.3284e-07
v  Velocity[Y]                 -15.126          30.642          6.7468          20.056
v  Velocity[Z]                     -30          28.799         -0.1018      -0.0061852
v  ǁVelocityǁ                0.0077626           34.55          10.493          20.215
v  Pressure                    -365.24          345.07         -54.635          31.044
v  k                        3.3627e-09          40.724           4.071          1.6325
v  omega                         1e-24      3.0077e+08          9327.6          11.907
v  turbulent_viscosity      1.6751e-15          1.2802        0.015818         0.10978
v  CourantNb                  0.030199          2028.9          43.894          1.3764
v  FourierNb                  0.010846           15504            94.1         0.69253
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010821        0.045754


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15559          137.99          2.0689


 TIME FOR THE TIME STEP              416:        0.47706E+02

===============================================================


 INSTANT    0.417000000E+02   TIME STEP NUMBER             417
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.334146474E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30908E+02 0.19814E+02
   Friction velocity        uet   :  0.87525E-03 0.28019E+01
   Friction velocity        uk    :  0.10263E-01 0.32046E+01
   Dimensionless distance   yplus :  0.88062E-01 0.27437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2008   0.46481E-02   0.36035E+00 
c  VelocityY    0.29380E+04    2008   0.46481E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2008   0.46481E-02   0.00000E+00 
c  Pressure     0.42008E+00    6982   0.29133E-01   0.19905E+00 
c  k            0.20842E+04    1378   0.60375E-04   0.86579E+00 
c  omega        0.35221E+09     106   0.79658E-05   0.33227E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1606e+05                             1
a  Local Time Step      1.1796e-05                         44311


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7955          1.3181      0.00099638     -7.7509e-07
v  Velocity[Y]                 -15.186          30.654          6.7669          20.055
v  Velocity[Z]                 -31.256          28.843        -0.11903       -0.006228
v  ǁVelocityǁ                 0.010232          36.343          10.506          20.215
v  Pressure                    -355.95           347.5         -53.054          31.121
v  k                        2.6554e-08          52.955          4.0897          1.6313
v  omega                         1e-24      1.5056e+08          8581.6          11.855
v  turbulent_viscosity       1.082e-14          1.2827        0.015832         0.10958
v  CourantNb                  0.050351          2037.5          44.074          1.3766
v  FourierNb                  0.010846           15515          93.266         0.69106
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14719        0.010821        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9045           15573          137.34          2.0676


 TIME FOR THE TIME STEP              417:        0.45370E+02

===============================================================


 INSTANT    0.418000000E+02   TIME STEP NUMBER             418
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.141856843E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30847E+02 0.18032E+02
   Friction velocity        uet   :  0.29392E-02 0.30493E+01
   Friction velocity        uk    :  0.10362E-01 0.31980E+01
   Dimensionless distance   yplus :  0.92780E-01 0.27155E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    2004   0.46829E-02   0.36200E+00 
c  VelocityY    0.29380E+04    2004   0.46829E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    2004   0.46829E-02   0.00000E+00 
c  Pressure     0.41947E+00    6993   0.32978E-01   0.19686E+00 
c  k            0.20872E+04    1297   0.70742E-04   0.10319E+01 
c  omega        0.88584E+08     163   0.16658E-04   0.98354E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -38336                             1
a  Local Time Step      1.0796e-05                         44334


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0427          1.4889      0.00081843     -5.5916e-07
v  Velocity[Y]                 -15.033          32.531          6.8022          20.056
v  Velocity[Z]                   -33.1          28.533        -0.12273      -0.0064448
v  ǁVelocityǁ                 0.019849          37.258          10.546          20.216
v  Pressure                    -405.92          348.69         -51.684          31.376
v  k                        6.1722e-08          63.755          4.1046          1.6304
v  omega                         1e-24      7.5653e+07          8371.1          11.865
v  turbulent_viscosity      3.8495e-15          1.2856        0.015875         0.10938
v  CourantNb                 0.0087241          2146.9          44.094          1.3765
v  FourierNb                  0.010847           15618          93.605         0.69017
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814        0.010822        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15681           137.7          2.0667


 TIME FOR THE TIME STEP              418:        0.45559E+02

===============================================================


 INSTANT    0.419000000E+02   TIME STEP NUMBER             419
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.107174252E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29729E+02 0.15469E+02
   Friction velocity        uet   :  0.15826E-02 0.31480E+01
   Friction velocity        uk    :  0.17151E-01 0.30664E+01
   Dimensionless distance   yplus :  0.11837E+00 0.27038E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    2031   0.44878E-02   0.37075E+00 
c  VelocityY    0.29381E+04    2031   0.44878E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    2031   0.44878E-02   0.00000E+00 
c  Pressure     0.43453E+00    7076   0.37426E-01   0.20515E+00 
c  k            0.20963E+04    1320   0.76815E-04   0.11463E+01 
c  omega        0.24328E+08     155   0.33921E-04   0.29347E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -85786                             1
a  Local Time Step      1.1691e-05                         44373


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2248          1.6753      0.00053501     -6.7859e-07
v  Velocity[Y]                  -15.11          31.535          6.8405          20.056
v  Velocity[Z]                 -33.212          28.533       -0.082011      -0.0066176
v  ǁVelocityǁ                0.0078351          35.237          10.594          20.216
v  Pressure                     -438.4          348.56         -50.769          31.642
v  k                        3.8202e-08           67.76          4.0947          1.6298
v  omega                         1e-24      3.8612e+07          7987.2          11.829
v  turbulent_viscosity      3.7647e-15          1.2877        0.015894         0.10918
v  CourantNb                  0.062092          2594.1          44.042          1.3763
v  FourierNb                  0.010848           15746          93.505         0.68881
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14822        0.010819        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15808          137.55          2.0651


 TIME FOR THE TIME STEP              419:        0.45806E+02

===============================================================


 INSTANT    0.420000000E+02   TIME STEP NUMBER             420
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.459097036E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29526E+02 0.16158E+02
   Friction velocity        uet   :  0.37500E-02 0.31064E+01
   Friction velocity        uk    :  0.15860E-01 0.27891E+01
   Dimensionless distance   yplus :  0.13342E+00 0.26844E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1983   0.46180E-02   0.37211E+00 
c  VelocityY    0.29381E+04    1983   0.46180E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1983   0.46180E-02   0.00000E+00 
c  Pressure     0.42385E+00    7097   0.37313E-01   0.19907E+00 
c  k            0.21098E+04    1491   0.79943E-04   0.11897E+01 
c  omega        0.11597E+08     258   0.23036E-03   0.19923E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.774e+05                             1
a  Local Time Step      1.1422e-05                         44388


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2884          1.8054      -9.018e-05     -1.5234e-06
v  Velocity[Y]                 -23.326          30.024          6.8503          20.056
v  Velocity[Z]                  -32.95          28.634       -0.015412      -0.0065329
v  ǁVelocityǁ                 0.012959          34.496          10.609          20.216
v  Pressure                    -445.11           347.3         -50.411          31.626
v  k                        2.9526e-08          61.582          4.0676          1.6294
v  omega                         1e-24      7.6103e+07          8442.5          11.873
v  turbulent_viscosity      5.5316e-15           1.288        0.015894           0.109
v  CourantNb                  0.032656          2695.5          44.152          1.3763
v  FourierNb                  0.010849           15716          93.963         0.68768
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010819        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95555           15778          138.12          2.0639


 TIME FOR THE TIME STEP              420:        0.46827E+02

===============================================================


 INSTANT    0.421000000E+02   TIME STEP NUMBER             421
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.325576370E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30635E+02 0.15085E+02
   Friction velocity        uet   :  0.18984E-03 0.29270E+01
   Friction velocity        uk    :  0.18623E-01 0.29714E+01
   Dimensionless distance   yplus :  0.16733E+00 0.26926E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        365
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1953   0.46189E-02   0.35370E+00 
c  VelocityY    0.29382E+04    1953   0.46189E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1953   0.46189E-02   0.00000E+00 
c  Pressure     0.43452E+00    7085   0.34596E-01   0.20437E+00 
c  k            0.21228E+04    1512   0.81624E-04   0.12193E+01 
c  omega        0.35533E+08     166   0.47922E-04   0.15453E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -55539                             1
a  Local Time Step       1.109e-05                         44380


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2401          1.8271       -0.001087     -1.8143e-06
v  Velocity[Y]                  -26.61          29.866          6.8059          20.056
v  Velocity[Z]                 -31.264          28.405        0.044344      -0.0062224
v  ǁVelocityǁ                 0.013877          32.598           10.59          20.216
v  Pressure                    -432.78          347.08         -50.046          31.736
v  k                        4.4383e-07          48.152          4.0364          1.6291
v  omega                         1e-24      3.8761e+07          8624.9          11.899
v  turbulent_viscosity      7.9108e-14          1.2888        0.015853         0.10883
v  CourantNb                  0.052675          2285.7          44.314          1.3764
v  FourierNb                   0.01085           15555          94.184         0.68624
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010818        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15618           138.5          2.0626


 TIME FOR THE TIME STEP              421:        0.45491E+02

===============================================================


 INSTANT    0.422000000E+02   TIME STEP NUMBER             422
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.396930384E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30341E+02 0.16918E+02
   Friction velocity        uet   :  0.16977E-02 0.27048E+01
   Friction velocity        uk    :  0.24650E-01 0.28755E+01
   Dimensionless distance   yplus :  0.14096E+00 0.26980E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        380
   Nb of faces within the viscous sub-layer     :        968
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1858   0.45230E-02   0.33714E+00 
c  VelocityY    0.29382E+04    1858   0.45230E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1858   0.45230E-02   0.00000E+00 
c  Pressure     0.42937E+00    7078   0.32533E-01   0.20236E+00 
c  k            0.21308E+04    1467   0.95855E-04   0.11742E+01 
c  omega        0.19740E+08     215   0.41996E-04   0.56080E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4649e+05                             1
a  Local Time Step         1.1e-05                         44391


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1657          1.8435      -0.0020785      -5.218e-06
v  Velocity[Y]                 -33.391          29.772          6.7105          20.055
v  Velocity[Z]                 -29.955          28.498        0.075322      -0.0059818
v  ǁVelocityǁ                0.0066555          33.695          10.592          20.215
v  Pressure                    -407.42          346.14         -50.458          31.615
v  k                         1.104e-06           86.08          4.0503           1.629
v  omega                         1e-24      2.0739e+07          8220.6          11.879
v  turbulent_viscosity      5.0901e-14          1.2895        0.015795         0.10867
v  CourantNb                  0.026831          2033.7          44.365          1.3764
v  FourierNb                  0.010851           15363          93.598         0.68493
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14783        0.010818        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15429          137.96          2.0613


 TIME FOR THE TIME STEP              422:        0.44964E+02

===============================================================


 INSTANT    0.423000000E+02   TIME STEP NUMBER             423
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.366738697E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30854E+02 0.22633E+02
   Friction velocity        uet   :  0.10631E-02 0.28120E+01
   Friction velocity        uk    :  0.25231E-01 0.31971E+01
   Dimensionless distance   yplus :  0.13617E+00 0.30907E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        370
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1734   0.44980E-02   0.32960E+00 
c  VelocityY    0.29383E+04    1734   0.44980E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1734   0.44980E-02   0.00000E+00 
c  Pressure     0.42721E+00    7044   0.34558E-01   0.20190E+00 
c  k            0.21309E+04    1376   0.13090E-03   0.10353E+01 
c  omega        0.11240E+08     449   0.56578E-04   0.27644E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1036e+05                             2
a  Local Time Step      1.1297e-05                         44361


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1204          1.8386      -0.0025438     -4.4256e-06
v  Velocity[Y]                 -39.303          30.028          6.6573          20.056
v  Velocity[Z]                 -28.615          28.476         0.10156      -0.0056187
v  ǁVelocityǁ                 0.014741           40.58            10.6          20.216
v  Pressure                    -411.04          344.88         -51.756          31.702
v  k                        5.6883e-08           106.2          4.0995          1.6292
v  omega                         1e-24       1.421e+07            8110          11.887
v  turbulent_viscosity      2.3019e-13          1.2888         0.01575         0.10852
v  CourantNb                  0.020594          2022.8          44.488          1.3765
v  FourierNb                  0.010853           15172          93.211          0.6841
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14785        0.010818        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15239           137.7          2.0606


 TIME FOR THE TIME STEP              423:        0.43506E+02

===============================================================


 INSTANT    0.424000000E+02   TIME STEP NUMBER             424
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.417810251E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54139E+02 0.13477E+02
   Friction velocity        uet   :  0.13034E-02 0.35760E+01
   Friction velocity        uk    :  0.23729E-01 0.48346E+01
   Dimensionless distance   yplus :  0.13320E+00 0.39948E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        400
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1681   0.47572E-02   0.32917E+00 
c  VelocityY    0.29383E+04    1681   0.47572E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1681   0.47572E-02   0.00000E+00 
c  Pressure     0.42130E+00    7010   0.38151E-01   0.19897E+00 
c  k            0.21270E+04    1207   0.12925E-03   0.90032E+00 
c  omega        0.10394E+08     497   0.21127E-03   0.20055E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1497e+05                             1
a  Local Time Step      1.1328e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0127          1.8326      -0.0024037     -5.2374e-06
v  Velocity[Y]                 -28.986          30.512          6.6545          20.055
v  Velocity[Z]                 -28.741          28.812         0.10903      -0.0054633
v  ǁVelocityǁ                 0.014093           33.54          10.588          20.216
v  Pressure                    -412.17          343.69         -53.539          31.861
v  k                         2.035e-08           49.19          4.0898          1.6296
v  omega                         1e-24      5.3714e+07          8977.6          11.943
v  turbulent_viscosity      1.8517e-13          1.2865        0.015728         0.10839
v  CourantNb                   0.02823          2342.5          44.732          1.3766
v  FourierNb                  0.010855           15081          92.783         0.68357
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14774        0.010818        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15149          137.51          2.0602


 TIME FOR THE TIME STEP              424:        0.43099E+02

===============================================================


 INSTANT    0.425000000E+02   TIME STEP NUMBER             425
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.593101403E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29865E+02 0.13487E+02
   Friction velocity        uet   :  0.10433E-02 0.28962E+01
   Friction velocity        uk    :  0.21800E-01 0.29372E+01
   Dimensionless distance   yplus :  0.13333E+00 0.26563E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1794   0.44297E-02   0.33632E+00 
c  VelocityY    0.29384E+04    1794   0.44297E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1794   0.44297E-02   0.00000E+00 
c  Pressure     0.46399E+00    7116   0.38279E-01   0.22008E+00 
c  k            0.21232E+04    1203   0.68217E-04   0.75128E+00 
c  omega        0.23395E+08     255   0.61152E-04   0.17176E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2768e+05                             1
a  Local Time Step      1.1411e-05                         44294


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7754          1.8343      -0.0020614     -4.8818e-06
v  Velocity[Y]                 -17.728          30.735          6.6661          20.055
v  Velocity[Z]                 -28.423          28.811        0.094851      -0.0048685
v  ǁVelocityǁ                 0.020677          33.461           10.56          20.216
v  Pressure                    -413.12          342.76         -54.962          31.926
v  k                        2.1954e-09          51.193          4.1145          1.6302
v  omega                         1e-24      4.8058e+07          8876.7          11.934
v  turbulent_viscosity      2.1029e-14          1.2822        0.015719         0.10829
v  CourantNb                  0.024627          2969.4          44.893          1.3765
v  FourierNb                  0.010857           15001          92.556         0.68298
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14856        0.010817        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15068          137.45          2.0595


 TIME FOR THE TIME STEP              425:        0.44016E+02

===============================================================


 INSTANT    0.426000000E+02   TIME STEP NUMBER             426
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.377521050E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31395E+02 0.13348E+02
   Friction velocity        uet   :  0.32500E-03 0.29114E+01
   Friction velocity        uk    :  0.22733E-01 0.32036E+01
   Dimensionless distance   yplus :  0.17535E+00 0.27076E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        565
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2081   0.43758E-02   0.35064E+00 
c  VelocityY    0.29385E+04    2081   0.43758E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2081   0.43758E-02   0.00000E+00 
c  Pressure     0.42266E+00    7081   0.33877E-01   0.20002E+00 
c  k            0.21209E+04    1355   0.69021E-04   0.71006E+00 
c  omega        0.20464E+08     345   0.43911E-04   0.94954E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0427e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3987          1.8637      -0.0015844     -3.9337e-06
v  Velocity[Y]                 -17.182          33.561           6.688          20.056
v  Velocity[Z]                 -28.302          29.008        0.056464      -0.0041389
v  ǁVelocityǁ                 0.015473          33.903          10.522          20.216
v  Pressure                    -413.26          342.41         -55.583          31.715
v  k                        1.5893e-08          50.491            4.16          1.6311
v  omega                         1e-24      2.4634e+07          8655.3          11.912
v  turbulent_viscosity      5.5048e-15          1.2777         0.01573          0.1082
v  CourantNb                  0.017753          2001.8          44.629          1.3764
v  FourierNb                   0.01086           14984          93.836          0.6829
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14842        0.010817         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15049          138.46          2.0593


 TIME FOR THE TIME STEP              426:        0.46548E+02

===============================================================


 INSTANT    0.427000000E+02   TIME STEP NUMBER             427
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.202005678E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31073E+02 0.14185E+02
   Friction velocity        uet   :  0.13055E-02 0.29859E+01
   Friction velocity        uk    :  0.14394E-01 0.31810E+01
   Dimensionless distance   yplus :  0.11948E+00 0.31478E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        509
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    2071   0.44535E-02   0.36929E+00 
c  VelocityY    0.29386E+04    2071   0.44535E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    2071   0.44535E-02   0.00000E+00 
c  Pressure     0.41847E+00    7013   0.31124E-01   0.19706E+00 
c  k            0.21185E+04    1457   0.67488E-04   0.79990E+00 
c  omega        0.12886E+08     463   0.45733E-03   0.65987E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9512e+05                             2
a  Local Time Step      1.1627e-05                         44325


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95095          1.9043      -0.0010113     -4.0628e-07
v  Velocity[Y]                 -15.261          34.223          6.7078          20.056
v  Velocity[Z]                  -28.31          29.028       0.0091683      -0.0034429
v  ǁVelocityǁ                0.0079781           34.28          10.488          20.216
v  Pressure                    -406.49          343.28         -55.906          31.469
v  k                        3.3025e-07          52.091          4.1533          1.6319
v  omega                         1e-24      1.4587e+08          9546.4          11.946
v  turbulent_viscosity       5.236e-14          1.2747        0.015748         0.10813
v  CourantNb                  0.058564          1991.2           44.29          1.3764
v  FourierNb                  0.010862           15007          96.335         0.68343
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1489        0.010817        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15071          140.62          2.0598


 TIME FOR THE TIME STEP              427:        0.47275E+02

===============================================================


 INSTANT    0.428000000E+02   TIME STEP NUMBER             428
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.509325361E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30119E+02 0.15112E+02
   Friction velocity        uet   :  0.20940E-02 0.29029E+01
   Friction velocity        uk    :  0.16294E-01 0.28828E+01
   Dimensionless distance   yplus :  0.13936E+00 0.36440E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2111   0.44509E-02   0.38567E+00 
c  VelocityY    0.29385E+04    2111   0.44509E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2111   0.44509E-02   0.00000E+00 
c  Pressure     0.43633E+00    6769   0.30868E-01   0.20482E+00 
c  k            0.21138E+04    1491   0.64633E-04   0.72846E+00 
c  omega        0.11594E+09     159   0.20626E-04   0.17103E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7294e+05                             1
a  Local Time Step      1.1666e-05                         44316


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85936          1.9885      -0.0011678     -1.5678e-08
v  Velocity[Y]                  -15.03          34.979          6.6854          20.056
v  Velocity[Z]                 -28.922          28.857       -0.046598      -0.0029127
v  ǁVelocityǁ                  0.01615          35.242          10.479          20.216
v  Pressure                    -391.89          342.97         -56.892          30.637
v  k                        4.6785e-08          40.189          4.1318          1.6327
v  omega                         1e-24      7.3249e+07          8744.5          11.887
v  turbulent_viscosity      8.2427e-14          1.2712         0.01573         0.10807
v  CourantNb                 0.0067249          1980.3          44.113          1.3764
v  FourierNb                  0.010865           15043          96.535         0.68321
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14931        0.010818        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15105          140.65          2.0596


 TIME FOR THE TIME STEP              428:        0.47767E+02

===============================================================


 INSTANT    0.429000000E+02   TIME STEP NUMBER             429
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.781973041E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29195E+02 0.23798E+02
   Friction velocity        uet   :  0.19204E-02 0.28142E+01
   Friction velocity        uk    :  0.10137E-01 0.30126E+01
   Dimensionless distance   yplus :  0.12282E+00 0.38762E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        523
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2120   0.44500E-02   0.39877E+00 
c  VelocityY    0.29384E+04    2120   0.44500E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2120   0.44500E-02   0.00000E+00 
c  Pressure     0.40905E+00    6955   0.29241E-01   0.19210E+00 
c  k            0.21087E+04    1511   0.60382E-04   0.71556E+00 
c  omega        0.31579E+08     192   0.37657E-04   0.49825E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0702e+05                             1
a  Local Time Step      1.1553e-05                         44324


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2053          2.0916       -0.001045      1.0438e-06
v  Velocity[Y]                 -15.068          32.473           6.673          20.056
v  Velocity[Z]                 -28.503          28.815       -0.081883      -0.0019468
v  ǁVelocityǁ                 0.014936          33.433          10.485          20.215
v  Pressure                    -379.71          343.36         -56.866          30.434
v  k                        2.1959e-08          36.349          4.1161          1.6337
v  omega                         1e-24      3.7275e+07          8461.6           11.86
v  turbulent_viscosity      2.3473e-14          1.2672        0.015726         0.10804
v  CourantNb                  0.027511          1967.4          43.844          1.3766
v  FourierNb                  0.010867           15250          96.206           0.683
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821         0.01082        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15310          140.05          2.0596


 TIME FOR THE TIME STEP              429:        0.46509E+02

===============================================================


 INSTANT    0.430000000E+02   TIME STEP NUMBER             430
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.578971835E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30493E+02 0.21118E+02
   Friction velocity        uet   :  0.40741E-03 0.26392E+01
   Friction velocity        uk    :  0.19311E-01 0.30209E+01
   Dimensionless distance   yplus :  0.15124E+00 0.30914E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2136   0.44255E-02   0.40685E+00 
c  VelocityY    0.29384E+04    2136   0.44255E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2136   0.44255E-02   0.00000E+00 
c  Pressure     0.41930E+00    7039   0.28369E-01   0.19749E+00 
c  k            0.21042E+04    1444   0.58340E-04   0.81258E+00 
c  omega        0.13340E+08     214   0.45760E-04   0.17636E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6627e+05                             1
a  Local Time Step      1.1219e-05                         44318


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4427          2.1488     -0.00052749      1.0679e-06
v  Velocity[Y]                 -14.965          30.522          6.6894          20.056
v  Velocity[Z]                 -31.029          28.812        -0.10901      -0.0011814
v  ǁVelocityǁ                 0.013618          36.402          10.501          20.215
v  Pressure                    -353.81          344.16         -55.778          30.595
v  k                        1.3084e-07          49.091          4.1081          1.6348
v  omega                         1e-24      1.9963e+07          8169.6          11.834
v  turbulent_viscosity      7.5301e-16          1.2624        0.015741         0.10802
v  CourantNb                  0.049083          1992.9          43.965          1.3767
v  FourierNb                  0.010869           15468          95.808         0.68296
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.148        0.010821        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15529          139.77          2.0597


 TIME FOR THE TIME STEP              430:        0.47769E+02

===============================================================


 INSTANT    0.431000000E+02   TIME STEP NUMBER             431
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.932619009E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30258E+02 0.18164E+02
   Friction velocity        uet   :  0.30589E-02 0.30450E+01
   Friction velocity        uk    :  0.16361E-01 0.32514E+01
   Dimensionless distance   yplus :  0.10324E+00 0.27225E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        494
   Nb of faces within the viscous sub-layer     :       1004
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2184   0.44514E-02   0.39892E+00 
c  VelocityY    0.29384E+04    2184   0.44514E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2184   0.44514E-02   0.00000E+00 
c  Pressure     0.43860E+00    7045   0.32327E-01   0.20829E+00 
c  k            0.21025E+04    1135   0.64806E-04   0.96696E+00 
c  omega        0.10731E+08     230   0.58157E-04   0.12376E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3737e+05                             2
a  Local Time Step      1.1811e-05                         44266


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.569          2.1792      0.00026441      -2.722e-07
v  Velocity[Y]                 -15.107          30.701           6.734          20.057
v  Velocity[Z]                 -32.156          28.913        -0.11294     -0.00074521
v  ǁVelocityǁ                 0.010611          36.579          10.551          20.215
v  Pressure                    -406.73          344.52         -54.356          30.917
v  k                        1.2205e-08          62.079          4.1051          1.6359
v  omega                         1e-24      1.4063e+07          8096.9           11.83
v  turbulent_viscosity      1.3832e-13          1.2583        0.015778         0.10801
v  CourantNb                  0.093245          2029.2          43.969          1.3766
v  FourierNb                  0.010872           15680          95.094           0.683
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14857        0.010821        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15742          139.06          2.0596


 TIME FOR THE TIME STEP              431:        0.47297E+02

===============================================================


 INSTANT    0.432000000E+02   TIME STEP NUMBER             432
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.251830108E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29736E+02 0.13929E+02
   Friction velocity        uet   :  0.49636E-03 0.30999E+01
   Friction velocity        uk    :  0.16667E-01 0.29650E+01
   Dimensionless distance   yplus :  0.74905E-01 0.27084E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2215   0.44050E-02   0.39668E+00 
c  VelocityY    0.29383E+04    2215   0.44050E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2215   0.44050E-02   0.00000E+00 
c  Pressure     0.42734E+00    7036   0.37456E-01   0.20371E+00 
c  k            0.21063E+04    1316   0.71073E-04   0.10774E+01 
c  omega        0.10369E+08     250   0.16480E-03   0.96037E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6301e+05                             1
a  Local Time Step      1.1747e-05                         44282


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9486          2.2625       0.0012398     -2.6203e-07
v  Velocity[Y]                 -14.926          31.901          6.7923          20.056
v  Velocity[Z]                 -32.359           28.71       -0.079219      6.6584e-06
v  ǁVelocityǁ                 0.015173          34.766          10.606          20.214
v  Pressure                    -440.79          344.68         -53.035          31.175
v  k                        9.0202e-09          69.352          4.1032           1.637
v  omega                         1e-24      6.4669e+07          8290.7          11.842
v  turbulent_viscosity      5.6926e-14          1.2536        0.015816         0.10802
v  CourantNb                  0.090816          2525.2          43.982          1.3765
v  FourierNb                  0.010874           15806          94.599         0.68296
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14797        0.010819        0.045735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9916           15885          138.58          2.0595


 TIME FOR THE TIME STEP              432:        0.48177E+02

===============================================================


 INSTANT    0.433000000E+02   TIME STEP NUMBER             433
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.389999545E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28893E+02 0.15356E+02
   Friction velocity        uet   :  0.64434E-03 0.31538E+01
   Friction velocity        uk    :  0.17591E-01 0.30891E+01
   Dimensionless distance   yplus :  0.16252E+00 0.26898E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        444
   Nb of faces within the viscous sub-layer     :        959
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2200   0.45101E-02   0.39140E+00 
c  VelocityY    0.29383E+04    2200   0.45101E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2200   0.45101E-02   0.00000E+00 
c  Pressure     0.41179E+00    7106   0.39141E-01   0.19510E+00 
c  k            0.21149E+04    1509   0.73939E-04   0.11219E+01 
c  omega        0.21551E+08     167   0.90388E-04   0.11181E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -78886                             1
a  Local Time Step      1.1451e-05                         44310


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9932          2.5557       0.0025562      7.7091e-07
v  Velocity[Y]                  -21.14          30.247          6.8352          20.057
v  Velocity[Z]                 -32.923          28.668      -0.0097589      0.00065053
v  ǁVelocityǁ                 0.013265          34.361          10.634          20.215
v  Pressure                    -450.59          344.21         -52.473          31.358
v  k                        6.5847e-07          65.502          4.0773           1.638
v  omega                         1e-24      7.1952e+07          8287.5          11.859
v  turbulent_viscosity      1.6261e-15          1.2494        0.015826         0.10803
v  CourantNb                  0.024237          2744.5          44.133          1.3764
v  FourierNb                  0.010876           15817          94.649         0.68285
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14759        0.010819        0.045756


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15898          138.78          2.0593


 TIME FOR THE TIME STEP              433:        0.48323E+02

===============================================================


 INSTANT    0.434000000E+02   TIME STEP NUMBER             434
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240831021E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30736E+02 0.14081E+02
   Friction velocity        uet   :  0.23042E-02 0.29269E+01
   Friction velocity        uk    :  0.18149E-01 0.29364E+01
   Dimensionless distance   yplus :  0.11829E+00 0.26665E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2111   0.45261E-02   0.36507E+00 
c  VelocityY    0.29384E+04    2111   0.45261E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2111   0.45261E-02   0.00000E+00 
c  Pressure     0.42673E+00    7075   0.36582E-01   0.20217E+00 
c  k            0.21245E+04    1546   0.73655E-04   0.11596E+01 
c  omega        0.21998E+15       2   0.19968E-10   0.69375E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8158e+05                             1
a  Local Time Step       1.097e-05                         44320


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3209          2.7389       0.0032628     -2.1504e-06
v  Velocity[Y]                 -24.568           30.08           6.819          20.057
v  Velocity[Z]                 -32.949          28.645        0.062597        0.001408
v  ǁVelocityǁ                 0.018476          33.624          10.611          20.214
v  Pressure                    -440.44          344.27         -51.959          31.439
v  k                        9.6049e-08          52.748          4.0172          1.6388
v  omega                         1e-24      3.6726e+07          8365.3          11.882
v  turbulent_viscosity       1.143e-13          1.2456        0.015784         0.10806
v  CourantNb                  0.021724          2432.6          44.392          1.3766
v  FourierNb                  0.010878           15662          95.054         0.68248
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14785        0.010819        0.045742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93291           15742          139.45          2.0591


 TIME FOR THE TIME STEP              434:        0.46608E+02

===============================================================


 INSTANT    0.435000000E+02   TIME STEP NUMBER             435
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.374765492E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31439E+02 0.14677E+02
   Friction velocity        uet   :  0.76022E-03 0.28745E+01
   Friction velocity        uk    :  0.16715E-01 0.31946E+01
   Dimensionless distance   yplus :  0.73531E-01 0.26534E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        355
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2000   0.47150E-02   0.33604E+00 
c  VelocityY    0.29385E+04    2000   0.47150E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2000   0.47150E-02   0.00000E+00 
c  Pressure     0.43230E+00    7069   0.33219E-01   0.20556E+00 
c  k            0.21293E+04    1529   0.80746E-04   0.12258E+01 
c  omega        0.11956E+16       2   0.13544E-10   0.14775E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7354e+05                             2
a  Local Time Step      1.1318e-05                         44322


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4029            2.77       0.0031412     -3.8625e-06
v  Velocity[Y]                 -34.511          29.908          6.7411          20.056
v  Velocity[Z]                 -29.769          28.777         0.10447       0.0017069
v  ǁVelocityǁ                 0.019603          34.664           10.59          20.213
v  Pressure                    -415.53          344.53         -51.724          31.552
v  k                        3.1555e-07          73.434          3.9879          1.6393
v  omega                         1e-24      5.3263e+07          8270.6          11.892
v  turbulent_viscosity      3.1968e-14           1.244        0.015689         0.10809
v  CourantNb                  0.045817          2124.8          44.489          1.3766
v  FourierNb                   0.01088           15335          93.756         0.68147
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14854         0.01082        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15410          138.25          2.0581


 TIME FOR THE TIME STEP              435:        0.46075E+02

===============================================================


 INSTANT    0.436000000E+02   TIME STEP NUMBER             436
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.136552828E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31734E+02 0.23614E+02
   Friction velocity        uet   :  0.12420E-02 0.30246E+01
   Friction velocity        uk    :  0.20052E-01 0.31265E+01
   Dimensionless distance   yplus :  0.97640E-01 0.26627E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1917   0.46481E-02   0.32031E+00 
c  VelocityY    0.29386E+04    1917   0.46481E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1917   0.46481E-02   0.00000E+00 
c  Pressure     0.44446E+00    7094   0.33668E-01   0.21131E+00 
c  k            0.21264E+04    1410   0.91599E-04   0.10933E+01 
c  omega        0.36542E+08     267   0.14444E-04   0.57961E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0399e+05                             2
a  Local Time Step      1.0371e-05                         44276


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4744          2.6219       0.0024258     -2.1052e-06
v  Velocity[Y]                 -34.466          29.881          6.6776          20.056
v  Velocity[Z]                 -28.471          29.079         0.12865       0.0019178
v  ǁVelocityǁ                0.0080539          40.523          10.582          20.214
v  Pressure                    -412.36          344.34         -52.383          31.688
v  k                        9.0952e-07          89.663          4.0204          1.6398
v  omega                         1e-24       2.662e+07          8123.3          11.927
v  turbulent_viscosity      4.7123e-14          1.2433        0.015598         0.10812
v  CourantNb                   0.02253          2118.8          44.621          1.3766
v  FourierNb                  0.010881           14969          92.283          0.6806
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14836         0.01082        0.045743


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier               1           15038           136.9          2.0571


 TIME FOR THE TIME STEP              436:        0.45158E+02

===============================================================


 INSTANT    0.437000000E+02   TIME STEP NUMBER             437
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.106136272E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61927E+02 0.16298E+02
   Friction velocity        uet   :  0.27150E-03 0.34728E+01
   Friction velocity        uk    :  0.12184E-01 0.46310E+01
   Dimensionless distance   yplus :  0.10934E+00 0.35865E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        385
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1802   0.43758E-02   0.31266E+00 
c  VelocityY    0.29387E+04    1802   0.43758E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1802   0.43758E-02   0.00000E+00 
c  Pressure     0.44274E+00    7022   0.37241E-01   0.20966E+00 
c  k            0.21200E+04    1030   0.86138E-04   0.81009E+00 
c  omega        0.14186E+08     432   0.76473E-04   0.67284E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1414e-05                         44215


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4901          2.2896       0.0017585     -3.2902e-06
v  Velocity[Y]                  -33.31          30.327          6.6656          20.057
v  Velocity[Z]                  -28.43          28.984         0.14494       0.0023341
v  ǁVelocityǁ                 0.012968          34.128          10.566          20.214
v  Pressure                    -413.47           344.5         -53.589          31.912
v  k                        3.4052e-08          72.294          4.0092          1.6403
v  omega                         1e-24      4.9905e+07          8279.2          11.929
v  turbulent_viscosity      1.3151e-13          1.2415         0.01553         0.10816
v  CourantNb                  0.013953          2100.2          44.754          1.3765
v  FourierNb                  0.010882           14970          91.447         0.68023
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1477        0.010821        0.045749


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15032           136.2          2.0567


 TIME FOR THE TIME STEP              437:        0.43622E+02

===============================================================


 INSTANT    0.438000000E+02   TIME STEP NUMBER             438
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.940863165E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31007E+02 0.14403E+02
   Friction velocity        uet   :  0.15292E-02 0.32258E+01
   Friction velocity        uk    :  0.32711E-01 0.31401E+01
   Dimensionless distance   yplus :  0.14328E+00 0.28915E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1681   0.44975E-02   0.30470E+00 
c  VelocityY    0.29388E+04    1681   0.44975E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1681   0.44975E-02   0.00000E+00 
c  Pressure     0.44453E+00    7070   0.38599E-01   0.21019E+00 
c  k            0.21141E+04    1160   0.85216E-04   0.70022E+00 
c  omega        0.14770E+08     293   0.17745E-03   0.29903E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.3854e+05                             1
a  Local Time Step      1.1308e-05                         44174


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5578          1.7968       0.0015003     -4.6784e-06
v  Velocity[Y]                 -18.447          30.895          6.6705          20.057
v  Velocity[Z]                 -28.361          28.899         0.13459        0.002271
v  ǁVelocityǁ                 0.011353          33.651          10.535          20.214
v  Pressure                    -414.14          344.99          -54.83          32.117
v  k                        1.7245e-09          44.604          4.0334          1.6407
v  omega                         1e-24      6.0105e+07          9397.6          11.977
v  turbulent_viscosity      1.5511e-14          1.2417        0.015541         0.10821
v  CourantNb                  0.025027          3170.3          45.042          1.3764
v  FourierNb                  0.010883           14989          90.985         0.68047
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14834        0.010822        0.045763


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15046          136.03          2.0568


 TIME FOR THE TIME STEP              438:        0.42229E+02

===============================================================


 INSTANT    0.439000000E+02   TIME STEP NUMBER             439
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.326874349E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31244E+02 0.13290E+02
   Friction velocity        uet   :  0.16260E-02 0.28397E+01
   Friction velocity        uk    :  0.22895E-01 0.29159E+01
   Dimensionless distance   yplus :  0.15723E+00 0.26890E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        524
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1697   0.43822E-02   0.31077E+00 
c  VelocityY    0.29390E+04    1697   0.43822E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1697   0.43822E-02   0.00000E+00 
c  Pressure     0.42878E+00    7069   0.35666E-01   0.20349E+00 
c  k            0.21100E+04    1310   0.60433E-04   0.59481E+00 
c  omega        0.28440E+08     176   0.87262E-04   0.20802E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1513e-05                         44144


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4585          1.1567      0.00095515     -6.6428e-06
v  Velocity[Y]                 -17.499          32.944          6.6814          20.056
v  Velocity[Z]                 -28.668          28.906         0.10015       0.0021099
v  ǁVelocityǁ                 0.011278          34.112          10.501          20.213
v  Pressure                    -413.67          345.23         -55.453          31.927
v  k                        3.2554e-09          60.809          4.0952          1.6412
v  omega                         1e-24      7.7885e+07          9064.1          11.937
v  turbulent_viscosity      2.2924e-15           1.243        0.015584         0.10826
v  CourantNb                  0.022274          2292.7          44.803          1.3761
v  FourierNb                  0.010883           15007          91.812         0.68121
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14936        0.010823         0.04576


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15062          136.61          2.0573


 TIME FOR THE TIME STEP              439:        0.43046E+02

===============================================================


 INSTANT    0.440000000E+02   TIME STEP NUMBER             440
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.164802833E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30641E+02 0.13637E+02
   Friction velocity        uet   :  0.11287E-02 0.29545E+01
   Friction velocity        uk    :  0.18440E-01 0.29923E+01
   Dimensionless distance   yplus :  0.70992E-01 0.29478E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        581
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1842   0.45495E-02   0.32405E+00 
c  VelocityY    0.29391E+04    1842   0.45495E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1842   0.45495E-02   0.00000E+00 
c  Pressure     0.40827E+00    7052   0.34360E-01   0.19379E+00 
c  k            0.21076E+04    1350   0.64974E-04   0.66497E+00 
c  omega        0.29270E+08     286   0.40917E-04   0.79308E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1224e-05                         44144


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4948          1.2552     -0.00042161     -7.0882e-06
v  Velocity[Y]                 -16.108          33.903          6.7048          20.056
v  Velocity[Z]                   -28.5           28.75        0.049223       0.0020643
v  ǁVelocityǁ                  0.01803          34.048          10.467          20.212
v  Pressure                    -408.22          344.85         -55.933          31.797
v  k                         6.739e-09          92.988          4.1117          1.6415
v  omega                         1e-24      3.9565e+07          8554.9          11.902
v  turbulent_viscosity      1.1245e-15          1.2455        0.015645         0.10831
v  CourantNb                   0.04959          2019.6          44.296          1.3758
v  FourierNb                  0.010883           15067          94.228         0.68263
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14938        0.010822        0.045745


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98628           15131          138.52          2.0584


 TIME FOR THE TIME STEP              440:        0.45102E+02

===============================================================


 INSTANT    0.441000000E+02   TIME STEP NUMBER             441
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.200867643E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30173E+02 0.14196E+02
   Friction velocity        uet   :  0.15323E-02 0.29038E+01
   Friction velocity        uk    :  0.20910E-01 0.32078E+01
   Dimensionless distance   yplus :  0.78349E-01 0.35563E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1747   0.44494E-02   0.34658E+00 
c  VelocityY    0.29393E+04    1747   0.44494E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1747   0.44494E-02   0.00000E+00 
c  Pressure     0.43263E+00    6971   0.32174E-01   0.20478E+00 
c  k            0.21054E+04    1305   0.63226E-04   0.63349E+00 
c  omega        0.13497E+08     341   0.10598E-03   0.77280E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -21504                             1
a  Local Time Step      1.1191e-05                         44185


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6512          1.4025      -0.0021496     -4.4808e-06
v  Velocity[Y]                 -15.106          33.706          6.7027          20.057
v  Velocity[Z]                 -28.464          28.737      -0.0063891       0.0015643
v  ǁVelocityǁ                 0.011722          35.594          10.459          20.213
v  Pressure                    -392.51          343.31         -56.867          31.283
v  k                        4.3114e-09          101.06          4.0943          1.6418
v  omega                         1e-24      4.3493e+07          8612.2          11.911
v  turbulent_viscosity      1.1549e-14          1.2486        0.015679         0.10836
v  CourantNb                  0.033332          2013.9          44.006          1.3756
v  FourierNb                  0.010882           15166          96.102         0.68371
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010823        0.045726


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15229          140.11          2.0594


 TIME FOR THE TIME STEP              441:        0.44588E+02

===============================================================


 INSTANT    0.442000000E+02   TIME STEP NUMBER             442
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.435612964E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29016E+02 0.24654E+02
   Friction velocity        uet   :  0.10247E-02 0.27438E+01
   Friction velocity        uk    :  0.22682E-01 0.32146E+01
   Dimensionless distance   yplus :  0.99903E-01 0.37308E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        493
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    1815   0.44059E-02   0.35684E+00 
c  VelocityY    0.29395E+04    1815   0.44059E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    1815   0.44059E-02   0.00000E+00 
c  Pressure     0.44439E+00    6977   0.30170E-01   0.20825E+00 
c  k            0.21036E+04    1193   0.55370E-04   0.60625E+00 
c  omega        0.14998E+08     276   0.93719E-04   0.73309E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8476e+05                             2
a  Local Time Step      1.2134e-05                         44224


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7107           1.493      -0.0035321     -8.3668e-07
v  Velocity[Y]                 -17.548           32.26          6.6807          20.056
v  Velocity[Z]                 -28.595          28.677       -0.043354       0.0010805
v  ǁVelocityǁ                 0.021914          33.043          10.453          20.212
v  Pressure                    -380.65          342.13         -57.062          30.829
v  k                        4.3362e-08          79.279          4.0879          1.6421
v  omega                         1e-24      4.2266e+07          8603.4          11.888
v  turbulent_viscosity      2.4161e-16          1.2523        0.015708         0.10841
v  CourantNb                  0.010284          2030.6          43.841          1.3757
v  FourierNb                  0.010881           15251          96.188          0.6841
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010823        0.045717


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15314          140.03          2.0598


 TIME FOR THE TIME STEP              442:        0.43514E+02

===============================================================


 INSTANT    0.443000000E+02   TIME STEP NUMBER             443
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.225363865E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30947E+02 0.21366E+02
   Friction velocity        uet   :  0.38949E-03 0.25518E+01
   Friction velocity        uk    :  0.23362E-01 0.32413E+01
   Dimensionless distance   yplus :  0.90503E-01 0.37242E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        479
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    1840   0.44467E-02   0.36736E+00 
c  VelocityY    0.29396E+04    1840   0.44467E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    1840   0.44467E-02   0.00000E+00 
c  Pressure     0.43041E+00    7002   0.28130E-01   0.20298E+00 
c  k            0.21031E+04    1143   0.56253E-04   0.70024E+00 
c  omega        0.15224E+08     188   0.47976E-04   0.21459E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -6003.9                             1
a  Local Time Step      1.2175e-05                         44208


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6511          1.4976      -0.0044266      7.7449e-07
v  Velocity[Y]                 -15.136          30.532          6.6855          20.055
v  Velocity[Z]                  -30.04          28.645       -0.063561      0.00033782
v  ǁVelocityǁ                  0.01081          36.393          10.464           20.21
v  Pressure                    -360.51          341.92         -55.982          30.885
v  k                        7.2917e-08          47.248           4.088          1.6425
v  omega                         1e-24      2.2318e+07          8246.9          11.851
v  turbulent_viscosity      1.9408e-13          1.2584        0.015745         0.10846
v  CourantNb                  0.046118          2040.2          43.854          1.3758
v  FourierNb                   0.01088           15340          96.121         0.68432
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814        0.010823        0.045676


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15405          139.97          2.0601


 TIME FOR THE TIME STEP              443:        0.43734E+02

===============================================================


 INSTANT    0.444000000E+02   TIME STEP NUMBER             444
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.671183580E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30380E+02 0.19238E+02
   Friction velocity        uet   :  0.68226E-03 0.30060E+01
   Friction velocity        uk    :  0.24175E-01 0.29951E+01
   Dimensionless distance   yplus :  0.14098E+00 0.34241E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1856   0.43969E-02   0.36323E+00 
c  VelocityY    0.29397E+04    1856   0.43969E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1856   0.43969E-02   0.00000E+00 
c  Pressure     0.42349E+00    7038   0.30125E-01   0.19999E+00 
c  k            0.21053E+04    1153   0.62116E-04   0.86570E+00 
c  omega        0.10886E+08     224   0.36311E-04   0.10880E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2084e-05                         44205


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5572          1.4726      -0.0044715      2.5754e-07
v  Velocity[Y]                 -15.028          30.688           6.711          20.056
v  Velocity[Z]                 -32.209          28.573       -0.082799     -0.00052701
v  ǁVelocityǁ                 0.011751          36.909          10.495          20.211
v  Pressure                    -392.42          342.47         -54.545          31.175
v  k                        2.6822e-09          59.015          4.0915           1.643
v  omega                         1e-24      1.3483e+07          8052.4           11.82
v  turbulent_viscosity      8.0932e-14          1.2646        0.015786         0.10852
v  CourantNb                  0.039972            2049          43.979          1.3757
v  FourierNb                  0.010878           15429           95.13         0.68439
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14749        0.010821         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95195           15497          139.11          2.0601


 TIME FOR THE TIME STEP              444:        0.43785E+02

===============================================================


 INSTANT    0.445000000E+02   TIME STEP NUMBER             445
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.938263359E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31205E+02 0.15426E+02
   Friction velocity        uet   :  0.10593E-02 0.31291E+01
   Friction velocity        uk    :  0.17602E-01 0.31777E+01
   Dimensionless distance   yplus :  0.58640E-01 0.26718E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1853   0.45608E-02   0.36490E+00 
c  VelocityY    0.29399E+04    1853   0.45608E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1853   0.45608E-02   0.00000E+00 
c  Pressure     0.44236E+00    7000   0.34101E-01   0.20792E+00 
c  k            0.21122E+04    1303   0.72488E-04   0.10155E+01 
c  omega        0.10381E+08     210   0.60378E-04   0.13653E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3216e+05                             1
a  Local Time Step      1.1933e-05                         44266


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5031          1.4436          -0.004      2.6495e-06
v  Velocity[Y]                 -14.534          32.093          6.7576          20.056
v  Velocity[Z]                 -33.266          28.626       -0.069469     -0.00097213
v  ǁVelocityǁ                 0.010812          36.168          10.555          20.211
v  Pressure                    -436.82           343.1          -53.33          31.354
v  k                        2.4669e-08           68.05          4.0947          1.6435
v  omega                         1e-24      1.4939e+07          7984.9          11.817
v  turbulent_viscosity      2.6953e-15          1.2706        0.015824         0.10858
v  CourantNb                  0.012631          2384.7          43.926          1.3755
v  FourierNb                  0.010876           15477           94.58         0.68447
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14771         0.01082        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15546          138.51            2.06


 TIME FOR THE TIME STEP              445:        0.43706E+02

===============================================================


 INSTANT    0.446000000E+02   TIME STEP NUMBER             446
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.116037525E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30700E+02 0.14067E+02
   Friction velocity        uet   :  0.12614E-02 0.31357E+01
   Friction velocity        uk    :  0.98264E-02 0.32518E+01
   Dimensionless distance   yplus :  0.45256E-01 0.26576E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1827   0.45558E-02   0.37108E+00 
c  VelocityY    0.29400E+04    1827   0.45558E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1827   0.45558E-02   0.00000E+00 
c  Pressure     0.44397E+00    7109   0.37755E-01   0.20953E+00 
c  k            0.21250E+04    1370   0.77393E-04   0.10821E+01 
c  omega        0.10317E+08     245   0.27167E-03   0.22530E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3868e+05                             1
a  Local Time Step      1.2301e-05                         44302


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4875          1.4235      -0.0039149      4.4603e-06
v  Velocity[Y]                 -18.848          30.272          6.8061          20.056
v  Velocity[Z]                 -32.895           29.13       -0.018942      -0.0014859
v  ǁVelocityǁ                0.0086193          34.304          10.598          20.211
v  Pressure                    -453.81          343.54         -52.417          31.656
v  k                        3.9236e-07          67.881          4.0807          1.6441
v  omega                         1e-24      8.3689e+07          8722.2          11.884
v  turbulent_viscosity      2.0688e-14          1.2791        0.015842         0.10864
v  CourantNb                  0.015189          2730.4          43.938          1.3754
v  FourierNb                  0.010875           15408          94.265         0.68448
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14785         0.01082        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15478           138.2          2.0598


 TIME FOR THE TIME STEP              446:        0.44732E+02

===============================================================


 INSTANT    0.447000000E+02   TIME STEP NUMBER             447
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.507072816E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29975E+02 0.14979E+02
   Friction velocity        uet   :  0.88075E-03 0.29524E+01
   Friction velocity        uk    :  0.76139E-02 0.29952E+01
   Dimensionless distance   yplus :  0.92041E-01 0.26411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        366
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1860   0.45376E-02   0.36277E+00 
c  VelocityY    0.29401E+04    1860   0.45376E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1860   0.45376E-02   0.00000E+00 
c  Pressure     0.43349E+00    7082   0.37177E-01   0.20542E+00 
c  k            0.21397E+04    1265   0.77580E-04   0.11183E+01 
c  omega        0.39071E+08     143   0.32751E-04   0.80212E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2063e-05                         44303


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3771          1.4137      -0.0040279      4.8086e-06
v  Velocity[Y]                 -23.967          30.119          6.8171          20.056
v  Velocity[Z]                 -32.694          28.875        0.041421      -0.0019916
v  ǁVelocityǁ                0.0076858          34.287          10.601          20.211
v  Pressure                    -448.79          344.02         -52.021          31.783
v  k                          3.51e-07           56.65           4.042          1.6446
v  omega                         1e-24      4.2486e+07          8348.9          11.867
v  turbulent_viscosity      1.8197e-13          1.2874        0.015832         0.10871
v  CourantNb                  0.017978          2602.2          44.113          1.3754
v  FourierNb                  0.010873           15274            94.5         0.68455
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010821        0.045735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89823           15345          138.61            2.06


 TIME FOR THE TIME STEP              447:        0.44293E+02

===============================================================


 INSTANT    0.448000000E+02   TIME STEP NUMBER             448
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.283788000E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31437E+02 0.13579E+02
   Friction velocity        uet   :  0.18806E-02 0.28980E+01
   Friction velocity        uk    :  0.55575E-02 0.29208E+01
   Dimensionless distance   yplus :  0.60592E-01 0.26319E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        322
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1884   0.44801E-02   0.33394E+00 
c  VelocityY    0.29402E+04    1884   0.44801E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1884   0.44801E-02   0.00000E+00 
c  Pressure     0.43739E+00    7085   0.33890E-01   0.20741E+00 
c  k            0.21518E+04    1189   0.78775E-04   0.11159E+01 
c  omega        0.15267E+08     209   0.60395E-04   0.44979E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3773e+05                             1
a  Local Time Step      1.1298e-05                         44311


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1458          1.4442      -0.0032128      4.2616e-06
v  Velocity[Y]                 -32.003          29.967          6.7567          20.056
v  Velocity[Z]                 -31.413          28.925        0.086724      -0.0028047
v  ǁVelocityǁ                0.0063128          33.289          10.574          20.211
v  Pressure                    -426.81          345.02         -51.647          31.764
v  k                        5.5528e-08          65.763          4.0251          1.6451
v  omega                         1e-24      2.3103e+07          8205.4          11.869
v  turbulent_viscosity      6.9557e-14          1.2957        0.015785         0.10878
v  CourantNb                  0.014693          2042.4          44.331          1.3755
v  FourierNb                  0.010872           15110          93.963         0.68438
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010822        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8538           15182          138.29          2.0599


 TIME FOR THE TIME STEP              448:        0.44068E+02

===============================================================


 INSTANT    0.449000000E+02   TIME STEP NUMBER             449
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.461139924E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31220E+02 0.22185E+02
   Friction velocity        uet   :  0.23086E-02 0.28925E+01
   Friction velocity        uk    :  0.18830E-01 0.28865E+01
   Dimensionless distance   yplus :  0.11435E+00 0.26437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        302
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1995   0.46120E-02   0.31821E+00 
c  VelocityY    0.29403E+04    1995   0.46120E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1995   0.46120E-02   0.00000E+00 
c  Pressure     0.41611E+00    7044   0.32230E-01   0.19683E+00 
c  k            0.21569E+04    1341   0.10211E-03   0.98615E+00 
c  omega        0.11459E+08     326   0.43699E-04   0.27858E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3216e+05                             1
a  Local Time Step      1.1322e-05                         44280


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8189          1.4796       -0.001964       3.169e-06
v  Velocity[Y]                 -23.857          29.988          6.6765          20.056
v  Velocity[Z]                 -29.016          28.715         0.10075      -0.0035232
v  ǁVelocityǁ                 0.010173          33.332          10.574          20.211
v  Pressure                    -412.53          346.05         -52.103            31.7
v  k                        2.1234e-09          97.514          4.0644          1.6458
v  omega                         1e-24      1.4294e+07          8050.3          11.867
v  turbulent_viscosity      1.3281e-13          1.3028        0.015729         0.10887
v  CourantNb                  0.036057          2035.4           44.41          1.3756
v  FourierNb                   0.01087           15089          93.436         0.68421
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010823        0.045732


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81565           15145          137.85          2.0598


 TIME FOR THE TIME STEP              449:        0.45892E+02

===============================================================


 INSTANT    0.450000000E+02   TIME STEP NUMBER             450
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.638378309E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30393E+02 0.17228E+02
   Friction velocity        uet   :  0.13987E-02 0.27031E+01
   Friction velocity        uk    :  0.22547E-01 0.37956E+01
   Dimensionless distance   yplus :  0.13293E+00 0.33533E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        373
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2065   0.47242E-02   0.31650E+00 
c  VelocityY    0.29405E+04    2065   0.47242E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2065   0.47242E-02   0.00000E+00 
c  Pressure     0.43646E+00    7033   0.35286E-01   0.20615E+00 
c  k            0.21563E+04    1413   0.12147E-03   0.82553E+00 
c  omega        0.10439E+08     500   0.71712E-04   0.55227E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8577e+05                             1
a  Local Time Step      1.1445e-05                         44242


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4184          1.5205      -0.0008795      6.8732e-07
v  Velocity[Y]                 -36.507          30.179          6.6579          20.056
v  Velocity[Z]                 -28.507          28.921         0.10967      -0.0043383
v  ǁVelocityǁ                 0.015171          37.131          10.565          20.212
v  Pressure                    -414.08          346.68         -53.237          32.056
v  k                         2.266e-09          86.798          4.1026          1.6466
v  omega                         1e-24      4.1745e+07          8109.8          11.879
v  turbulent_viscosity       8.442e-15          1.3088        0.015706         0.10896
v  CourantNb                  0.055152          2024.5          44.559          1.3757
v  FourierNb                  0.010868           15168          93.632         0.68465
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14882        0.010821        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15222          138.19          2.0603


 TIME FOR THE TIME STEP              450:        0.48929E+02

===============================================================


 INSTANT    0.451000000E+02   TIME STEP NUMBER             451
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.547232915E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39616E+02 0.13600E+02
   Friction velocity        uet   :  0.14737E-02 0.34258E+01
   Friction velocity        uk    :  0.22073E-01 0.37745E+01
   Dimensionless distance   yplus :  0.17691E+00 0.36239E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    2073   0.44683E-02   0.31710E+00 
c  VelocityY    0.29407E+04    2073   0.44683E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    2073   0.44683E-02   0.00000E+00 
c  Pressure     0.43632E+00    7088   0.38202E-01   0.20804E+00 
c  k            0.21545E+04    1443   0.99729E-04   0.73540E+00 
c  omega        0.14526E+08     362   0.21703E-03   0.33453E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.115e-05                         44245


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1054          1.5489     -0.00015036     -1.9469e-07
v  Velocity[Y]                 -21.795          30.824          6.6695          20.056
v  Velocity[Z]                  -28.49          28.668         0.10163      -0.0048838
v  ǁVelocityǁ                 0.014166          33.674          10.549          20.212
v  Pressure                    -414.71          346.85          -54.53          32.116
v  k                        1.3978e-09          42.995          4.1082          1.6477
v  omega                         1e-24      6.0882e+07          9370.7           11.95
v  turbulent_viscosity      2.0614e-15          1.3159        0.015716         0.10907
v  CourantNb                  0.011129          3106.8          44.901          1.3758
v  FourierNb                  0.010867           15258          93.448         0.68518
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010821        0.045656


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15314          138.35           2.061


 TIME FOR THE TIME STEP              451:        0.48095E+02

===============================================================


 INSTANT    0.452000000E+02   TIME STEP NUMBER             452
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.195199884E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30552E+02 0.13494E+02
   Friction velocity        uet   :  0.14135E-02 0.26581E+01
   Friction velocity        uk    :  0.24005E-01 0.30680E+01
   Dimensionless distance   yplus :  0.10946E+00 0.27476E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        523
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    2134   0.45463E-02   0.32536E+00 
c  VelocityY    0.29409E+04    2134   0.45463E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    2134   0.45463E-02   0.00000E+00 
c  Pressure     0.41693E+00    7111   0.35679E-01   0.19828E+00 
c  k            0.21541E+04    1419   0.59636E-04   0.59236E+00 
c  omega        0.33634E+08     183   0.45133E-04   0.21786E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0954e-05                         44235


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1406          1.5527      0.00077152     -2.4065e-07
v  Velocity[Y]                 -17.567          31.953          6.6902          20.056
v  Velocity[Z]                 -28.655           28.87        0.066197      -0.0055833
v  ǁVelocityǁ                 0.010452          33.956          10.521          20.212
v  Pressure                    -414.79           346.4         -55.212          32.184
v  k                        1.6164e-08          46.809           4.162           1.649
v  omega                         1e-24      5.0388e+07            9068          11.925
v  turbulent_viscosity      3.1222e-15          1.3222        0.015747         0.10918
v  CourantNb                  0.039238          2664.1          44.776          1.3758
v  FourierNb                  0.010866           15435          93.784         0.68586
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14852        0.010819        0.045617


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15495          138.56          2.0616


 TIME FOR THE TIME STEP              452:        0.50566E+02

===============================================================


 INSTANT    0.453000000E+02   TIME STEP NUMBER             453
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.440588886E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30339E+02 0.13288E+02
   Friction velocity        uet   :  0.43448E-03 0.29260E+01
   Friction velocity        uk    :  0.11189E-01 0.32301E+01
   Dimensionless distance   yplus :  0.95419E-01 0.27748E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        600
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2149   0.43704E-02   0.34464E+00 
c  VelocityY    0.29411E+04    2149   0.43704E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2149   0.43704E-02   0.00000E+00 
c  Pressure     0.41207E+00    7053   0.32832E-01   0.19516E+00 
c  k            0.21557E+04    1311   0.63478E-04   0.62055E+00 
c  omega        0.26449E+08     322   0.20192E-03   0.74533E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5241e+05                             2
a  Local Time Step      1.0841e-05                         44254


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1621          1.5406       0.0020996     -2.0594e-07
v  Velocity[Y]                 -16.515          33.565          6.7219          20.057
v  Velocity[Z]                 -28.683          28.474        0.015577      -0.0062222
v  ǁVelocityǁ                0.0040129           33.71            10.5          20.213
v  Pressure                    -412.12          345.59         -55.434          31.954
v  k                        3.4589e-08          51.721          4.1944          1.6505
v  omega                         1e-24      1.3723e+08          9934.7          11.979
v  turbulent_viscosity       2.277e-14          1.3269        0.015792         0.10931
v  CourantNb                  0.029022          2000.1          44.408          1.3758
v  FourierNb                  0.010865           15634          95.936         0.68725
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14795        0.010818        0.045599


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15700          140.34           2.063


 TIME FOR THE TIME STEP              453:        0.48254E+02

===============================================================


 INSTANT    0.454000000E+02   TIME STEP NUMBER             454
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.629079128E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30372E+02 0.15450E+02
   Friction velocity        uet   :  0.76319E-03 0.29396E+01
   Friction velocity        uk    :  0.19953E-01 0.31817E+01
   Dimensionless distance   yplus :  0.13309E+00 0.30056E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        542
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2085   0.43667E-02   0.37067E+00 
c  VelocityY    0.29412E+04    2085   0.43667E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2085   0.43667E-02   0.00000E+00 
c  Pressure     0.41925E+00    6903   0.31228E-01   0.20035E+00 
c  k            0.21572E+04    1107   0.64641E-04   0.65699E+00 
c  omega        0.11378E+09     204   0.20408E-04   0.18973E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -78644                             1
a  Local Time Step      1.1576e-05                         44249


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3828          1.5005       0.0037987     -3.2814e-06
v  Velocity[Y]                  -15.03           33.38          6.7321          20.056
v  Velocity[Z]                 -28.767          28.612       -0.042642      -0.0069542
v  ǁVelocityǁ                0.0064853          33.472          10.492          20.212
v  Pressure                    -399.21          343.51         -56.186          31.304
v  k                        2.4498e-08          44.934          4.1762          1.6522
v  omega                         1e-24      6.8949e+07          8901.6          11.906
v  turbulent_viscosity      4.0975e-15          1.3313        0.015817         0.10945
v  CourantNb                  0.036998          2006.4          44.124          1.3758
v  FourierNb                  0.010864           15778          97.901          0.6886
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010818        0.045621


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15851          142.03          2.0644


 TIME FOR THE TIME STEP              454:        0.46408E+02

===============================================================


 INSTANT    0.455000000E+02   TIME STEP NUMBER             455
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.175018547E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30176E+02 0.22627E+02
   Friction velocity        uet   :  0.16123E-02 0.28185E+01
   Friction velocity        uk    :  0.17495E-01 0.30106E+01
   Dimensionless distance   yplus :  0.11050E+00 0.37840E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :        914
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2029   0.45818E-02   0.38275E+00 
c  VelocityY    0.29411E+04    2029   0.45818E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2029   0.45818E-02   0.00000E+00 
c  Pressure     0.43087E+00    6944   0.30163E-01   0.20582E+00 
c  k            0.21577E+04    1176   0.55873E-04   0.60636E+00 
c  omega        0.30751E+08     237   0.38006E-04   0.57533E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3031e+05                             1
a  Local Time Step      1.1648e-05                         44252


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7249          1.4214       0.0050074     -2.9641e-06
v  Velocity[Y]                 -15.211          33.152          6.7143          20.056
v  Velocity[Z]                 -28.418          28.697       -0.084411      -0.0075937
v  ǁVelocityǁ                  0.02263          33.352          10.492          20.212
v  Pressure                    -384.91          342.22         -56.693          30.837
v  k                        1.2001e-07          39.217          4.1545          1.6541
v  omega                         1e-24      3.5169e+07          8460.2          11.869
v  turbulent_viscosity      4.1877e-16          1.3332        0.015814          0.1096
v  CourantNb                  0.025221          2030.9           43.94          1.3761
v  FourierNb                  0.010863           15855          97.388         0.68913
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1492        0.010819        0.045638


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15934          141.33          2.0652


 TIME FOR THE TIME STEP              455:        0.46617E+02

===============================================================


 INSTANT    0.456000000E+02   TIME STEP NUMBER             456
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.784924960E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30214E+02 0.20430E+02
   Friction velocity        uet   :  0.14945E-02 0.26920E+01
   Friction velocity        uk    :  0.70641E-02 0.31205E+01
   Dimensionless distance   yplus :  0.97310E-01 0.30197E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :        925
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    2034   0.45495E-02   0.39835E+00 
c  VelocityY    0.29409E+04    2034   0.45495E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    2034   0.45495E-02   0.00000E+00 
c  Pressure     0.44333E+00    6972   0.28282E-01   0.21124E+00 
c  k            0.21588E+04    1269   0.54687E-04   0.66526E+00 
c  omega        0.13103E+08     207   0.42831E-04   0.16946E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -47791                             1
a  Local Time Step      1.1194e-05                         44249


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.895          1.3131       0.0055178     -3.9673e-06
v  Velocity[Y]                 -15.018           30.53          6.7179          20.056
v  Velocity[Z]                 -29.943          28.581         -0.1038      -0.0078114
v  ǁVelocityǁ                  0.01059          35.435          10.498          20.213
v  Pressure                    -367.12          342.93          -55.97          30.908
v  k                        1.3219e-07          42.829          4.1375          1.6563
v  omega                         1e-24      1.8985e+07          8146.3          11.825
v  turbulent_viscosity       4.022e-15          1.3357        0.015823         0.10977
v  CourantNb                  0.054656          2051.5          43.942          1.3765
v  FourierNb                  0.010863           15923          96.589         0.68975
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14782        0.010819        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16003          140.53          2.0662


 TIME FOR THE TIME STEP              456:        0.46042E+02

===============================================================


 INSTANT    0.457000000E+02   TIME STEP NUMBER             457
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.283601983E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31138E+02 0.20152E+02
   Friction velocity        uet   :  0.25163E-02 0.28957E+01
   Friction velocity        uk    :  0.83201E-02 0.30822E+01
   Dimensionless distance   yplus :  0.10966E+00 0.27443E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :        956
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    2079   0.44950E-02   0.39448E+00 
c  VelocityY    0.29407E+04    2079   0.44950E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    2079   0.44950E-02   0.00000E+00 
c  Pressure     0.42278E+00    6957   0.29707E-01   0.20208E+00 
c  k            0.21612E+04    1295   0.57067E-04   0.80554E+00 
c  omega        0.10676E+08     235   0.30620E-04   0.88484E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7409e+05                             1
a  Local Time Step      1.1504e-05                         44287


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0414          1.3179       0.0054222     -1.1794e-06
v  Velocity[Y]                 -15.206          30.495          6.7467          20.056
v  Velocity[Z]                 -31.869          28.858        -0.11532      -0.0076141
v  ǁVelocityǁ                 0.018345          36.764          10.522          20.213
v  Pressure                    -370.58          344.25         -54.762          30.988
v  k                        5.9873e-08          54.385          4.1301          1.6587
v  omega                         1e-24      1.2286e+07          8004.5          11.805
v  turbulent_viscosity      1.1119e-14          1.3377        0.015848         0.10994
v  CourantNb                  0.046681          2066.1          44.118          1.3766
v  FourierNb                  0.010863           16005           95.92         0.69052
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010819        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16083          140.04          2.0672


 TIME FOR THE TIME STEP              457:        0.46613E+02

===============================================================


 INSTANT    0.458000000E+02   TIME STEP NUMBER             458
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.564417824E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31143E+02 0.15197E+02
   Friction velocity        uet   :  0.11298E-02 0.30892E+01
   Friction velocity        uk    :  0.19276E-01 0.31421E+01
   Dimensionless distance   yplus :  0.12747E+00 0.27166E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        466
   Nb of faces within the viscous sub-layer     :        934
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2101   0.44337E-02   0.39149E+00 
c  VelocityY    0.29405E+04    2101   0.44337E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2101   0.44337E-02   0.00000E+00 
c  Pressure     0.40167E+00    6991   0.33733E-01   0.19122E+00 
c  k            0.21673E+04    1339   0.68754E-04   0.96468E+00 
c  omega        0.10362E+08     296   0.27755E-03   0.39072E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1049e+05                             2
a  Local Time Step      1.1847e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0811          1.2924       0.0050723     -4.6727e-07
v  Velocity[Y]                 -15.115          31.547          6.7931          20.056
v  Velocity[Z]                 -33.327           28.81        -0.10009      -0.0073985
v  ǁVelocityǁ                 0.022563          36.121          10.574          20.213
v  Pressure                     -426.8          345.44         -53.456          31.276
v  k                        4.1106e-10          65.786          4.1226          1.6613
v  omega                         1e-24      2.6097e+07          8225.7          11.876
v  turbulent_viscosity      2.9405e-14          1.3379        0.015862         0.11013
v  CourantNb                  0.031571            2238          44.107          1.3766
v  FourierNb                  0.010863           16068          95.424         0.69104
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1491        0.010818        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16139          139.53          2.0676


 TIME FOR THE TIME STEP              458:        0.47232E+02

===============================================================


 INSTANT    0.459000000E+02   TIME STEP NUMBER             459
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.408134537E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31755E+02 0.13899E+02
   Friction velocity        uet   :  0.19935E-02 0.31340E+01
   Friction velocity        uk    :  0.13840E-01 0.30098E+01
   Dimensionless distance   yplus :  0.18044E+00 0.26714E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :        950
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2065   0.44253E-02   0.39590E+00 
c  VelocityY    0.29405E+04    2065   0.44253E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2065   0.44253E-02   0.00000E+00 
c  Pressure     0.44408E+00    7096   0.37359E-01   0.21102E+00 
c  k            0.21787E+04    1339   0.71131E-04   0.10429E+01 
c  omega        0.15631E+08     206   0.15583E-03   0.18051E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0039e+05                             1
a  Local Time Step      1.1431e-05                         44379


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2559          1.1488        0.004437     -1.0216e-06
v  Velocity[Y]                 -15.967          30.296           6.846          20.057
v  Velocity[Z]                 -32.763          28.965       -0.045612      -0.0073534
v  ǁVelocityǁ                0.0044545          34.756          10.627          20.214
v  Pressure                    -450.57          346.53         -52.404           31.56
v  k                        8.4157e-09          68.339          4.0934          1.6638
v  omega                         1e-24      6.5003e+07            8569          11.885
v  turbulent_viscosity        3.37e-16          1.3362        0.015855         0.11033
v  CourantNb                  0.053613          2704.6          44.199          1.3765
v  FourierNb                  0.010863           16048          95.231          0.6915
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14931        0.010817        0.045727


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16111          139.43           2.068


 TIME FOR THE TIME STEP              459:        0.46954E+02

===============================================================


 INSTANT    0.460000000E+02   TIME STEP NUMBER             460
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.235694441E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30559E+02 0.14666E+02
   Friction velocity        uet   :  0.18356E-02 0.30085E+01
   Friction velocity        uk    :  0.17957E-01 0.28784E+01
   Dimensionless distance   yplus :  0.14713E+00 0.26720E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        399
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1978   0.45938E-02   0.38747E+00 
c  VelocityY    0.29405E+04    1978   0.45938E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1978   0.45938E-02   0.00000E+00 
c  Pressure     0.42288E+00    7099   0.37372E-01   0.20044E+00 
c  k            0.21923E+04    1270   0.71813E-04   0.10794E+01 
c  omega        0.28533E+08     178   0.39209E-04   0.63101E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1284e-05                         44413


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4438          0.9338       0.0034099     -4.9723e-08
v  Velocity[Y]                 -22.996          30.099          6.8661          20.057
v  Velocity[Z]                 -32.759          28.882        0.016791      -0.0072347
v  ǁVelocityǁ                0.0065474          34.125          10.632          20.215
v  Pressure                    -451.36             348         -51.903           31.54
v  k                        6.8458e-08          59.723          4.0451          1.6663
v  omega                         1e-24      3.3304e+07          8187.6           11.87
v  turbulent_viscosity      4.0971e-14          1.3335        0.015831         0.11053
v  CourantNb                  0.037139          2688.1          44.442          1.3766
v  FourierNb                  0.010864           15896          95.527         0.69225
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14855        0.010817        0.045699


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15954          139.97          2.0689


 TIME FOR THE TIME STEP              460:        0.46342E+02

===============================================================


 INSTANT    0.461000000E+02   TIME STEP NUMBER             461
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.605739201E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31020E+02 0.13591E+02
   Friction velocity        uet   :  0.24138E-02 0.28921E+01
   Friction velocity        uk    :  0.19842E-01 0.31979E+01
   Dimensionless distance   yplus :  0.12805E+00 0.27246E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        375
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1955   0.43373E-02   0.35582E+00 
c  VelocityY    0.29405E+04    1955   0.43373E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1955   0.43373E-02   0.00000E+00 
c  Pressure     0.41462E+00    7072   0.34229E-01   0.19574E+00 
c  k            0.22035E+04    1196   0.72186E-04   0.11031E+01 
c  omega        0.12698E+08     234   0.11305E-03   0.85119E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1469e+05                             2
a  Local Time Step      1.0952e-05                         44421


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5822         0.91481       0.0023643     -1.0031e-07
v  Velocity[Y]                 -30.333          29.954          6.8147          20.057
v  Velocity[Z]                 -31.924          28.835        0.074305      -0.0070204
v  ǁVelocityǁ                 0.014488          32.926          10.596          20.215
v  Pressure                    -433.88             350         -51.323          31.576
v  k                        4.2003e-08          56.962          4.0053          1.6686
v  omega                         1e-24      3.8187e+07          8502.3          11.896
v  turbulent_viscosity      2.4793e-14          1.3311         0.01577         0.11074
v  CourantNb                  0.048494          2118.8          44.691          1.3769
v  FourierNb                  0.010864           15718          94.175         0.69262
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14922        0.010817        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15774          138.87          2.0695


 TIME FOR THE TIME STEP              461:        0.45878E+02

===============================================================


 INSTANT    0.462000000E+02   TIME STEP NUMBER             462
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.279846914E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30974E+02 0.21557E+02
   Friction velocity        uet   :  0.19428E-02 0.28212E+01
   Friction velocity        uk    :  0.20314E-01 0.28707E+01
   Dimensionless distance   yplus :  0.63748E-01 0.27448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        308
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2029   0.44038E-02   0.32813E+00 
c  VelocityY    0.29403E+04    2029   0.44038E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2029   0.44038E-02   0.00000E+00 
c  Pressure     0.41356E+00    7087   0.31926E-01   0.19596E+00 
c  k            0.22080E+04    1260   0.93020E-04   0.10098E+01 
c  omega        0.12697E+08     259   0.75652E-04   0.10209E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7732e+05                             1
a  Local Time Step      1.1041e-05                         44397


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5747         0.97044       0.0012718     -1.1793e-06
v  Velocity[Y]                 -24.942          29.821          6.7283          20.057
v  Velocity[Z]                 -29.682          28.661        0.093201      -0.0061936
v  ǁVelocityǁ                 0.014267          33.197          10.586          20.215
v  Pressure                     -409.1          350.56         -51.687          31.466
v  k                        7.5815e-08           88.98          4.0269          1.6707
v  omega                         1e-24      3.3437e+07          8340.5          11.903
v  turbulent_viscosity      4.2415e-15          1.3273        0.015712         0.11095
v  CourantNb                  0.035218          2003.9          44.634          1.3769
v  FourierNb                  0.010865           15558          93.691          0.6933
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010817        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15616          138.32          2.0702


 TIME FOR THE TIME STEP              462:        0.46774E+02

===============================================================


 INSTANT    0.463000000E+02   TIME STEP NUMBER             463
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.255609000E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30554E+02 0.18673E+02
   Friction velocity        uet   :  0.18276E-02 0.25084E+01
   Friction velocity        uk    :  0.87480E-02 0.33453E+01
   Dimensionless distance   yplus :  0.99889E-01 0.32388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        330
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2081   0.43155E-02   0.31662E+00 
c  VelocityY    0.29403E+04    2081   0.43155E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2081   0.43155E-02   0.00000E+00 
c  Pressure     0.42384E+00    7036   0.34015E-01   0.20027E+00 
c  k            0.22047E+04    1299   0.11317E-03   0.85619E+00 
c  omega        0.17753E+08     429   0.68286E-04   0.99667E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1006e+05                             1
a  Local Time Step      1.0779e-05                         44381


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7385          1.0747      -0.0001688     -1.8572e-06
v  Velocity[Y]                 -36.752          30.241          6.6918          20.056
v  Velocity[Z]                 -29.112          28.794          0.1117      -0.0056286
v  ǁVelocityǁ                 0.019423          37.194          10.581          20.215
v  Pressure                    -411.42          350.52         -52.485          31.613
v  k                        3.4889e-08          94.479          4.0692          1.6729
v  omega                         1e-24      5.7932e+07          8457.4          11.921
v  turbulent_viscosity      7.6527e-15          1.3262        0.015669         0.11116
v  CourantNb                  0.029349          2011.7          44.702           1.377
v  FourierNb                  0.010865           15432          93.516         0.69451
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14868        0.010817        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15495          138.22          2.0715


 TIME FOR THE TIME STEP              463:        0.47457E+02

===============================================================


 INSTANT    0.464000000E+02   TIME STEP NUMBER             464
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.163910868E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43472E+02 0.13812E+02
   Friction velocity        uet   :  0.57465E-03 0.33889E+01
   Friction velocity        uk    :  0.95690E-02 0.41472E+01
   Dimensionless distance   yplus :  0.13182E+00 0.40209E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        382
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2069   0.42768E-02   0.31194E+00 
c  VelocityY    0.29403E+04    2069   0.42768E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2069   0.42768E-02   0.00000E+00 
c  Pressure     0.39287E+00    7058   0.37429E-01   0.18530E+00 
c  k            0.21984E+04    1255   0.11050E-03   0.74276E+00 
c  omega        0.18120E+08     363   0.13777E-03   0.18263E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1101e+05                             3
a  Local Time Step       1.082e-05                         44336


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6805          1.2633       -0.001991      -2.211e-06
v  Velocity[Y]                 -26.178          30.638          6.6877          20.056
v  Velocity[Z]                 -28.564          28.428         0.10786       -0.004877
v  ǁVelocityǁ                0.0073734          33.657           10.56          20.215
v  Pressure                    -412.55          349.29           -53.8          31.735
v  k                        5.4504e-10          39.579          4.0638          1.6748
v  omega                         1e-24      6.6376e+07          8847.8          11.923
v  turbulent_viscosity      1.5091e-14          1.3233         0.01566         0.11138
v  CourantNb                  0.018831            3038          44.973          1.3771
v  FourierNb                  0.010865           15404          93.066         0.69589
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010818        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15463          138.04           2.073


 TIME FOR THE TIME STEP              464:        0.47158E+02

===============================================================


 INSTANT    0.465000000E+02   TIME STEP NUMBER             465
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.405498141E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30660E+02 0.13630E+02
   Friction velocity        uet   :  0.51760E-03 0.28666E+01
   Friction velocity        uk    :  0.15817E-01 0.30779E+01
   Dimensionless distance   yplus :  0.12560E+00 0.27350E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        505
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2064   0.43906E-02   0.31893E+00 
c  VelocityY    0.29402E+04    2064   0.43906E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2064   0.43906E-02   0.00000E+00 
c  Pressure     0.42980E+00    7114   0.36538E-01   0.20189E+00 
c  k            0.21920E+04    1228   0.60852E-04   0.57829E+00 
c  omega        0.27295E+08     312   0.10350E-03   0.22877E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step        1.13e-05                         44291


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6988          1.3559      -0.0038399     -4.8013e-07
v  Velocity[Y]                 -17.721          31.833          6.6945          20.056
v  Velocity[Z]                 -28.756          28.517        0.081911      -0.0042013
v  ǁVelocityǁ                0.0064328          33.734          10.532          20.215
v  Pressure                    -413.22          347.47         -54.642          31.767
v  k                        1.8612e-10          49.094          4.1043          1.6766
v  omega                         1e-24      7.1167e+07          9168.9          11.939
v  turbulent_viscosity      1.0318e-15          1.3193        0.015659         0.11158
v  CourantNb                  0.023222          2922.2          44.923           1.377
v  FourierNb                  0.010865           15383          92.602         0.69716
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010819        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15440          137.53          2.0742


 TIME FOR THE TIME STEP              465:        0.47180E+02

===============================================================


 INSTANT    0.466000000E+02   TIME STEP NUMBER             466
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.188701851E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30179E+02 0.13870E+02
   Friction velocity        uet   :  0.17342E-02 0.29574E+01
   Friction velocity        uk    :  0.19583E-01 0.28806E+01
   Dimensionless distance   yplus :  0.11172E+00 0.28517E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        586
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2067   0.43231E-02   0.33786E+00 
c  VelocityY    0.29402E+04    2067   0.43231E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2067   0.43231E-02   0.00000E+00 
c  Pressure     0.43123E+00    7014   0.34224E-01   0.20437E+00 
c  k            0.21862E+04    1276   0.60333E-04   0.55910E+00 
c  omega        0.29525E+08     258   0.90337E-04   0.21704E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1426e-05                         44283


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.739          1.4033      -0.0053643      2.3639e-06
v  Velocity[Y]                  -16.95          33.745          6.7148          20.056
v  Velocity[Z]                 -28.824          28.643        0.037344      -0.0037503
v  ǁVelocityǁ                 0.012879          34.072          10.504          20.216
v  Pressure                    -411.96          346.06         -54.932          31.659
v  k                        2.2212e-08          51.471          4.1451          1.6782
v  omega                         1e-24      1.0551e+08          8852.5          11.916
v  turbulent_viscosity      2.2476e-16          1.3148        0.015679         0.11178
v  CourantNb                  0.076902            2040          44.537          1.3769
v  FourierNb                  0.010866           15347          93.924         0.69904
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14911        0.010819        0.045683


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15405          138.46          2.0759


 TIME FOR THE TIME STEP              466:        0.46745E+02

===============================================================


 INSTANT    0.467000000E+02   TIME STEP NUMBER             467
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.965300584E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30785E+02 0.14565E+02
   Friction velocity        uet   :  0.20526E-02 0.29778E+01
   Friction velocity        uk    :  0.16393E-01 0.30258E+01
   Dimensionless distance   yplus :  0.77470E-01 0.31856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        560
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1996   0.44417E-02   0.36555E+00 
c  VelocityY    0.29403E+04    1996   0.44417E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1996   0.44417E-02   0.00000E+00 
c  Pressure     0.44436E+00    6970   0.31545E-01   0.21067E+00 
c  k            0.21804E+04    1343   0.64344E-04   0.64959E+00 
c  omega        0.45727E+08     308   0.34011E-04   0.10274E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0726e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7544          1.3938       -0.006411      4.1043e-06
v  Velocity[Y]                 -15.172          33.804          6.7267          20.057
v  Velocity[Z]                 -29.461          28.379       -0.011453      -0.0030382
v  ǁVelocityǁ                 0.012766           33.99           10.49          20.216
v  Pressure                     -402.4          344.26         -55.499          31.201
v  k                        1.7976e-07          50.071          4.1321          1.6794
v  omega                         1e-24      5.3295e+07          8621.3          11.907
v  turbulent_viscosity      4.2946e-15          1.3091        0.015701         0.11197
v  CourantNb                  0.032528          2044.2          44.141          1.3767
v  FourierNb                  0.010866           15280          96.032         0.70125
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010819        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15341          140.17           2.078


 TIME FOR THE TIME STEP              467:        0.46744E+02

===============================================================


 INSTANT    0.468000000E+02   TIME STEP NUMBER             468
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.160609491E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30755E+02 0.15019E+02
   Friction velocity        uet   :  0.15583E-02 0.28742E+01
   Friction velocity        uk    :  0.12423E-01 0.31072E+01
   Dimensionless distance   yplus :  0.14359E+00 0.36812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :        973
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1906   0.44351E-02   0.38167E+00 
c  VelocityY    0.29401E+04    1906   0.44351E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1906   0.44351E-02   0.00000E+00 
c  Pressure     0.40994E+00    7023   0.30522E-01   0.19366E+00 
c  k            0.21732E+04    1357   0.55236E-04   0.58968E+00 
c  omega        0.19703E+08     296   0.41467E-04   0.32667E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.128e-05                         44344


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8571          1.3668      -0.0069162      5.7171e-06
v  Velocity[Y]                 -15.067          34.126          6.6951          20.057
v  Velocity[Z]                 -28.999          28.854       -0.061824      -0.0024715
v  ǁVelocityǁ                 0.013791          34.505          10.486          20.216
v  Pressure                    -388.58           342.8         -55.893          30.633
v  k                        3.7828e-08          35.315           4.109          1.6804
v  omega                         1e-24      2.7753e+07          8417.5          11.878
v  turbulent_viscosity      1.0858e-14          1.3028        0.015709         0.11214
v  CourantNb                  0.027893          2048.9           43.91          1.3769
v  FourierNb                  0.010866           15185          95.925          0.7028
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14776        0.010821        0.045696


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86775           15251          139.83          2.0797


 TIME FOR THE TIME STEP              468:        0.46134E+02

===============================================================


 INSTANT    0.469000000E+02   TIME STEP NUMBER             469
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.496754540E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30170E+02 0.20592E+02
   Friction velocity        uet   :  0.22748E-02 0.27385E+01
   Friction velocity        uk    :  0.99840E-02 0.32521E+01
   Dimensionless distance   yplus :  0.14581E+00 0.31968E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        488
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1917   0.45969E-02   0.39672E+00 
c  VelocityY    0.29398E+04    1917   0.45969E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1917   0.45969E-02   0.00000E+00 
c  Pressure     0.42265E+00    6954   0.28216E-01   0.19942E+00 
c  k            0.21663E+04    1257   0.52534E-04   0.63971E+00 
c  omega        0.11419E+08     271   0.54238E-04   0.20060E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2473e+05                             2
a  Local Time Step      1.1497e-05                         44314


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9664          1.3434      -0.0068654      5.5699e-06
v  Velocity[Y]                 -15.806          30.766          6.6744          20.057
v  Velocity[Z]                 -29.707          28.687       -0.087624      -0.0017796
v  ǁVelocityǁ                 0.019696          34.339          10.491          20.216
v  Pressure                     -373.9          342.59         -55.508          30.541
v  k                        2.1367e-08          40.322          4.0836          1.6811
v  omega                         1e-24       1.607e+07          8320.6          11.878
v  turbulent_viscosity      1.1476e-13          1.2955        0.015726          0.1123
v  CourantNb                  0.027216            2049          43.673          1.3772
v  FourierNb                  0.010865           15067          95.398         0.70412
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010822        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91692           15137          139.07          2.0813


 TIME FOR THE TIME STEP              469:        0.45342E+02

===============================================================


 INSTANT    0.470000000E+02   TIME STEP NUMBER             470
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.236874087E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31570E+02 0.20011E+02
   Friction velocity        uet   :  0.61962E-03 0.27765E+01
   Friction velocity        uk    :  0.15681E-01 0.28092E+01
   Dimensionless distance   yplus :  0.14678E+00 0.26624E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2028   0.45459E-02   0.40746E+00 
c  VelocityY    0.29397E+04    2028   0.45459E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2028   0.45459E-02   0.00000E+00 
c  Pressure     0.44534E+00    7043   0.28672E-01   0.21137E+00 
c  k            0.21604E+04    1235   0.57812E-04   0.77393E+00 
c  omega        0.10551E+08     229   0.33110E-04   0.10069E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.559e+05                             1
a  Local Time Step      1.1794e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9665          1.3475      -0.0064264      8.2464e-06
v  Velocity[Y]                 -15.096          30.574          6.6789          20.057
v  Velocity[Z]                 -31.729          29.207        -0.11356      -0.0013964
v  ǁVelocityǁ                 0.012944          36.569          10.505          20.216
v  Pressure                    -356.29          343.53         -54.308          30.782
v  k                        2.1815e-08          52.612           4.072          1.6816
v  omega                         1e-24      1.2084e+07            8105          11.845
v  turbulent_viscosity      4.0229e-14          1.2875         0.01576         0.11244
v  CourantNb                  0.030027          2049.5          43.852          1.3773
v  FourierNb                  0.010864           14978          94.634         0.70539
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14854        0.010821        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15047          138.49          2.0827


 TIME FOR THE TIME STEP              470:        0.48327E+02

===============================================================


 INSTANT    0.471000000E+02   TIME STEP NUMBER             471
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.478555599E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31479E+02 0.16323E+02
   Friction velocity        uet   :  0.19405E-02 0.30959E+01
   Friction velocity        uk    :  0.17647E-01 0.29965E+01
   Dimensionless distance   yplus :  0.12190E+00 0.26823E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    2046   0.43742E-02   0.41349E+00 
c  VelocityY    0.29395E+04    2046   0.43742E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    2046   0.43742E-02   0.00000E+00 
c  Pressure     0.42593E+00    6767   0.32751E-01   0.20265E+00 
c  k            0.21572E+04    1314   0.69269E-04   0.93975E+00 
c  omega        0.10272E+08     219   0.41379E-04   0.73276E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -16117                             1
a  Local Time Step      1.0996e-05                         44391


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8231          1.3674      -0.0057832         6.9e-06
v  Velocity[Y]                 -15.217          32.908           6.712          20.056
v  Velocity[Z]                 -33.217          28.921        -0.11624     -0.00087034
v  ǁVelocityǁ                 0.015536          37.157          10.549          20.216
v  Pressure                    -414.56           344.4         -53.432          30.878
v  k                        1.0876e-08           64.07           4.072          1.6818
v  omega                         1e-24      1.1704e+07          7946.1          11.834
v  turbulent_viscosity      2.2247e-14          1.2791        0.015798         0.11255
v  CourantNb                  0.057305          2185.1          43.859          1.3772
v  FourierNb                  0.010863           15050          93.813         0.70644
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.148        0.010821        0.045735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15108          137.67          2.0837


 TIME FOR THE TIME STEP              471:        0.46360E+02

===============================================================


 INSTANT    0.472000000E+02   TIME STEP NUMBER             472
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.365040363E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30819E+02 0.14941E+02
   Friction velocity        uet   :  0.12377E-02 0.31923E+01
   Friction velocity        uk    :  0.99730E-02 0.31292E+01
   Dimensionless distance   yplus :  0.13738E+00 0.26784E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2064   0.44049E-02   0.43090E+00 
c  VelocityY    0.29394E+04    2064   0.44049E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2064   0.44049E-02   0.00000E+00 
c  Pressure     0.42634E+00    7051   0.37445E-01   0.20186E+00 
c  k            0.21592E+04    1305   0.72628E-04   0.10399E+01 
c  omega        0.10131E+08     206   0.61582E-04   0.11669E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4953e+05                             1
a  Local Time Step      1.1569e-05                         44410


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5481          1.4295      -0.0048858      3.2939e-06
v  Velocity[Y]                 -15.062          32.164          6.7619          20.056
v  Velocity[Z]                 -33.181          28.888       -0.080053     -0.00018772
v  ǁVelocityǁ                0.0098082           35.51          10.596          20.216
v  Pressure                    -445.43          346.15         -52.544          31.173
v  k                        1.7328e-08          68.858          4.0617          1.6816
v  omega                         1e-24      1.4378e+07          7892.5          11.856
v  turbulent_viscosity      3.7527e-14          1.2705        0.015818         0.11264
v  CourantNb                  0.018774          2732.3          43.894          1.3771
v  FourierNb                  0.010861           15151          93.573         0.70719
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14758        0.010821        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15206          137.47          2.0843


 TIME FOR THE TIME STEP              472:        0.46708E+02

===============================================================


 INSTANT    0.473000000E+02   TIME STEP NUMBER             473
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.526322451E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29663E+02 0.16042E+02
   Friction velocity        uet   :  0.58547E-03 0.31956E+01
   Friction velocity        uk    :  0.81298E-02 0.30778E+01
   Dimensionless distance   yplus :  0.98277E-01 0.26935E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        366
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    2072   0.43497E-02   0.43764E+00 
c  VelocityY    0.29393E+04    2072   0.43497E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    2072   0.43497E-02   0.00000E+00 
c  Pressure     0.43653E+00    7105   0.38160E-01   0.20656E+00 
c  k            0.21647E+04    1303   0.73255E-04   0.10911E+01 
c  omega        0.15113E+08     225   0.15310E-03   0.15742E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -40200                             1
a  Local Time Step      1.1633e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1743          1.4916      -0.0037735      2.5336e-06
v  Velocity[Y]                 -22.511          30.247          6.7942          20.056
v  Velocity[Z]                 -32.647          29.014       -0.020011       0.0001858
v  ǁVelocityǁ                0.0025762          33.992           10.61          20.216
v  Pressure                    -451.78             347         -52.207          31.275
v  k                        7.6824e-07          62.944          4.0232          1.6809
v  omega                         1e-24      7.2329e+07          8230.1          11.883
v  turbulent_viscosity      1.2881e-13          1.2624        0.015814         0.11271
v  CourantNb                  0.017623          2823.9          44.104          1.3771
v  FourierNb                   0.01086           15222          93.883         0.70787
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14755        0.010822        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78322           15278          137.99          2.0849


 TIME FOR THE TIME STEP              473:        0.46699E+02

===============================================================


 INSTANT    0.474000000E+02   TIME STEP NUMBER             474
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.461792900E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30975E+02 0.14333E+02
   Friction velocity        uet   :  0.15577E-02 0.28744E+01
   Friction velocity        uk    :  0.12497E-01 0.28619E+01
   Dimensionless distance   yplus :  0.15541E+00 0.27191E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        352
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2017   0.45627E-02   0.41117E+00 
c  VelocityY    0.29392E+04    2017   0.45627E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2017   0.45627E-02   0.00000E+00 
c  Pressure     0.43216E+00    7075   0.34714E-01   0.20365E+00 
c  k            0.21690E+04    1332   0.71755E-04   0.11358E+01 
c  omega        0.31577E+08     150   0.45294E-04   0.80574E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5004e+05                             1
a  Local Time Step      1.1415e-05                         44471


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7156           1.557      -0.0031507     -5.5863e-07
v  Velocity[Y]                 -26.095          30.082           6.766          20.056
v  Velocity[Z]                 -31.736          28.935        0.032025      0.00089535
v  ǁVelocityǁ                 0.002905          32.741          10.582          20.215
v  Pressure                    -437.57          347.98         -51.601          31.301
v  k                        7.3531e-08          79.722          3.9824          1.6798
v  omega                         1e-24      3.6917e+07            8293          11.893
v  turbulent_viscosity       8.559e-14          1.2547        0.015763         0.11274
v  CourantNb                  0.060201            2366          44.372          1.3772
v  FourierNb                  0.010858           15249          93.039         0.70764
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14817        0.010823        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83084           15306          137.41          2.0848


 TIME FOR THE TIME STEP              474:        0.46285E+02

===============================================================


 INSTANT    0.475000000E+02   TIME STEP NUMBER             475
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.140256877E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30431E+02 0.16946E+02
   Friction velocity        uet   :  0.23348E-02 0.27552E+01
   Friction velocity        uk    :  0.11340E-01 0.29650E+01
   Dimensionless distance   yplus :  0.13739E+00 0.27496E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        344
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1988   0.45736E-02   0.38623E+00 
c  VelocityY    0.29392E+04    1988   0.45736E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1988   0.45736E-02   0.00000E+00 
c  Pressure     0.43049E+00    7061   0.31752E-01   0.20388E+00 
c  k            0.21682E+04    1360   0.87940E-04   0.10961E+01 
c  omega        0.13882E+08     216   0.55744E-04   0.38927E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -97727                             1
a  Local Time Step      1.1127e-05                         44489


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2415          1.6071       -0.002722     -3.1251e-06
v  Velocity[Y]                 -34.389          29.983          6.6845          20.056
v  Velocity[Z]                 -30.144          28.759        0.052312       0.0013619
v  ǁVelocityǁ                 0.006238          34.655           10.58          20.215
v  Pressure                    -410.42          347.98         -51.331           31.32
v  k                        1.4325e-08          82.644          4.0066          1.6781
v  omega                         1e-24      1.9891e+07          8000.6          11.868
v  turbulent_viscosity      1.5491e-13          1.2472        0.015708         0.11275
v  CourantNb                  0.055154          2029.5          44.469          1.3771
v  FourierNb                  0.010857           15298          92.686         0.70727
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14849        0.010824        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15365          137.16          2.0844


 TIME FOR THE TIME STEP              475:        0.46205E+02

===============================================================


 INSTANT    0.476000000E+02   TIME STEP NUMBER             476
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.604739437E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30630E+02 0.23177E+02
   Friction velocity        uet   :  0.16291E-02 0.28710E+01
   Friction velocity        uk    :  0.81159E-02 0.29884E+01
   Dimensionless distance   yplus :  0.42920E-01 0.33035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        355
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    2013   0.44916E-02   0.37558E+00 
c  VelocityY    0.29393E+04    2013   0.44916E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    2013   0.44916E-02   0.00000E+00 
c  Pressure     0.44660E+00    7056   0.33657E-01   0.21184E+00 
c  k            0.21597E+04    1307   0.11882E-03   0.96698E+00 
c  omega        0.10676E+08     452   0.44057E-04   0.27393E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1921e+05                             1
a  Local Time Step      1.0985e-05                         44452


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2172          1.6295      -0.0022342     -4.3985e-06
v  Velocity[Y]                 -38.957          30.135          6.6368          20.056
v  Velocity[Z]                 -28.589          28.856        0.069867       0.0013654
v  ǁVelocityǁ                0.0047805          40.428          10.585          20.216
v  Pressure                    -412.81          346.45         -51.963          31.401
v  k                        2.7248e-08          102.23            4.09          1.6762
v  omega                         1e-24      1.5868e+07          7906.7          11.872
v  turbulent_viscosity      1.5344e-13          1.2397        0.015685         0.11274
v  CourantNb                  0.003598          2010.2            44.6           1.377
v  FourierNb                  0.010855           15352          92.918          0.7074
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010824        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15412          137.52          2.0845


 TIME FOR THE TIME STEP              476:        0.46707E+02

===============================================================


 INSTANT    0.477000000E+02   TIME STEP NUMBER             477
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.122131493E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52821E+02 0.13759E+02
   Friction velocity        uet   :  0.16923E-02 0.35753E+01
   Friction velocity        uk    :  0.14602E-01 0.49082E+01
   Dimensionless distance   yplus :  0.12547E+00 0.40133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        391
   Nb of faces within the viscous sub-layer     :       1049
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2069   0.44296E-02   0.37886E+00 
c  VelocityY    0.29392E+04    2069   0.44296E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2069   0.44296E-02   0.00000E+00 
c  Pressure     0.43142E+00    6996   0.37818E-01   0.20575E+00 
c  k            0.21472E+04    1145   0.11948E-03   0.83035E+00 
c  omega        0.10470E+08     480   0.24425E-03   0.27315E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -67446                             1
a  Local Time Step      1.0324e-05                         44419


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2177           1.621       -0.001274     -7.2957e-06
v  Velocity[Y]                 -30.181          30.597          6.6413          20.056
v  Velocity[Z]                 -28.528           28.48          0.0768       0.0014168
v  ǁVelocityǁ                0.0090225          33.657          10.585          20.216
v  Pressure                    -412.64          345.33         -52.997          31.742
v  k                        1.2155e-09          51.574          4.1174          1.6741
v  omega                         1e-24      5.9767e+07          9185.4          11.965
v  turbulent_viscosity      3.5336e-14          1.2324        0.015704         0.11269
v  CourantNb                  0.026452            2375          44.805           1.377
v  FourierNb                  0.010854           15396          93.471         0.70789
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1491        0.010824        0.045692


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15472          138.28          2.0849


 TIME FOR THE TIME STEP              477:        0.46865E+02

===============================================================


 INSTANT    0.478000000E+02   TIME STEP NUMBER             478
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.151438531E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30222E+02 0.13398E+02
   Friction velocity        uet   :  0.76969E-03 0.29839E+01
   Friction velocity        uk    :  0.16798E-01 0.30873E+01
   Dimensionless distance   yplus :  0.14800E+00 0.27572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2077   0.43720E-02   0.38549E+00 
c  VelocityY    0.29392E+04    2077   0.43720E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2077   0.43720E-02   0.00000E+00 
c  Pressure     0.46161E+00    7110   0.37720E-01   0.22082E+00 
c  k            0.21353E+04     987   0.67600E-04   0.69696E+00 
c  omega        0.28125E+08     258   0.75183E-04   0.20000E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5571e+05                             2
a  Local Time Step      1.1543e-05                         44403


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.241          1.5776     -0.00043705     -1.0118e-05
v  Velocity[Y]                 -17.862          30.828          6.6606          20.056
v  Velocity[Z]                 -28.826          28.645        0.064154       0.0011859
v  ǁVelocityǁ                 0.006025          33.584          10.565          20.215
v  Pressure                    -412.11          344.53         -53.645          31.956
v  k                        1.3792e-08          49.971          4.1595          1.6717
v  omega                         1e-24      6.0021e+07          8945.2          11.946
v  turbulent_viscosity      2.1899e-15          1.2254        0.015743         0.11262
v  CourantNb                  0.052614          3037.4          45.025           1.377
v  FourierNb                  0.010851           15457          93.836         0.70825
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14794        0.010824        0.045692


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15526          138.86          2.0852


 TIME FOR THE TIME STEP              478:        0.46457E+02

===============================================================


 INSTANT    0.479000000E+02   TIME STEP NUMBER             479
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.476406629E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30718E+02 0.13390E+02
   Friction velocity        uet   :  0.22042E-02 0.28631E+01
   Friction velocity        uk    :  0.13573E-01 0.29132E+01
   Dimensionless distance   yplus :  0.10118E+00 0.28870E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        583
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2120   0.43757E-02   0.39677E+00 
c  VelocityY    0.29392E+04    2120   0.43757E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2120   0.43757E-02   0.00000E+00 
c  Pressure     0.44982E+00    7026   0.33920E-01   0.21459E+00 
c  k            0.21253E+04    1042   0.65436E-04   0.64644E+00 
c  omega        0.25227E+08     295   0.19179E-03   0.59958E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1449e-05                         44376


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5325          1.4849     -0.00038339     -9.6516e-06
v  Velocity[Y]                  -17.24          33.188          6.6884          20.056
v  Velocity[Z]                 -28.494          28.722        0.038235      0.00090206
v  ǁVelocityǁ                0.0021742          33.871          10.541          20.216
v  Pressure                     -411.2          345.19         -53.656          31.935
v  k                        2.5873e-08          54.899          4.2085          1.6691
v  omega                         1e-24      1.8427e+08          9336.9           11.95
v  turbulent_viscosity      2.8032e-14          1.2183        0.015783         0.11252
v  CourantNb                  0.029326          2038.3          44.761          1.3768
v  FourierNb                  0.010849           15506          95.501         0.70867
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14756        0.010822        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15568          140.26          2.0855


 TIME FOR THE TIME STEP              479:        0.46737E+02

===============================================================


 INSTANT    0.480000000E+02   TIME STEP NUMBER             480
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.236652386E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31636E+02 0.13806E+02
   Friction velocity        uet   :  0.22850E-02 0.29445E+01
   Friction velocity        uk    :  0.18816E-01 0.29709E+01
   Dimensionless distance   yplus :  0.14635E+00 0.32118E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        584
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2087   0.44302E-02   0.41802E+00 
c  VelocityY    0.29392E+04    2087   0.44302E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2087   0.44302E-02   0.00000E+00 
c  Pressure     0.43223E+00    6973   0.30838E-01   0.20542E+00 
c  k            0.21162E+04    1232   0.65548E-04   0.74230E+00 
c  omega        0.14046E+09     229   0.15724E-04   0.16250E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8632e+05                             1
a  Local Time Step      1.1397e-05                         44327


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6334          1.3602      -0.0010264     -7.4537e-06
v  Velocity[Y]                 -15.282          33.585           6.707          20.056
v  Velocity[Z]                 -28.449          28.774       0.0070243      0.00081755
v  ǁVelocityǁ                0.0043159          33.874          10.517          20.216
v  Pressure                    -403.69          343.35         -53.702          31.775
v  k                        7.9687e-08          52.032          4.2002          1.6662
v  omega                         1e-24      9.2382e+07            8672          11.916
v  turbulent_viscosity        8.57e-15          1.2136        0.015815         0.11239
v  CourantNb                  0.041616          2067.1          44.371          1.3766
v  FourierNb                  0.010848           15535          97.914         0.70908
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010822        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15600          142.29          2.0857


 TIME FOR THE TIME STEP              480:        0.46607E+02

===============================================================


 INSTANT    0.481000000E+02   TIME STEP NUMBER             481
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.506678896E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32120E+02 0.15226E+02
   Friction velocity        uet   :  0.19918E-03 0.28678E+01
   Friction velocity        uk    :  0.11947E-01 0.32468E+01
   Dimensionless distance   yplus :  0.11959E+00 0.37468E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    2016   0.46133E-02   0.43010E+00 
c  VelocityY    0.29391E+04    2016   0.46133E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    2016   0.46133E-02   0.00000E+00 
c  Pressure     0.43291E+00    6894   0.31506E-01   0.20665E+00 
c  k            0.21057E+04    1296   0.59672E-04   0.68271E+00 
c  omega        0.37151E+08     239   0.71728E-04   0.19341E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3294e+05                             2
a  Local Time Step      1.1856e-05                         44334


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6645          1.3302      -0.0023172     -4.6514e-06
v  Velocity[Y]                 -14.576          33.983          6.6786          20.056
v  Velocity[Z]                 -28.439          28.884       -0.021586      0.00024951
v  ǁVelocityǁ                0.0055303          34.292          10.512          20.216
v  Pressure                    -386.59          342.36         -54.024          31.337
v  k                        5.5067e-08          41.721          4.1803          1.6633
v  omega                         1e-24      8.3455e+07          8853.1          11.916
v  turbulent_viscosity      9.5414e-15          1.2135        0.015824         0.11224
v  CourantNb                  0.042924            2083          44.059          1.3766
v  FourierNb                  0.010846           15517          97.418         0.70844
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010823         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15582          141.48           2.085


 TIME FOR THE TIME STEP              481:        0.46224E+02

===============================================================


 INSTANT    0.482000000E+02   TIME STEP NUMBER             482
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.180188806E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32318E+02 0.22398E+02
   Friction velocity        uet   :  0.17717E-02 0.27346E+01
   Friction velocity        uk    :  0.20978E-01 0.32474E+01
   Dimensionless distance   yplus :  0.15517E+00 0.37671E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1984   0.45596E-02   0.43793E+00 
c  VelocityY    0.29389E+04    1984   0.45596E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1984   0.45596E-02   0.00000E+00 
c  Pressure     0.43413E+00    6860   0.30371E-01   0.20715E+00 
c  k            0.20964E+04    1315   0.56244E-04   0.69913E+00 
c  omega        0.34071E+08     186   0.37191E-04   0.58393E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step        1.13e-05                         44287


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0741          1.3064      -0.0031561     -2.5909e-06
v  Velocity[Y]                 -16.926          31.985           6.655          20.056
v  Velocity[Z]                 -28.618           28.88       -0.029411     -0.00035721
v  ǁVelocityǁ                0.0055174          33.252          10.504          20.216
v  Pressure                    -371.91          342.44         -53.722          31.175
v  k                        2.7023e-10          41.965          4.1529          1.6603
v  omega                         1e-24      4.2309e+07          8483.9          11.883
v  turbulent_viscosity      1.3896e-15          1.2169        0.015828         0.11207
v  CourantNb                  0.034869          2087.4          43.825          1.3767
v  FourierNb                  0.010845           15572          96.605         0.70743
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010824        0.045758


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15632          140.43          2.0842


 TIME FOR THE TIME STEP              482:        0.45242E+02

===============================================================


 INSTANT    0.483000000E+02   TIME STEP NUMBER             483
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.333890462E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30356E+02 0.20878E+02
   Friction velocity        uet   :  0.14046E-03 0.26664E+01
   Friction velocity        uk    :  0.17987E-01 0.32056E+01
   Dimensionless distance   yplus :  0.15528E+00 0.30711E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        517
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1957   0.45122E-02   0.43334E+00 
c  VelocityY    0.29389E+04    1957   0.45122E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1957   0.45122E-02   0.00000E+00 
c  Pressure     0.42952E+00    6951   0.29138E-01   0.20544E+00 
c  k            0.20892E+04    1363   0.61516E-04   0.80941E+00 
c  omega        0.13683E+08     207   0.43829E-04   0.16663E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2277e-05                         44267


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0962          1.1587      -0.0033009      1.0008e-07
v  Velocity[Y]                 -15.088          30.495          6.6584          20.057
v  Velocity[Z]                 -31.382          29.419       -0.032342      -0.0003799
v  ǁVelocityǁ                 0.013107          36.429          10.503          20.216
v  Pressure                    -345.19          343.94         -52.388          31.415
v  k                        1.6824e-08           48.87          4.1328          1.6574
v  omega                         1e-24       2.233e+07          8157.3          11.847
v  turbulent_viscosity      6.5422e-16          1.2221        0.015838         0.11188
v  CourantNb                  0.038408          2082.1          44.035          1.3769
v  FourierNb                  0.010843           15672          96.179         0.70637
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010822        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15729          140.21          2.0833


 TIME FOR THE TIME STEP              483:        0.45696E+02

===============================================================


 INSTANT    0.484000000E+02   TIME STEP NUMBER             484
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.158760080E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31247E+02 0.17904E+02
   Friction velocity        uet   :  0.32567E-02 0.30421E+01
   Friction velocity        uk    :  0.61729E-02 0.30673E+01
   Dimensionless distance   yplus :  0.78181E-01 0.27302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1945   0.42891E-02   0.42009E+00 
c  VelocityY    0.29389E+04    1945   0.42891E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1945   0.42891E-02   0.00000E+00 
c  Pressure     0.43860E+00    7013   0.31606E-01   0.20836E+00 
c  k            0.20860E+04    1360   0.69755E-04   0.95664E+00 
c  omega        0.10761E+08     327   0.33548E-04   0.74497E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1771e-05                         44320


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1009         0.90104      -0.0027754      1.1522e-06
v  Velocity[Y]                 -15.169          30.435          6.6951          20.057
v  Velocity[Z]                 -31.646          29.196       -0.021645      -0.0010796
v  ǁVelocityǁ                0.0088448           36.32          10.532          20.216
v  Pressure                    -398.52          345.73          -51.34          31.619
v  k                        8.0411e-09          60.811           4.117          1.6546
v  omega                         1e-24      1.3486e+07          8050.2          11.838
v  turbulent_viscosity      6.6897e-15          1.2297        0.015842         0.11168
v  CourantNb                  0.046394          2068.1          44.049          1.3768
v  FourierNb                  0.010841           15808          95.119         0.70493
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010822        0.045749


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15866          139.17          2.0817


 TIME FOR THE TIME STEP              484:        0.45776E+02

===============================================================


 INSTANT    0.485000000E+02   TIME STEP NUMBER             485
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.198582739E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31056E+02 0.14118E+02
   Friction velocity        uet   :  0.11394E-02 0.31044E+01
   Friction velocity        uk    :  0.60456E-02 0.31228E+01
   Dimensionless distance   yplus :  0.83281E-01 0.27350E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1968   0.44563E-02   0.42096E+00 
c  VelocityY    0.29389E+04    1968   0.44563E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1968   0.44563E-02   0.00000E+00 
c  Pressure     0.40837E+00    7092   0.35410E-01   0.19320E+00 
c  k            0.20895E+04    1258   0.72838E-04   0.10619E+01 
c  omega        0.10370E+08     215   0.38654E-04   0.72044E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.2106e-05                         44340


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0801          1.0287      -0.0018512      2.6684e-06
v  Velocity[Y]                 -15.141          31.635           6.753          20.056
v  Velocity[Z]                 -32.467          28.968        0.018692      -0.0019194
v  ǁVelocityǁ                0.0099543          34.543          10.586          20.216
v  Pressure                    -432.35          347.64         -50.215          31.865
v  k                        6.6562e-08          67.924          4.0956          1.6519
v  omega                         1e-24      1.1697e+07          7939.9          11.837
v  turbulent_viscosity      4.0228e-14          1.2381        0.015827         0.11146
v  CourantNb                  0.043428          2518.4          44.065          1.3767
v  FourierNb                   0.01084           15871           94.77         0.70326
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010822        0.045752


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15931          138.84            2.08


 TIME FOR THE TIME STEP              485:        0.45820E+02

===============================================================


 INSTANT    0.486000000E+02   TIME STEP NUMBER             486
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.513513757E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30829E+02 0.15404E+02
   Friction velocity        uet   :  0.14430E-02 0.31338E+01
   Friction velocity        uk    :  0.14169E-01 0.30129E+01
   Dimensionless distance   yplus :  0.82096E-01 0.27355E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1863   0.45200E-02   0.42247E+00 
c  VelocityY    0.29390E+04    1863   0.45200E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1863   0.45200E-02   0.00000E+00 
c  Pressure     0.40543E+00    7107   0.37701E-01   0.19216E+00 
c  k            0.20989E+04    1426   0.72703E-04   0.11012E+01 
c  omega        0.10267E+08     277   0.25944E-03   0.20515E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1695e-05                         44353


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0485          1.2408     -0.00070231      4.7681e-06
v  Velocity[Y]                 -21.241          30.086          6.8103          20.056
v  Velocity[Z]                 -32.802          28.875        0.079137       -0.002697
v  ǁVelocityǁ                 0.012452          34.196          10.615          20.216
v  Pressure                    -441.45          347.88         -49.757          32.103
v  k                        6.9366e-07          64.595          4.0482          1.6491
v  omega                         1e-24      8.5622e+07            8540          11.888
v  turbulent_viscosity      3.1743e-14           1.245          0.0158         0.11123
v  CourantNb                  0.024226          2731.1          44.316          1.3768
v  FourierNb                   0.01084           15815          94.456         0.70159
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14894        0.010823        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0023           15880          138.77          2.0784


 TIME FOR THE TIME STEP              486:        0.45153E+02

===============================================================


 INSTANT    0.487000000E+02   TIME STEP NUMBER             487
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.218678893E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29557E+02 0.14609E+02
   Friction velocity        uet   :  0.73496E-03 0.29194E+01
   Friction velocity        uk    :  0.18766E-01 0.29779E+01
   Dimensionless distance   yplus :  0.19567E+00 0.27091E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        377
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1814   0.45452E-02   0.38805E+00 
c  VelocityY    0.29391E+04    1814   0.45452E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1814   0.45452E-02   0.00000E+00 
c  Pressure     0.45860E+00    7056   0.35859E-01   0.21700E+00 
c  k            0.21096E+04    1496   0.70693E-04   0.11397E+01 
c  omega        0.40231E+08     137   0.35597E-04   0.88300E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -86734                             1
a  Local Time Step      1.1546e-05                         44339


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.218          1.4492      0.00019728      4.2074e-06
v  Velocity[Y]                 -24.294          29.895          6.8129          20.057
v  Velocity[Z]                 -32.729           28.78          0.1466      -0.0029762
v  ǁVelocityǁ                 0.015222          33.459          10.585          20.216
v  Pressure                    -431.29          347.68         -49.329          32.297
v  k                        3.7337e-07          64.143          3.9903          1.6464
v  omega                         1e-24      4.3452e+07          8485.6          11.879
v  turbulent_viscosity      7.7292e-14          1.2528        0.015746           0.111
v  CourantNb                  0.041838          2440.1          44.628          1.3771
v  FourierNb                   0.01084           15730          93.602         0.69946
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14792        0.010824         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98889           15794          138.23          2.0765


 TIME FOR THE TIME STEP              487:        0.44174E+02

===============================================================


 INSTANT    0.488000000E+02   TIME STEP NUMBER             488
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.208628384E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31168E+02 0.14640E+02
   Friction velocity        uet   :  0.10163E-02 0.28553E+01
   Friction velocity        uk    :  0.20914E-01 0.30897E+01
   Dimensionless distance   yplus :  0.16801E+00 0.27178E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        315
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1882   0.44123E-02   0.34539E+00 
c  VelocityY    0.29393E+04    1882   0.44123E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1882   0.44123E-02   0.00000E+00 
c  Pressure     0.45478E+00    7051   0.32123E-01   0.21619E+00 
c  k            0.21172E+04    1499   0.80038E-04   0.11071E+01 
c  omega        0.15267E+08     180   0.79288E-04   0.96186E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3502e+05                             1
a  Local Time Step      1.1736e-05                         44337


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4014          1.5946      0.00020674      4.0236e-06
v  Velocity[Y]                 -34.427          29.733          6.7415          20.056
v  Velocity[Z]                 -29.107          28.491         0.17976      -0.0031896
v  ǁVelocityǁ                 0.012758          34.595          10.554          20.216
v  Pressure                    -406.71          346.52         -49.047          32.231
v  k                        3.3407e-08          89.254          3.9899          1.6437
v  omega                         1e-24      4.4767e+07          8577.6          11.909
v  turbulent_viscosity      1.7202e-13           1.261        0.015702         0.11076
v  CourantNb                  0.051123          2063.1          44.704          1.3771
v  FourierNb                  0.010841           15720          92.969         0.69749
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14777        0.010823        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89646           15781          137.67          2.0746


 TIME FOR THE TIME STEP              488:        0.44720E+02

===============================================================


 INSTANT    0.489000000E+02   TIME STEP NUMBER             489
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.757518232E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30628E+02 0.23386E+02
   Friction velocity        uet   :  0.68054E-03 0.29898E+01
   Friction velocity        uk    :  0.20000E-01 0.31813E+01
   Dimensionless distance   yplus :  0.16303E+00 0.27289E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        345
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1945   0.46102E-02   0.32222E+00 
c  VelocityY    0.29393E+04    1945   0.46102E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1945   0.46102E-02   0.00000E+00 
c  Pressure     0.43815E+00    7000   0.31771E-01   0.20757E+00 
c  k            0.21179E+04    1438   0.10194E-03   0.97927E+00 
c  omega        0.16618E+08     331   0.59313E-04   0.61568E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1274e+05                             2
a  Local Time Step      1.1483e-05                         44300


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4666          1.7055     -0.00022796       2.252e-06
v  Velocity[Y]                 -31.848          29.897          6.6714          20.056
v  Velocity[Z]                 -28.577          28.415         0.19404      -0.0036884
v  ǁVelocityǁ                0.0089676          38.433          10.551          20.216
v  Pressure                    -403.02          345.58         -49.331          32.215
v  k                        5.8183e-09          114.55          4.0496          1.6413
v  omega                         1e-24      2.2339e+07          8689.3          11.954
v  turbulent_viscosity      2.3714e-14          1.2693         0.01568         0.11052
v  CourantNb                  0.017711          2056.1           44.74          1.3771
v  FourierNb                  0.010842           15681           92.73         0.69618
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14733        0.010822        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96711           15741          137.47          2.0733


 TIME FOR THE TIME STEP              489:        0.47325E+02

===============================================================


 INSTANT    0.490000000E+02   TIME STEP NUMBER             490
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.422053687E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54797E+02 0.13466E+02
   Friction velocity        uet   :  0.19505E-02 0.33381E+01
   Friction velocity        uk    :  0.11358E-01 0.44202E+01
   Dimensionless distance   yplus :  0.86095E-01 0.33905E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1957   0.44511E-02   0.31641E+00 
c  VelocityY    0.29393E+04    1957   0.44511E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1957   0.44511E-02   0.00000E+00 
c  Pressure     0.44914E+00    7106   0.35250E-01   0.21233E+00 
c  k            0.21139E+04    1321   0.10459E-03   0.82769E+00 
c  omega        0.16889E+08     412   0.51677E-02   0.47124E+12 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8893e+05                             2
a  Local Time Step       1.134e-05                         44303


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4204          1.7035     -0.00046548     -1.0389e-06
v  Velocity[Y]                 -32.074          30.088          6.6482          20.057
v  Velocity[Z]                 -28.594          28.406         0.19549      -0.0044822
v  ǁVelocityǁ                 0.010027          33.393           10.54          20.217
v  Pressure                    -404.98          344.56         -50.268          32.398
v  k                        6.9886e-10          88.002           4.086          1.6392
v  omega                         1e-24      4.8552e+09           22403          13.033
v  turbulent_viscosity      1.4666e-14          1.2761        0.015694         0.11029
v  CourantNb                  0.033745          2047.3          44.817          1.3772
v  FourierNb                  0.010842           15599          93.173         0.69549
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14789        0.010822        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15661          137.99          2.0727


 TIME FOR THE TIME STEP              490:        0.46644E+02

===============================================================


 INSTANT    0.491000000E+02   TIME STEP NUMBER             491
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.308243892E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31536E+02 0.14654E+02
   Friction velocity        uet   :  0.10010E-02 0.31111E+01
   Friction velocity        uk    :  0.12667E-01 0.33086E+01
   Dimensionless distance   yplus :  0.15921E+00 0.38016E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :       1047
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1961   0.44404E-02   0.31227E+00 
c  VelocityY    0.29393E+04    1961   0.44404E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1961   0.44404E-02   0.00000E+00 
c  Pressure     0.41244E+00    7137   0.37370E-01   0.19441E+00 
c  k            0.21094E+04    1218   0.73273E-04   0.73738E+00 
c  omega        0.14101E+12      20   0.28967E-06   0.12025E+12 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1372e-05                         44302


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3421          1.6415     -0.00018608      -3.039e-07
v  Velocity[Y]                 -17.922          30.661          6.6446          20.056
v  Velocity[Z]                 -28.478          28.341           0.178       -0.005073
v  ǁVelocityǁ                 0.010996          33.427          10.521          20.217
v  Pressure                    -406.81          343.64         -51.213          32.323
v  k                        4.6805e-09          48.482          4.1147          1.6374
v  omega                         1e-24      2.4276e+09           17551          12.639
v  turbulent_viscosity      1.1441e-15          1.2815         0.01572         0.11006
v  CourantNb                  0.010423          3136.4          45.075          1.3772
v  FourierNb                  0.010842           15521          92.802         0.69454
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14912        0.010823        0.045758


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15585          137.88          2.0717


 TIME FOR THE TIME STEP              491:        0.47106E+02

===============================================================


 INSTANT    0.492000000E+02   TIME STEP NUMBER             492
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.113645791E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30885E+02 0.13218E+02
   Friction velocity        uet   :  0.10767E-02 0.27913E+01
   Friction velocity        uk    :  0.13835E-01 0.33213E+01
   Dimensionless distance   yplus :  0.18247E+00 0.38163E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        532
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1979   0.43874E-02   0.32160E+00 
c  VelocityY    0.29393E+04    1979   0.43874E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1979   0.43874E-02   0.00000E+00 
c  Pressure     0.42007E+00    7111   0.36097E-01   0.19934E+00 
c  k            0.21062E+04    1328   0.60923E-04   0.63053E+00 
c  omega        0.35256E+11      15   0.54499E-06   0.30103E+11 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0659e-05                         44288


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.286          1.5929      7.5827e-05     -9.7945e-07
v  Velocity[Y]                 -17.273          32.467          6.6546          20.056
v  Velocity[Z]                  -28.53          28.568         0.13756      -0.0054502
v  ǁVelocityǁ                0.0071793          33.913          10.495          20.217
v  Pressure                    -406.97          343.08         -51.542            32.4
v  k                        6.3015e-08          45.739          4.1949          1.6359
v  omega                         1e-24      1.2138e+09           12886           12.26
v  turbulent_viscosity      6.9409e-15          1.2851        0.015775         0.10985
v  CourantNb                  0.042874          2302.4          44.756           1.377
v  FourierNb                  0.010843           15395           94.13         0.69408
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010823        0.045787


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97884           15461          138.89           2.071


 TIME FOR THE TIME STEP              492:        0.45869E+02

===============================================================


 INSTANT    0.493000000E+02   TIME STEP NUMBER             493
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.174396474E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30469E+02 0.13135E+02
   Friction velocity        uet   :  0.28811E-03 0.29094E+01
   Friction velocity        uk    :  0.15948E-01 0.31682E+01
   Dimensionless distance   yplus :  0.15790E+00 0.29159E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        576
   Nb of faces within the viscous sub-layer     :       1042
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2010   0.44811E-02   0.34369E+00 
c  VelocityY    0.29394E+04    2010   0.44811E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2010   0.44811E-02   0.00000E+00 
c  Pressure     0.43195E+00    6985   0.34739E-01   0.20416E+00 
c  k            0.21034E+04    1444   0.67047E-04   0.69517E+00 
c  omega        0.88136E+10      29   0.10885E-05   0.75734E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1399e-05                         44302


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1979          1.5309      0.00015265      5.1494e-07
v  Velocity[Y]                 -16.209          33.504          6.6708          20.057
v  Velocity[Z]                 -28.276          28.801        0.085123       -0.005887
v  ǁVelocityǁ                 0.014561          33.689          10.485          20.218
v  Pressure                    -402.81          342.18          -51.71          32.165
v  k                        8.9205e-09          53.297          4.2522          1.6348
v  omega                         1e-24      6.0685e+08           10605          12.098
v  turbulent_viscosity      6.1191e-17           1.288        0.015865         0.10964
v  CourantNb                  0.015892          2031.7          44.193          1.3767
v  FourierNb                  0.010843           15263           96.11         0.69418
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010822        0.045798


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15332           140.3          2.0709


 TIME FOR THE TIME STEP              493:        0.46061E+02

===============================================================


 INSTANT    0.494000000E+02   TIME STEP NUMBER             494
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.268997018E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31565E+02 0.14803E+02
   Friction velocity        uet   :  0.47532E-03 0.28784E+01
   Friction velocity        uk    :  0.17297E-01 0.28054E+01
   Dimensionless distance   yplus :  0.11501E+00 0.32111E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :       1042
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2026   0.44870E-02   0.37894E+00 
c  VelocityY    0.29394E+04    2026   0.44870E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2026   0.44870E-02   0.00000E+00 
c  Pressure     0.47263E+00    6917   0.32413E-01   0.22497E+00 
c  k            0.21000E+04    1489   0.62316E-04   0.72421E+00 
c  omega        0.22224E+10      37   0.21550E-05   0.19080E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.138e-05                         44279


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0088          1.4736     -2.8041e-05      2.3949e-06
v  Velocity[Y]                 -15.153          33.322          6.6692          20.056
v  Velocity[Z]                  -28.36          29.011        0.023996      -0.0058815
v  ǁVelocityǁ                 0.024002          33.421          10.485          20.217
v  Pressure                    -386.89          341.08         -52.403          31.508
v  k                        1.4461e-09          44.179          4.2477          1.6339
v  omega                         1e-24      3.0341e+08          9517.6          11.993
v  turbulent_viscosity      7.7135e-17          1.2912        0.015951         0.10945
v  CourantNb                  0.043323          2027.6          43.833          1.3767
v  FourierNb                  0.010843           15398          97.551         0.69435
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14937        0.010823        0.045776


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15444          141.38           2.071


 TIME FOR THE TIME STEP              494:        0.46118E+02

===============================================================


 INSTANT    0.495000000E+02   TIME STEP NUMBER             495
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.177779047E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31285E+02 0.22632E+02
   Friction velocity        uet   :  0.14626E-02 0.27370E+01
   Friction velocity        uk    :  0.93562E-02 0.30647E+01
   Dimensionless distance   yplus :  0.12888E+00 0.37699E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        534
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2031   0.46438E-02   0.40431E+00 
c  VelocityY    0.29394E+04    2031   0.46438E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2031   0.46438E-02   0.00000E+00 
c  Pressure     0.42095E+00    6987   0.30510E-01   0.19994E+00 
c  k            0.20968E+04    1530   0.58909E-04   0.70569E+00 
c  omega        0.55102E+09      76   0.43703E-05   0.48695E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1163e-05                         44243


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7031          1.4703     -7.7249e-06      2.6839e-06
v  Velocity[Y]                 -15.374          32.028          6.6375          20.056
v  Velocity[Z]                 -28.313          29.167       -0.016767      -0.0059007
v  ǁVelocityǁ                  0.01374          32.972          10.478          20.217
v  Pressure                     -372.8          342.21         -52.664          31.098
v  k                        1.6444e-10          38.791          4.2268          1.6335
v  omega                         1e-24       1.517e+08          8870.6          11.931
v  turbulent_viscosity      1.0254e-15          1.2938        0.015997         0.10927
v  CourantNb                  0.034874          2025.5          43.655          1.3769
v  FourierNb                  0.010844           15776          97.955         0.69352
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010823        0.045764


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.003           15822          141.61          2.0704


 TIME FOR THE TIME STEP              495:        0.47110E+02

===============================================================


 INSTANT    0.496000000E+02   TIME STEP NUMBER             496
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.159774750E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30041E+02 0.20697E+02
   Friction velocity        uet   :  0.22278E-02 0.25799E+01
   Friction velocity        uk    :  0.17488E-01 0.29796E+01
   Dimensionless distance   yplus :  0.10840E+00 0.30422E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        549
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2033   0.44360E-02   0.43313E+00 
c  VelocityY    0.29394E+04    2033   0.44360E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2033   0.44360E-02   0.00000E+00 
c  Pressure     0.43488E+00    6988   0.29668E-01   0.20816E+00 
c  k            0.20953E+04    1587   0.62303E-04   0.77060E+00 
c  omega        0.13817E+09     102   0.90282E-05   0.12924E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1253e-05                         44273


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3128           1.479     -0.00078917      2.6684e-06
v  Velocity[Y]                 -15.155          30.415          6.6275          20.056
v  Velocity[Z]                 -30.121          28.888       -0.041948      -0.0058797
v  ǁVelocityǁ                 0.009514          35.695          10.477          20.217
v  Pressure                     -354.8          343.95         -52.237          31.005
v  k                         2.535e-10          46.218          4.2095          1.6333
v  omega                         1e-24      7.5882e+07          8426.9          11.884
v  turbulent_viscosity      8.7773e-17          1.2951        0.016016         0.10911
v  CourantNb                  0.059308            2022          43.579           1.377
v  FourierNb                  0.010845           16067           97.46          0.6922
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14809         0.01082        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16117          141.04          2.0692


 TIME FOR THE TIME STEP              496:        0.47698E+02

===============================================================


 INSTANT    0.497000000E+02   TIME STEP NUMBER             497
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.162084784E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29136E+02 0.21108E+02
   Friction velocity        uet   :  0.61060E-03 0.29441E+01
   Friction velocity        uk    :  0.18588E-01 0.32267E+01
   Dimensionless distance   yplus :  0.86138E-01 0.27581E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        539
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2081   0.42996E-02   0.45801E+00 
c  VelocityY    0.29394E+04    2081   0.42996E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2081   0.42996E-02   0.00000E+00 
c  Pressure     0.42744E+00    7033   0.31338E-01   0.20374E+00 
c  k            0.20964E+04    1583   0.69127E-04   0.89798E+00 
c  omega        0.36023E+08     157   0.26338E-04   0.44168E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.233e+05                             2
a  Local Time Step      1.1865e-05                         44314


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89859          1.5037      -0.0015837      1.9634e-06
v  Velocity[Y]                 -14.997          31.729          6.6477          20.056
v  Velocity[Z]                 -31.847          28.947       -0.067645      -0.0062052
v  ǁVelocityǁ                 0.010802          37.818          10.489          20.217
v  Pressure                    -382.69          346.32         -51.055          31.134
v  k                        2.1998e-09          55.841          4.2027          1.6336
v  omega                         1e-24      3.8045e+07          8098.5          11.836
v  turbulent_viscosity      1.1491e-16          1.2957        0.016032         0.10896
v  CourantNb                  0.057321          2017.2          43.689           1.377
v  FourierNb                  0.010846           16320          96.696         0.69103
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14866        0.010819         0.04573


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16377          140.39           2.068


 TIME FOR THE TIME STEP              497:        0.46835E+02

===============================================================


 INSTANT    0.498000000E+02   TIME STEP NUMBER             498
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.313924555E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30350E+02 0.19059E+02
   Friction velocity        uet   :  0.15708E-02 0.31133E+01
   Friction velocity        uk    :  0.22488E-01 0.29687E+01
   Dimensionless distance   yplus :  0.16553E+00 0.27580E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    2149   0.44882E-02   0.48053E+00 
c  VelocityY    0.29395E+04    2149   0.44882E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    2149   0.44882E-02   0.00000E+00 
c  Pressure     0.41681E+00    6996   0.35901E-01   0.19773E+00 
c  k            0.21020E+04    1462   0.75466E-04   0.10249E+01 
c  omega        0.17368E+08     195   0.29086E-04   0.13892E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1925e-05                         44292


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94113          1.5174         -0.0023      2.6435e-06
v  Velocity[Y]                 -15.458          33.172          6.6996          20.057
v  Velocity[Z]                 -33.293          28.905       -0.067096      -0.0060321
v  ǁVelocityǁ                 0.013497          35.615          10.527          20.218
v  Pressure                    -431.92          347.12         -50.442          31.325
v  k                        1.0455e-09          64.448          4.1757           1.634
v  omega                         1e-24      1.9273e+07          7845.1          11.818
v  turbulent_viscosity      1.9775e-15          1.2956        0.016032         0.10883
v  CourantNb                  0.038051          2333.4          43.692          1.3769
v  FourierNb                  0.010847           16437          96.584         0.69002
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14819        0.010819        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16506          140.28          2.0669


 TIME FOR THE TIME STEP              498:        0.48421E+02

===============================================================


 INSTANT    0.499000000E+02   TIME STEP NUMBER             499
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.605790974E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30203E+02 0.16169E+02
   Friction velocity        uet   :  0.27709E-02 0.32037E+01
   Friction velocity        uk    :  0.22243E-01 0.30384E+01
   Dimensionless distance   yplus :  0.98424E-01 0.27235E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2249   0.46278E-02   0.49951E+00 
c  VelocityY    0.29396E+04    2249   0.46278E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2249   0.46278E-02   0.00000E+00 
c  Pressure     0.42979E+00    7102   0.39123E-01   0.20371E+00 
c  k            0.21125E+04    1350   0.76640E-04   0.10891E+01 
c  omega        0.11620E+08     256   0.22439E-03   0.18746E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1951e-05                         44257


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.094          1.5285      -0.0028022     -1.0986e-06
v  Velocity[Y]                 -18.631           30.17          6.7591          20.056
v  Velocity[Z]                 -33.043          28.749       -0.023276      -0.0054525
v  ǁVelocityǁ                 0.013526          34.835          10.558          20.217
v  Pressure                    -451.27          346.73         -50.051          31.419
v  k                        1.0498e-07          64.787          4.1264          1.6347
v  omega                         1e-24      8.3566e+07          8376.6          11.862
v  turbulent_viscosity      3.9035e-15          1.2934        0.016004         0.10872
v  CourantNb                  0.042421          2746.6          43.839          1.3768
v  FourierNb                  0.010849           16479          96.499         0.68897
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14816        0.010819        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16556          140.34          2.0657


 TIME FOR THE TIME STEP              499:        0.49079E+02

===============================================================


 INSTANT    0.500000000E+02   TIME STEP NUMBER             500
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.265388128E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30066E+02 0.15359E+02
   Friction velocity        uet   :  0.67230E-03 0.29926E+01
   Friction velocity        uk    :  0.25770E-01 0.30646E+01
   Dimensionless distance   yplus :  0.15268E+00 0.27535E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :        958
   Total number of wall faces                   :       7680
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        500, Physical time    0.50000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 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                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
   End writing the wall distance                        
 End writing


 Time for restart files:    0.18277E+01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2279   0.44853E-02   0.48847E+00 
c  VelocityY    0.29397E+04    2279   0.44853E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2279   0.44853E-02   0.00000E+00 
c  Pressure     0.45408E+00    7095   0.37625E-01   0.21651E+00 
c  k            0.21236E+04    1490   0.76268E-04   0.11173E+01 
c  omega        0.30339E+27       2   0.11325E-15   0.58721E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -84784                             1
a  Local Time Step       1.104e-05                         44278


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.373          1.4932       -0.002693     -3.4995e-06
v  Velocity[Y]                 -24.627          30.009          6.7822          20.056
v  Velocity[Z]                 -31.678          28.704        0.027279       -0.004755
v  ǁVelocityǁ                 0.010446          33.023          10.549          20.217
v  Pressure                    -447.57          345.95         -49.826           31.47
v  k                        1.5335e-06          54.769          4.0596          1.6353
v  omega                         1e-24      4.2414e+07          8051.9          11.846
v  turbulent_viscosity      4.0477e-13          1.2896        0.015935         0.10862
v  CourantNb                  0.039831          2656.1          44.151          1.3768
v  FourierNb                  0.010851           16410          95.488         0.68762
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14928        0.010819        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96752           16491          139.64          2.0644


 TIME FOR THE TIME STEP              500:        0.51322E+02

===============================================================


 INSTANT    0.501000000E+02   TIME STEP NUMBER             501
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.475481945E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.28994E+02 0.13683E+02
   Friction velocity        uet   :  0.13582E-02 0.27963E+01
   Friction velocity        uk    :  0.22910E-01 0.31445E+01
   Dimensionless distance   yplus :  0.11708E+00 0.27597E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2242   0.46110E-02   0.45458E+00 
c  VelocityY    0.29397E+04    2242   0.46110E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2242   0.46110E-02   0.00000E+00 
c  Pressure     0.42815E+00    7029   0.33542E-01   0.20427E+00 
c  k            0.21317E+04    1601   0.79160E-04   0.11995E+01 
c  omega        0.13673E+08     237   0.10542E-03   0.79309E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3394e+05                             1
a  Local Time Step      1.1382e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5219          1.4228      -0.0014989      -3.407e-06
v  Velocity[Y]                 -30.651          29.842          6.7361          20.056
v  Velocity[Z]                 -30.825          28.701        0.063155       -0.004346
v  ǁVelocityǁ                 0.014794          33.085          10.529          20.217
v  Pressure                    -427.34          346.77         -49.546          31.489
v  k                        1.9866e-07          66.409          4.0277           1.636
v  omega                         1e-24      4.9436e+07          8339.3          11.886
v  turbulent_viscosity      6.3366e-13          1.2851        0.015848         0.10856
v  CourantNb                  0.050944          2031.2           44.38          1.3769
v  FourierNb                  0.010853           16288          94.129         0.68628
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14852        0.010819        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16348          138.51          2.0631


 TIME FOR THE TIME STEP              501:        0.49794E+02

===============================================================


 INSTANT    0.502000000E+02   TIME STEP NUMBER             502
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.402730814E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30627E+02 0.21763E+02
   Friction velocity        uet   :  0.15536E-02 0.28234E+01
   Friction velocity        uk    :  0.22491E-01 0.31682E+01
   Dimensionless distance   yplus :  0.13264E+00 0.27614E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :        939
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2261   0.46056E-02   0.43473E+00 
c  VelocityY    0.29396E+04    2261   0.46056E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2261   0.46056E-02   0.00000E+00 
c  Pressure     0.45386E+00    7060   0.32550E-01   0.21486E+00 
c  k            0.21337E+04    1566   0.10057E-03   0.99710E+00 
c  omega        0.14830E+08     301   0.58365E-04   0.64224E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4449e+05                             1
a  Local Time Step      1.0347e-05                         44329


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6689          1.3676     -0.00015384     -5.2002e-06
v  Velocity[Y]                 -23.587          29.851          6.6547          20.056
v  Velocity[Z]                 -29.034          28.807        0.069958      -0.0036953
v  ǁVelocityǁ                0.0046411          33.224          10.542          20.217
v  Pressure                    -408.98           346.4         -50.088          31.514
v  k                        9.5633e-08           100.5          4.0631          1.6368
v  omega                         1e-24       2.594e+07          8228.7          11.876
v  turbulent_viscosity      6.9377e-14          1.2821        0.015772         0.10851
v  CourantNb                  0.011374          2057.1          44.417          1.3767
v  FourierNb                  0.010854           16031          93.533         0.68543
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14937        0.010819        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16096          137.95          2.0621


 TIME FOR THE TIME STEP              502:        0.50432E+02

===============================================================


 INSTANT    0.503000000E+02   TIME STEP NUMBER             503
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.446392766E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30437E+02 0.18422E+02
   Friction velocity        uet   :  0.42378E-03 0.26267E+01
   Friction velocity        uk    :  0.14607E-01 0.36613E+01
   Dimensionless distance   yplus :  0.10009E+00 0.34991E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2247   0.45756E-02   0.43112E+00 
c  VelocityY    0.29397E+04    2247   0.45756E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2247   0.45756E-02   0.00000E+00 
c  Pressure     0.45406E+00    6993   0.36470E-01   0.21564E+00 
c  k            0.21293E+04    1535   0.13612E-03   0.83360E+00 
c  omega        0.12320E+08     508   0.23932E-03   0.28137E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5361e+05                             1
a  Local Time Step      1.1155e-05                         44302


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.735          1.4236      0.00041561     -5.0742e-06
v  Velocity[Y]                 -35.931          30.159          6.6349          20.056
v  Velocity[Z]                 -28.464          28.541        0.076114      -0.0031063
v  ǁVelocityǁ                 0.012797          36.377          10.557          20.217
v  Pressure                    -410.05          345.57         -51.486          31.588
v  k                        7.8801e-09          93.918          4.1312          1.6379
v  omega                         1e-24      5.7417e+07          9338.6          11.961
v  turbulent_viscosity      1.3371e-13          1.2794        0.015745         0.10847
v  CourantNb                   0.01486            2071          44.511          1.3765
v  FourierNb                  0.010856           15890          93.777         0.68554
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14907        0.010819        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15959          138.29          2.0621


 TIME FOR THE TIME STEP              503:        0.49562E+02

===============================================================


 INSTANT    0.504000000E+02   TIME STEP NUMBER             504
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.218551209E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40625E+02 0.12788E+02
   Friction velocity        uet   :  0.18951E-02 0.33809E+01
   Friction velocity        uk    :  0.15069E-01 0.40626E+01
   Dimensionless distance   yplus :  0.92127E-01 0.39138E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2192   0.45806E-02   0.43230E+00 
c  VelocityY    0.29398E+04    2192   0.45806E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2192   0.45806E-02   0.00000E+00 
c  Pressure     0.44632E+00    6962   0.39151E-01   0.21220E+00 
c  k            0.21233E+04    1445   0.11320E-03   0.76488E+00 
c  omega        0.29411E+08     341   0.46856E-04   0.99446E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7108e+05                             1
a  Local Time Step      1.0966e-05                         44266


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8803          1.3747     -9.6324e-05     -3.4589e-06
v  Velocity[Y]                 -21.888          30.653          6.6525          20.056
v  Velocity[Z]                 -28.321          28.574        0.067811      -0.0025828
v  ǁVelocityǁ                0.0046564          33.529          10.555          20.217
v  Pressure                    -410.59          344.29         -53.476          31.718
v  k                        3.3215e-08          53.229          4.1487           1.639
v  omega                         1e-24      2.9789e+07          8831.6          11.933
v  turbulent_viscosity      3.3349e-15          1.2755        0.015749         0.10845
v  CourantNb                  0.019666          3019.1          44.769          1.3765
v  FourierNb                  0.010858           15801          93.709         0.68587
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14817        0.010819        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15873          138.48          2.0623


 TIME FOR THE TIME STEP              504:        0.48352E+02

===============================================================


 INSTANT    0.505000000E+02   TIME STEP NUMBER             505
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.134066463E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           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+02 0.13383E+02
   Friction velocity        uet   :  0.31133E-02 0.26020E+01
   Friction velocity        uk    :  0.17069E-01 0.32221E+01
   Dimensionless distance   yplus :  0.14892E+00 0.27232E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2178   0.45721E-02   0.44077E+00 
c  VelocityY    0.29397E+04    2178   0.45721E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2178   0.45721E-02   0.00000E+00 
c  Pressure     0.44867E+00    7124   0.36158E-01   0.21266E+00 
c  k            0.21181E+04    1309   0.73330E-04   0.61986E+00 
c  omega        0.13226E+08     327   0.88726E-04   0.60612E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3639e+05                             2
a  Local Time Step      1.1477e-05                         44221


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0746          1.2105     -0.00058826     -2.2722e-06
v  Velocity[Y]                 -17.685          31.515          6.6837          20.057
v  Velocity[Z]                 -28.759          28.567        0.044005      -0.0018824
v  ǁVelocityǁ                  0.00582           33.77          10.543          20.218
v  Pressure                    -411.45          343.55         -54.943          31.631
v  k                        1.2711e-07          51.622           4.195          1.6403
v  omega                         1e-24      4.0647e+07          8555.2          11.891
v  turbulent_viscosity      1.8227e-14          1.2701        0.015755         0.10845
v  CourantNb                  0.016568            2641          44.609          1.3763
v  FourierNb                   0.01086           15720          94.288         0.68619
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14811        0.010819        0.045748


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15777           138.9          2.0625


 TIME FOR THE TIME STEP              505:        0.48491E+02

===============================================================


 INSTANT    0.506000000E+02   TIME STEP NUMBER             506
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.259313082E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31043E+02 0.13862E+02
   Friction velocity        uet   :  0.20879E-02 0.29100E+01
   Friction velocity        uk    :  0.90614E-02 0.31160E+01
   Dimensionless distance   yplus :  0.79513E-01 0.27188E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        539
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2138   0.45521E-02   0.45027E+00 
c  VelocityY    0.29397E+04    2138   0.45521E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2138   0.45521E-02   0.00000E+00 
c  Pressure     0.44174E+00    7012   0.31844E-01   0.20962E+00 
c  k            0.21143E+04    1141   0.79426E-04   0.66330E+00 
c  omega        0.12871E+08     456   0.63873E-04   0.33589E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6643e+05                             1
a  Local Time Step      1.1024e-05                         44201


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1846         0.93673     -0.00066028     -1.1663e-06
v  Velocity[Y]                 -16.325          33.267          6.7175          20.056
v  Velocity[Z]                 -28.534          28.975        0.016909        -0.00138
v  ǁVelocityǁ                0.0020023          33.714          10.515          20.217
v  Pressure                    -409.46          343.26         -55.777          31.486
v  k                        7.5098e-09           52.23          4.2107          1.6415
v  omega                         1e-24      3.3584e+07          8347.7          11.866
v  turbulent_viscosity      2.1314e-14          1.2664        0.015787         0.10846
v  CourantNb                  0.055613          2060.5          44.298          1.3763
v  FourierNb                  0.010863           15705          96.654         0.68719
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14753        0.010819        0.045767


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15756          140.95          2.0635


 TIME FOR THE TIME STEP              506:        0.47797E+02

===============================================================


 INSTANT    0.507000000E+02   TIME STEP NUMBER             507
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.300426870E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31139E+02 0.16350E+02
   Friction velocity        uet   :  0.69303E-03 0.29282E+01
   Friction velocity        uk    :  0.12680E-01 0.31800E+01
   Dimensionless distance   yplus :  0.10822E+00 0.30511E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        463
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2145   0.46158E-02   0.46655E+00 
c  VelocityY    0.29396E+04    2145   0.46158E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2145   0.46158E-02   0.00000E+00 
c  Pressure     0.45256E+00    6970   0.30434E-01   0.21356E+00 
c  k            0.21089E+04    1118   0.66992E-04   0.68134E+00 
c  omega        0.11732E+08     400   0.45118E-04   0.14596E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -28972                             1
a  Local Time Step      1.1957e-05                         44288


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2761          0.8021     -0.00018146      1.1621e-06
v  Velocity[Y]                 -15.091          33.169          6.7191          20.057
v  Velocity[Z]                 -28.265          29.005      -0.0025374     -0.00078004
v  ǁVelocityǁ                 0.015673          33.978          10.502          20.217
v  Pressure                    -396.81          343.68          -56.72          31.046
v  k                        5.0295e-07          45.809          4.1865          1.6427
v  omega                         1e-24      1.8304e+07          8249.5           11.85
v  turbulent_viscosity      1.2714e-14          1.2622        0.015811         0.10849
v  CourantNb                  0.042089          2037.7          44.033          1.3763
v  FourierNb                  0.010865           15645          98.136         0.68808
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14862        0.010819        0.045788


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15696          142.17          2.0644


 TIME FOR THE TIME STEP              507:        0.48313E+02

===============================================================


 INSTANT    0.508000000E+02   TIME STEP NUMBER             508
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.340120323E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31017E+02 0.20526E+02
   Friction velocity        uet   :  0.11956E-02 0.28123E+01
   Friction velocity        uk    :  0.12241E-01 0.31677E+01
   Dimensionless distance   yplus :  0.62280E-01 0.39814E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        471
   Nb of faces within the viscous sub-layer     :        937
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2169   0.45279E-02   0.47084E+00 
c  VelocityY    0.29397E+04    2169   0.45279E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2169   0.45279E-02   0.00000E+00 
c  Pressure     0.42980E+00    6970   0.29983E-01   0.20421E+00 
c  k            0.21042E+04    1194   0.57116E-04   0.61432E+00 
c  omega        0.10596E+08     287   0.31355E-04   0.10724E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6703e+05                             1
a  Local Time Step      1.1455e-05                         44304


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3062         0.97472      0.00068138      4.1668e-06
v  Velocity[Y]                 -15.127          33.627          6.6971          20.057
v  Velocity[Z]                 -28.495          29.032       -0.012185     -0.00014667
v  ǁVelocityǁ                 0.007426          33.866          10.502          20.216
v  Pressure                    -382.36          344.05         -57.519          30.662
v  k                        4.6643e-08          39.019          4.1552           1.644
v  omega                         1e-24      1.2093e+07          8180.2           11.84
v  turbulent_viscosity      1.0966e-13          1.2569        0.015819         0.10852
v  CourantNb                  0.030291          2016.2            43.8          1.3765
v  FourierNb                  0.010868           15581          98.266         0.68834
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010818        0.045749


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15637          142.07          2.0648


 TIME FOR THE TIME STEP              508:        0.48769E+02

===============================================================


 INSTANT    0.509000000E+02   TIME STEP NUMBER             509
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.818684061E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29750E+02 0.21255E+02
   Friction velocity        uet   :  0.11685E-02 0.27064E+01
   Friction velocity        uk    :  0.23753E-01 0.33386E+01
   Dimensionless distance   yplus :  0.83564E-01 0.32325E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        493
   Nb of faces within the viscous sub-layer     :        931
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2171   0.45588E-02   0.46823E+00 
c  VelocityY    0.29396E+04    2171   0.45588E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2171   0.45588E-02   0.00000E+00 
c  Pressure     0.42943E+00    6959   0.27752E-01   0.20419E+00 
c  k            0.21011E+04    1302   0.62280E-04   0.66606E+00 
c  omega        0.10490E+08     239   0.28761E-04   0.97896E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2408e+05                             1
a  Local Time Step      1.2044e-05                         44332


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4624          1.1413       0.0011333      5.1606e-06
v  Velocity[Y]                 -15.082          30.404          6.6967          20.056
v  Velocity[Z]                 -29.519          28.942       -0.007179      0.00010996
v  ǁVelocityǁ                 0.018727          35.156          10.516          20.215
v  Pressure                    -364.44          345.58         -56.969          30.588
v  k                        1.4276e-08          39.925          4.1005          1.6452
v  omega                         1e-24      1.1782e+07          8066.9          11.825
v  turbulent_viscosity      3.2769e-14          1.2529        0.015813         0.10857
v  CourantNb                  0.032322          2033.5          43.745          1.3767
v  FourierNb                  0.010871           15531          98.135         0.68828
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14852        0.010817        0.045747


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15595          141.88           2.065


 TIME FOR THE TIME STEP              509:        0.48431E+02

===============================================================


 INSTANT    0.510000000E+02   TIME STEP NUMBER             510
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.437961826E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30702E+02 0.20035E+02
   Friction velocity        uet   :  0.14859E-02 0.28285E+01
   Friction velocity        uk    :  0.26088E-01 0.28944E+01
   Dimensionless distance   yplus :  0.12803E+00 0.27749E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        953
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    2164   0.45590E-02   0.45160E+00 
c  VelocityY    0.29395E+04    2164   0.45590E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    2164   0.45590E-02   0.00000E+00 
c  Pressure     0.42581E+00    6982   0.27959E-01   0.20258E+00 
c  k            0.21003E+04    1358   0.63103E-04   0.79047E+00 
c  omega        0.10500E+08     258   0.32302E-04   0.64983E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8106e+05                             1
a  Local Time Step      1.1899e-05                         44318


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3785          1.2907      0.00082547      5.1465e-06
v  Velocity[Y]                 -15.186          30.359          6.7218          20.056
v  Velocity[Z]                 -31.639          29.076      2.4286e-05       0.0005967
v  ǁVelocityǁ                  0.02019          36.529          10.546          20.215
v  Pressure                    -358.53          347.22         -55.501          31.011
v  k                        5.4705e-08          51.153          4.0525          1.6464
v  omega                         1e-24      1.1782e+07          7968.4          11.807
v  turbulent_viscosity      4.1502e-15          1.2498        0.015783         0.10862
v  CourantNb                  0.041019          2047.4          43.962          1.3768
v  FourierNb                  0.010875           15487          96.765         0.68762
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14829        0.010817        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99736           15560          140.73          2.0644


 TIME FOR THE TIME STEP              510:        0.47862E+02

===============================================================


 INSTANT    0.511000000E+02   TIME STEP NUMBER             511
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.461150081E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30838E+02 0.16092E+02
   Friction velocity        uet   :  0.15679E-02 0.30647E+01
   Friction velocity        uk    :  0.18528E-01 0.30076E+01
   Dimensionless distance   yplus :  0.84653E-01 0.27094E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        414
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2085   0.43849E-02   0.43114E+00 
c  VelocityY    0.29396E+04    2085   0.43849E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2085   0.43849E-02   0.00000E+00 
c  Pressure     0.43171E+00    7082   0.32123E-01   0.20415E+00 
c  k            0.21042E+04    1388   0.67249E-04   0.92738E+00 
c  omega        0.10460E+08     236   0.78408E-04   0.28924E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -20375                             1
a  Local Time Step      1.1733e-05                         44293


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4737           1.371      0.00022105      4.6229e-06
v  Velocity[Y]                 -15.102          30.312          6.7747          20.056
v  Velocity[Z]                 -32.885           28.93        0.025166      0.00071287
v  ǁVelocityǁ                 0.013145          36.229          10.606          20.214
v  Pressure                    -414.87          348.28         -53.646          31.408
v  k                        3.5823e-10          63.654          4.0149          1.6476
v  omega                         1e-24      3.5701e+07          8105.3           11.83
v  turbulent_viscosity      1.1958e-13          1.2464        0.015745         0.10868
v  CourantNb                  0.030762          2053.1          44.113          1.3767
v  FourierNb                  0.010878           15563          95.896         0.68684
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14921        0.010817        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15622          140.01          2.0635


 TIME FOR THE TIME STEP              511:        0.47583E+02

===============================================================


 INSTANT    0.512000000E+02   TIME STEP NUMBER             512
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.302673526E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30332E+02 0.13930E+02
   Friction velocity        uet   :  0.14365E-02 0.30236E+01
   Friction velocity        uk    :  0.23859E-01 0.31575E+01
   Dimensionless distance   yplus :  0.73234E-01 0.27450E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2025   0.45815E-02   0.42381E+00 
c  VelocityY    0.29398E+04    2025   0.45815E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2025   0.45815E-02   0.00000E+00 
c  Pressure     0.44561E+00    7103   0.36813E-01   0.21012E+00 
c  k            0.21146E+04    1481   0.66827E-04   0.98794E+00 
c  omega        0.12146E+08     244   0.16402E-03   0.11610E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3299e+05                             2
a  Local Time Step      1.1857e-05                         44290


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4713          1.3626     -0.00045218      3.5195e-06
v  Velocity[Y]                 -15.884          30.161          6.8423          20.057
v  Velocity[Z]                 -32.589          28.875        0.072156       0.0012268
v  ǁVelocityǁ                 0.013618          34.565          10.663          20.215
v  Pressure                       -439          349.06         -51.933          31.932
v  k                        1.5443e-08          67.653          3.9746          1.6487
v  omega                         1e-24      6.5909e+07          8468.2          11.846
v  turbulent_viscosity      1.1773e-15          1.2445        0.015689         0.10873
v  CourantNb                  0.023004          2641.8          44.495          1.3767
v  FourierNb                  0.010881           15597          94.927         0.68589
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14919        0.010817        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15656          139.42          2.0626


 TIME FOR THE TIME STEP              512:        0.46900E+02

===============================================================


 INSTANT    0.513000000E+02   TIME STEP NUMBER             513
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.352517444E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30250E+02 0.13642E+02
   Friction velocity        uet   :  0.98994E-03 0.29863E+01
   Friction velocity        uk    :  0.20620E-01 0.27908E+01
   Dimensionless distance   yplus :  0.18417E+00 0.27302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        341
   Nb of faces within the viscous sub-layer     :       1043
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1979   0.46328E-02   0.40392E+00 
c  VelocityY    0.29399E+04    1979   0.46328E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1979   0.46328E-02   0.00000E+00 
c  Pressure     0.43552E+00    7090   0.38273E-01   0.20441E+00 
c  k            0.21289E+04    1504   0.68079E-04   0.10232E+01 
c  omega        0.25707E+08     152   0.14891E-03   0.94927E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -33217                             1
a  Local Time Step       1.165e-05                         44273


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4443          1.3623      -0.0013919       2.359e-06
v  Velocity[Y]                 -22.709          29.956          6.8794          20.057
v  Velocity[Z]                 -32.063          28.748         0.13392       0.0014578
v  ǁVelocityǁ                 0.011629          33.292          10.664          20.215
v  Pressure                    -439.28          349.43         -50.955          32.068
v  k                        1.0488e-08           60.21          3.9218          1.6495
v  omega                         1e-24      2.1243e+08            8858          11.907
v  turbulent_viscosity      7.2164e-14          1.2452        0.015639         0.10879
v  CourantNb                  0.011306          2659.7          44.874          1.3768
v  FourierNb                  0.010885           15459          93.688         0.68515
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010818        0.045696


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78337           15521          138.56          2.0619


 TIME FOR THE TIME STEP              513:        0.45695E+02

===============================================================


 INSTANT    0.514000000E+02   TIME STEP NUMBER             514
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.224195923E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30716E+02 0.13723E+02
   Friction velocity        uet   :  0.30936E-03 0.28175E+01
   Friction velocity        uk    :  0.16104E-01 0.30416E+01
   Dimensionless distance   yplus :  0.14610E+00 0.27247E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        332
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1943   0.46526E-02   0.35857E+00 
c  VelocityY    0.29401E+04    1943   0.46526E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1943   0.46526E-02   0.00000E+00 
c  Pressure     0.45135E+00    7078   0.35403E-01   0.21362E+00 
c  k            0.21422E+04    1490   0.71200E-04   0.10465E+01 
c  omega        0.27040E+09     105   0.81542E-05   0.27054E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -97694                             1
a  Local Time Step      1.1468e-05                         44264


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4657          1.3196      -0.0018863      2.2669e-06
v  Velocity[Y]                 -27.688          29.767          6.8317          20.056
v  Velocity[Z]                 -29.231          28.719         0.18745        0.001322
v  ǁVelocityǁ                0.0087331          32.615          10.614          20.213
v  Pressure                    -422.03          349.47         -50.274          32.204
v  k                        7.8176e-09          54.154          3.8961          1.6501
v  omega                         1e-24      1.0624e+08          8680.6          11.882
v  turbulent_viscosity      6.9787e-14          1.2474        0.015594         0.10886
v  CourantNb                  0.013232          2059.1          45.071          1.3768
v  FourierNb                  0.010889           15186          92.793         0.68463
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947         0.01082        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94751           15251          137.86          2.0615


 TIME FOR THE TIME STEP              514:        0.46937E+02

===============================================================


 INSTANT    0.515000000E+02   TIME STEP NUMBER             515
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.902472279E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30962E+02 0.19761E+02
   Friction velocity        uet   :  0.11099E-02 0.26264E+01
   Friction velocity        uk    :  0.14093E-01 0.31944E+01
   Dimensionless distance   yplus :  0.10672E+00 0.27148E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        343
   Nb of faces within the viscous sub-layer     :       1032
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1827   0.45333E-02   0.31774E+00 
c  VelocityY    0.29402E+04    1827   0.45333E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1827   0.45333E-02   0.00000E+00 
c  Pressure     0.45068E+00    7094   0.30658E-01   0.21388E+00 
c  k            0.21491E+04    1391   0.89214E-04   0.97442E+00 
c  omega        0.68596E+08     129   0.44078E-04   0.61642E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9526e+05                             1
a  Local Time Step      1.1219e-05                         44252


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4895          1.2912      -0.0016018     -4.7651e-08
v  Velocity[Y]                 -22.474          29.581          6.7352          20.056
v  Velocity[Z]                 -29.352          28.832         0.20536       0.0012921
v  ǁVelocityǁ                 0.021372          32.951          10.595          20.213
v  Pressure                    -395.69          348.48         -50.228          32.195
v  k                        6.5293e-09          83.047           3.948          1.6506
v  omega                         1e-24      3.9194e+08          9587.9          12.063
v  turbulent_viscosity       8.789e-14          1.2501        0.015569         0.10892
v  CourantNb                   0.01554          2030.6           44.96          1.3766
v  FourierNb                  0.010893           14828          91.913         0.68448
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14904         0.01082        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14897          136.87          2.0611


 TIME FOR THE TIME STEP              515:        0.44495E+02

===============================================================


 INSTANT    0.516000000E+02   TIME STEP NUMBER             516
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.202275405E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31104E+02 0.17329E+02
   Friction velocity        uet   :  0.23888E-02 0.25298E+01
   Friction velocity        uk    :  0.12667E-01 0.31754E+01
   Dimensionless distance   yplus :  0.98240E-01 0.30315E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1757   0.46360E-02   0.29730E+00 
c  VelocityY    0.29403E+04    1757   0.46360E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1757   0.46360E-02   0.00000E+00 
c  Pressure     0.43705E+00    7064   0.32109E-01   0.20698E+00 
c  k            0.21479E+04    1278   0.10262E-03   0.83405E+00 
c  omega        0.18164E+10      58   0.76893E-06   0.15649E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74514                             1
a  Local Time Step      1.1399e-05                         44255


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4156          1.2825      -0.0010919      -3.669e-07
v  Velocity[Y]                 -40.088          29.941          6.6803          20.056
v  Velocity[Z]                 -28.517          28.811         0.21673       0.0012739
v  ǁVelocityǁ                  0.01537          40.129          10.577          20.213
v  Pressure                    -399.26          347.06         -50.893          32.203
v  k                        3.6434e-08          88.726          4.0224          1.6509
v  omega                         1e-24      1.9596e+08          9019.3          11.988
v  turbulent_viscosity      2.9408e-14          1.2532        0.015562         0.10898
v  CourantNb                   0.02536          2022.8          44.908          1.3765
v  FourierNb                  0.010895           14547          91.331         0.68497
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14831         0.01082        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14620          136.24          2.0615


 TIME FOR THE TIME STEP              516:        0.43410E+02

===============================================================


 INSTANT    0.517000000E+02   TIME STEP NUMBER             517
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.139517642E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49196E+02 0.13869E+02
   Friction velocity        uet   :  0.12802E-02 0.36852E+01
   Friction velocity        uk    :  0.16999E-01 0.38476E+01
   Dimensionless distance   yplus :  0.13969E+00 0.37891E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1784   0.46189E-02   0.28735E+00 
c  VelocityY    0.29406E+04    1784   0.46189E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1784   0.46189E-02   0.00000E+00 
c  Pressure     0.45990E+00    7114   0.36892E-01   0.21824E+00 
c  k            0.21434E+04    1321   0.10560E-03   0.72637E+00 
c  omega        0.45413E+09      89   0.38729E-05   0.47608E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8903e+05                             1
a  Local Time Step      1.1142e-05                         44244


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.238          1.4081     -0.00085211      -1.326e-06
v  Velocity[Y]                 -28.288          30.394          6.6578          20.056
v  Velocity[Z]                 -28.486           28.59         0.20827      0.00084384
v  ǁVelocityǁ                 0.010273          33.389          10.557          20.213
v  Pressure                    -400.58           346.2         -52.002          32.413
v  k                        3.5726e-10          40.597          4.0604          1.6513
v  omega                         1e-24      9.7955e+07          8982.5           11.94
v  turbulent_viscosity      2.5622e-14          1.2603         0.01559         0.10904
v  CourantNb                  0.013944            2982          45.127          1.3765
v  FourierNb                  0.010897           14554          91.461         0.68582
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14769         0.01082         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14607          136.59          2.0624


 TIME FOR THE TIME STEP              517:        0.44058E+02

===============================================================


 INSTANT    0.518000000E+02   TIME STEP NUMBER             518
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.400256155E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31054E+02 0.13447E+02
   Friction velocity        uet   :  0.17571E-02 0.30149E+01
   Friction velocity        uk    :  0.19275E-01 0.31043E+01
   Dimensionless distance   yplus :  0.17524E+00 0.27180E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        550
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1897   0.46281E-02   0.27912E+00 
c  VelocityY    0.29408E+04    1897   0.46281E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1897   0.46281E-02   0.00000E+00 
c  Pressure     0.45021E+00    7133   0.37957E-01   0.21382E+00 
c  k            0.21390E+04    1419   0.59296E-04   0.55287E+00 
c  omega        0.11458E+09     185   0.75962E-05   0.14052E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1262e-05                         44232


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9468          1.6616     -0.00093702      5.5841e-07
v  Velocity[Y]                 -17.175          31.923          6.6507          20.055
v  Velocity[Z]                 -28.425          28.646         0.17491      0.00024037
v  ǁVelocityǁ                 0.010312          33.345           10.53          20.212
v  Pressure                    -402.13          345.81         -53.132          32.339
v  k                         3.454e-08          49.396          4.1235          1.6516
v  omega                         1e-24      4.8949e+07          8582.5          11.921
v  turbulent_viscosity      6.0947e-16          1.2679         0.01563         0.10909
v  CourantNb                  0.023193          2879.9          44.943          1.3763
v  FourierNb                  0.010899           14743          91.585         0.68651
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1477         0.01082        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14790          136.53          2.0629


 TIME FOR THE TIME STEP              518:        0.46828E+02

===============================================================


 INSTANT    0.519000000E+02   TIME STEP NUMBER             519
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.383289771E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30482E+02 0.13516E+02
   Friction velocity        uet   :  0.19546E-02 0.29199E+01
   Friction velocity        uk    :  0.66404E-02 0.31341E+01
   Dimensionless distance   yplus :  0.80274E-01 0.27975E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        605
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1875   0.46133E-02   0.29166E+00 
c  VelocityY    0.29410E+04    1875   0.46133E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1875   0.46133E-02   0.00000E+00 
c  Pressure     0.43785E+00    7088   0.35555E-01   0.20772E+00 
c  k            0.21358E+04    1478   0.58043E-04   0.49505E+00 
c  omega        0.30502E+08     195   0.15938E-04   0.74293E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0782e+05                             1
a  Local Time Step      1.0832e-05                         44238


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5802          1.7857     -0.00088287     -8.7714e-07
v  Velocity[Y]                 -16.864          33.043          6.6634          20.055
v  Velocity[Z]                 -28.688          28.906         0.12725     -0.00057767
v  ǁVelocityǁ                 0.012464          33.752          10.516          20.212
v  Pressure                    -401.35          345.66          -53.65          32.226
v  k                        2.5569e-08          52.705          4.1964           1.652
v  omega                         1e-24      2.4452e+07          8410.7          11.922
v  turbulent_viscosity      2.9477e-14          1.2749        0.015694         0.10915
v  CourantNb                  0.030347          2030.1          44.401          1.3761
v  FourierNb                  0.010899           14872          92.859         0.68744
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14736        0.010819        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14920          137.26          2.0635


 TIME FOR THE TIME STEP              519:        0.44874E+02

===============================================================


 INSTANT    0.520000000E+02   TIME STEP NUMBER             520
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.523443399E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31497E+02 0.14232E+02
   Friction velocity        uet   :  0.10211E-02 0.29143E+01
   Friction velocity        uk    :  0.10849E-01 0.28965E+01
   Dimensionless distance   yplus :  0.13201E+00 0.31751E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        509
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1870   0.45298E-02   0.31711E+00 
c  VelocityY    0.29413E+04    1870   0.45298E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1870   0.45298E-02   0.00000E+00 
c  Pressure     0.43188E+00    7031   0.33793E-01   0.20583E+00 
c  k            0.21341E+04    1510   0.63220E-04   0.59362E+00 
c  omega        0.14202E+08     325   0.28131E-04   0.38894E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -79394                             1
a  Local Time Step      1.0949e-05                         44286


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1717            1.81     -0.00017747     -1.1399e-06
v  Velocity[Y]                 -15.508          32.895          6.6884          20.057
v  Velocity[Z]                 -28.393          29.129        0.073077      -0.0012212
v  ǁVelocityǁ                0.0078614          33.816          10.511          20.213
v  Pressure                    -392.54          344.77         -54.491          31.874
v  k                        2.1928e-08          50.944          4.2134          1.6523
v  omega                         1e-24      1.6924e+07            8373          11.907
v  turbulent_viscosity      7.7535e-15           1.282        0.015772          0.1092
v  CourantNb                  0.034993          2032.6          43.822          1.3759
v  FourierNb                  0.010899           15018          95.723         0.68893
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14725        0.010819        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15072          139.54          2.0648


 TIME FOR THE TIME STEP              520:        0.45891E+02

===============================================================


 INSTANT    0.521000000E+02   TIME STEP NUMBER             521
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.140360440E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30439E+02 0.13994E+02
   Friction velocity        uet   :  0.23337E-02 0.28018E+01
   Friction velocity        uk    :  0.13785E-01 0.31516E+01
   Dimensionless distance   yplus :  0.18989E+00 0.35077E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1923   0.43461E-02   0.34382E+00 
c  VelocityY    0.29415E+04    1923   0.43461E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1923   0.43461E-02   0.00000E+00 
c  Pressure     0.43483E+00    6952   0.31635E-01   0.20703E+00 
c  k            0.21331E+04    1486   0.63578E-04   0.57269E+00 
c  omega        0.11230E+08     397   0.33264E-04   0.32205E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3703e+05                             1
a  Local Time Step       1.168e-05                         44276


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0211          1.6489      0.00064691     -1.1542e-06
v  Velocity[Y]                 -15.743           32.99          6.6875          20.057
v  Velocity[Z]                 -28.434          28.886         0.02113       -0.001918
v  ǁVelocityǁ                 0.004087          33.473          10.518          20.213
v  Pressure                     -374.4          343.64         -55.399          31.187
v  k                        2.3992e-10          40.629          4.1783          1.6526
v  omega                         1e-24      1.1671e+07          8553.3          11.924
v  turbulent_viscosity      1.5792e-14          1.2883        0.015816         0.10925
v  CourantNb                  0.027768          2027.9          43.626           1.376
v  FourierNb                  0.010899           15133          97.183         0.68982
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14832        0.010819        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15194          140.81          2.0658


 TIME FOR THE TIME STEP              521:        0.45269E+02

===============================================================


 INSTANT    0.522000000E+02   TIME STEP NUMBER             522
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.579989432E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30113E+02 0.19816E+02
   Friction velocity        uet   :  0.11894E-02 0.27129E+01
   Friction velocity        uk    :  0.12313E-01 0.29090E+01
   Dimensionless distance   yplus :  0.12984E+00 0.34439E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        506
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1977   0.43420E-02   0.36006E+00 
c  VelocityY    0.29415E+04    1977   0.43420E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1977   0.43420E-02   0.00000E+00 
c  Pressure     0.42266E+00    6960   0.29692E-01   0.20195E+00 
c  k            0.21326E+04    1425   0.61948E-04   0.59651E+00 
c  omega        0.10485E+08     256   0.30775E-04   0.14031E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -42198                             1
a  Local Time Step      1.1656e-05                         44211


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0277          1.4865       0.0014489     -1.0294e-06
v  Velocity[Y]                 -15.878          30.866          6.6792          20.056
v  Velocity[Z]                 -28.666          28.851      -0.0089059      -0.0024606
v  ǁVelocityǁ                0.0036848          33.312          10.516          20.212
v  Pressure                       -360           342.9         -55.601          30.872
v  k                        2.5497e-10           40.46          4.1341          1.6532
v  omega                         1e-24      1.1798e+07          8285.1          11.883
v  turbulent_viscosity      3.3883e-16          1.2947        0.015824          0.1093
v  CourantNb                  0.019109          2016.6          43.628          1.3763
v  FourierNb                  0.010898           15287          96.713         0.68962
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1491        0.010819        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15358          140.34          2.0659


 TIME FOR THE TIME STEP              522:        0.44849E+02

===============================================================


 INSTANT    0.523000000E+02   TIME STEP NUMBER             523
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.469950721E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30586E+02 0.19661E+02
   Friction velocity        uet   :  0.10060E-02 0.27160E+01
   Friction velocity        uk    :  0.10731E-01 0.29400E+01
   Dimensionless distance   yplus :  0.12731E+00 0.27432E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        448
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    2061   0.45820E-02   0.39081E+00 
c  VelocityY    0.29416E+04    2061   0.45820E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    2061   0.45820E-02   0.00000E+00 
c  Pressure     0.42772E+00    6993   0.28743E-01   0.20383E+00 
c  k            0.21338E+04    1390   0.65230E-04   0.70410E+00 
c  omega        0.35676E+11       7   0.11229E-07   0.99003E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3019e+05                             1
a  Local Time Step      1.1691e-05                         44232


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1192          1.4682        0.001974     -1.0618e-06
v  Velocity[Y]                 -15.411          31.257          6.6941          20.055
v  Velocity[Z]                 -30.947          29.051       -0.031839      -0.0030262
v  ǁVelocityǁ                 0.010594          36.135          10.519          20.211
v  Pressure                    -348.63           343.2         -54.413          30.832
v  k                        2.5756e-09          50.791          4.1147          1.6539
v  omega                         1e-24      1.1787e+07          8051.8          11.852
v  turbulent_viscosity      1.5642e-16          1.3018        0.015817         0.10935
v  CourantNb                  0.052776          2003.1          43.787          1.3764
v  FourierNb                  0.010896           15447          96.085         0.68912
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010819        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15524          139.87          2.0655


 TIME FOR THE TIME STEP              523:        0.44810E+02

===============================================================


 INSTANT    0.524000000E+02   TIME STEP NUMBER             524
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.654922682E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30677E+02 0.19829E+02
   Friction velocity        uet   :  0.57648E-03 0.30649E+01
   Friction velocity        uk    :  0.15890E-01 0.31388E+01
   Dimensionless distance   yplus :  0.19669E+00 0.27654E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        461
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    2225   0.44573E-02   0.40958E+00 
c  VelocityY    0.29418E+04    2225   0.44573E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    2225   0.44573E-02   0.00000E+00 
c  Pressure     0.43072E+00    7040   0.32030E-01   0.20469E+00 
c  k            0.21376E+04    1192   0.72932E-04   0.87671E+00 
c  omega        0.74588E+27       2   0.27197E-23   0.92845E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -18682                             1
a  Local Time Step      1.1917e-05                         44293


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.483          1.4101       0.0024193      2.0044e-07
v  Velocity[Y]                 -15.804          33.457          6.7326          20.056
v  Velocity[Z]                 -32.457          29.039       -0.054161      -0.0038689
v  ǁVelocityǁ                 0.011465           36.55           10.54          20.212
v  Pressure                    -395.65          344.82         -52.899            31.1
v  k                         6.506e-09          60.721          4.0964          1.6548
v  omega                         1e-24      1.1756e+07          7888.4          11.823
v  turbulent_viscosity      3.1144e-15          1.3064        0.015829         0.10939
v  CourantNb                  0.061307          2035.9          43.927          1.3764
v  FourierNb                  0.010894           15813          95.571         0.68895
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14906         0.01082        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15872           139.5          2.0654


 TIME FOR THE TIME STEP              524:        0.47802E+02

===============================================================


 INSTANT    0.525000000E+02   TIME STEP NUMBER             525
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.292626528E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30217E+02 0.14931E+02
   Friction velocity        uet   :  0.10120E-02 0.32139E+01
   Friction velocity        uk    :  0.21219E-01 0.29117E+01
   Dimensionless distance   yplus :  0.13260E+00 0.27908E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    2289   0.44488E-02   0.43269E+00 
c  VelocityY    0.29419E+04    2289   0.44488E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    2289   0.44488E-02   0.00000E+00 
c  Pressure     0.42884E+00    7118   0.36897E-01   0.20269E+00 
c  k            0.21467E+04    1246   0.75803E-04   0.98984E+00 
c  omega        0.10158E+08     291   0.50797E-04   0.99506E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1743e-05                         44322


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5957          1.3096       0.0029012      1.3233e-06
v  Velocity[Y]                 -15.024          32.777          6.7853          20.056
v  Velocity[Z]                 -33.698          28.911       -0.041786      -0.0043844
v  ǁVelocityǁ                0.0085071          35.982          10.574          20.212
v  Pressure                    -429.11          345.98         -51.551          31.366
v  k                        2.6164e-08          63.819          4.0609          1.6559
v  omega                         1e-24      1.4609e+07          7772.5          11.829
v  turbulent_viscosity      3.2381e-14          1.3073        0.015825         0.10941
v  CourantNb                  0.030132          2490.3          44.016          1.3762
v  FourierNb                  0.010892           16041          95.001         0.68844
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14849         0.01082        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0013           16105          139.02          2.0647


 TIME FOR THE TIME STEP              525:        0.49162E+02

===============================================================


 INSTANT    0.526000000E+02   TIME STEP NUMBER             526
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.159873647E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30656E+02 0.13980E+02
   Friction velocity        uet   :  0.19573E-02 0.32095E+01
   Friction velocity        uk    :  0.27301E-01 0.32117E+01
   Dimensionless distance   yplus :  0.13181E+00 0.28179E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        385
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2272   0.46128E-02   0.44190E+00 
c  VelocityY    0.29422E+04    2272   0.46128E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2272   0.46128E-02   0.00000E+00 
c  Pressure     0.43770E+00    7107   0.38033E-01   0.20708E+00 
c  k            0.21635E+04    1476   0.73186E-04   0.96289E+00 
c  omega        0.10085E+08     224   0.21023E-03   0.11674E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7803e+05                             2
a  Local Time Step      1.1752e-05                         44352


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6291          1.4552       0.0033146      3.0595e-06
v  Velocity[Y]                 -20.179          29.947          6.8263          20.056
v  Velocity[Z]                 -33.334          28.879        -0.00381      -0.0051265
v  ǁVelocityǁ                0.0087293          34.717           10.58          20.212
v  Pressure                    -439.82          346.39         -50.723           31.49
v  k                        3.6259e-08          60.537          3.9941          1.6569
v  omega                         1e-24      8.0077e+07          8088.6          11.861
v  turbulent_viscosity        1.01e-13          1.3119         0.01578         0.10948
v  CourantNb                   0.02917          2718.4           44.16           1.376
v  FourierNb                  0.010889           15997          93.901         0.68752
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877         0.01082        0.045674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97065           16067          138.06          2.0636


 TIME FOR THE TIME STEP              526:        0.48886E+02

===============================================================


 INSTANT    0.527000000E+02   TIME STEP NUMBER             527
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.414665443E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30375E+02 0.13881E+02
   Friction velocity        uet   :  0.11005E-02 0.29471E+01
   Friction velocity        uk    :  0.25380E-01 0.32044E+01
   Dimensionless distance   yplus :  0.94737E-01 0.27864E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        388
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2212   0.46214E-02   0.42253E+00 
c  VelocityY    0.29423E+04    2212   0.46214E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2212   0.46214E-02   0.00000E+00 
c  Pressure     0.43241E+00    7086   0.34822E-01   0.20361E+00 
c  k            0.21772E+04    1523   0.73242E-04   0.95884E+00 
c  omega        0.32008E+08     157   0.83210E-04   0.23794E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1366e-05                         44369


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0074          1.4711       0.0026551      2.6387e-06
v  Velocity[Y]                 -24.375          29.812          6.8114          20.057
v  Velocity[Z]                 -31.601          28.912        0.032217      -0.0058544
v  ǁVelocityǁ                 0.020519          32.337          10.559          20.213
v  Pressure                       -431          346.63         -50.105          31.538
v  k                        2.1521e-07          49.055          3.9591          1.6581
v  omega                         1e-24      1.0917e+08            8597          11.896
v  turbulent_viscosity      1.8985e-14          1.3173        0.015747         0.10955
v  CourantNb                  0.017701          2419.5          44.323          1.3759
v  FourierNb                  0.010887           15839          93.148         0.68715
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14758         0.01082        0.045662


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87799           15913          137.47          2.0631


 TIME FOR THE TIME STEP              527:        0.48660E+02

===============================================================


 INSTANT    0.528000000E+02   TIME STEP NUMBER             528
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.688699990E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31563E+02 0.15527E+02
   Friction velocity        uet   :  0.58829E-03 0.27299E+01
   Friction velocity        uk    :  0.16117E-01 0.28449E+01
   Dimensionless distance   yplus :  0.73558E-01 0.27418E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1004
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2164   0.45477E-02   0.39393E+00 
c  VelocityY    0.29424E+04    2164   0.45477E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2164   0.45477E-02   0.00000E+00 
c  Pressure     0.44395E+00    7099   0.31709E-01   0.20899E+00 
c  k            0.21853E+04    1432   0.76951E-04   0.93541E+00 
c  omega        0.49516E+08     150   0.39500E-04   0.13358E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -86569                             1
a  Local Time Step      1.1556e-05                         44381


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1339          1.3032       0.0014126      2.4363e-06
v  Velocity[Y]                 -36.414          29.667           6.735          20.056
v  Velocity[Z]                 -30.674          28.786         0.04777      -0.0061428
v  ǁVelocityǁ                0.0085333          36.555          10.553          20.212
v  Pressure                    -406.43          346.23         -50.091          31.398
v  k                        7.1543e-08          75.827          4.0002          1.6593
v  omega                         1e-24      5.9527e+07          8452.1          11.877
v  turbulent_viscosity      7.6058e-14          1.3213        0.015736         0.10964
v  CourantNb                  0.042834          2094.2          44.474          1.3757
v  FourierNb                  0.010884           15705          92.842          0.6874
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14757         0.01082        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15765          137.32          2.0631


 TIME FOR THE TIME STEP              528:        0.47175E+02

===============================================================


 INSTANT    0.529000000E+02   TIME STEP NUMBER             529
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.111665942E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31508E+02 0.24864E+02
   Friction velocity        uet   :  0.98190E-03 0.31346E+01
   Friction velocity        uk    :  0.28593E-01 0.29888E+01
   Dimensionless distance   yplus :  0.12947E+00 0.28827E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        416
   Nb of faces within the viscous sub-layer     :       1057
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2109   0.44652E-02   0.38205E+00 
c  VelocityY    0.29424E+04    2109   0.44652E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2109   0.44652E-02   0.00000E+00 
c  Pressure     0.43908E+00    7042   0.33033E-01   0.20763E+00 
c  k            0.21866E+04    1236   0.11338E-03   0.83823E+00 
c  omega        0.21975E+08     346   0.25749E-03   0.82292E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9191e+05                             1
a  Local Time Step      1.1262e-05                         44370


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2115           1.074      0.00063779      3.1343e-06
v  Velocity[Y]                 -34.936          29.942           6.671          20.056
v  Velocity[Z]                 -28.424          28.565        0.052464      -0.0063935
v  ǁVelocityǁ                 0.007081          40.861          10.577          20.213
v  Pressure                    -407.53          345.16         -51.214           31.41
v  k                        3.7961e-08          111.96          4.0918          1.6608
v  omega                         1e-24      2.1089e+08          9288.8          11.947
v  turbulent_viscosity      1.1809e-13          1.3256        0.015748         0.10973
v  CourantNb                  0.041095          2076.2          44.495          1.3755
v  FourierNb                  0.010882           15600          93.264         0.68831
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010821        0.045674


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15655          137.76          2.0638


 TIME FOR THE TIME STEP              529:        0.47247E+02

===============================================================


 INSTANT    0.530000000E+02   TIME STEP NUMBER             530
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.182516079E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.61443E+02 0.15405E+02
   Friction velocity        uet   :  0.88457E-03 0.34992E+01
   Friction velocity        uk    :  0.20423E-01 0.45356E+01
   Dimensionless distance   yplus :  0.56537E-01 0.38581E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        479
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29425E+04    2115   0.44412E-02   0.38271E+00 
c  VelocityY    0.29425E+04    2115   0.44412E-02   0.00000E+00 
c  VelocityZ    0.29425E+04    2115   0.44412E-02   0.00000E+00 
c  Pressure     0.42607E+00    7104   0.37247E-01   0.20230E+00 
c  k            0.21834E+04    1274   0.14400E-03   0.71303E+00 
c  omega        0.18495E+09     218   0.22930E-04   0.47946E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6595e+05                             2
a  Local Time Step      1.1164e-05                         44348


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2398         0.87932      0.00095418     -4.1022e-07
v  Velocity[Y]                 -30.644          30.339          6.6707          20.056
v  Velocity[Z]                 -28.547          28.708        0.052474      -0.0065764
v  ǁVelocityǁ                0.0090317          33.457          10.592          20.213
v  Pressure                     -409.5          345.35         -53.409          31.481
v  k                        7.6401e-08          75.022          4.1487          1.6626
v  omega                         1e-24      1.0566e+08          9728.6          11.981
v  turbulent_viscosity      3.4258e-14          1.3273        0.015762         0.10985
v  CourantNb                  0.062256          2049.1          44.581          1.3755
v  FourierNb                   0.01088           15548          93.881         0.68951
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14724        0.010821        0.045681


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15599          138.46           2.065


 TIME FOR THE TIME STEP              530:        0.47750E+02

===============================================================


 INSTANT    0.531000000E+02   TIME STEP NUMBER             531
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.202204764E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30723E+02 0.13819E+02
   Friction velocity        uet   :  0.11229E-02 0.29601E+01
   Friction velocity        uk    :  0.89839E-02 0.34145E+01
   Dimensionless distance   yplus :  0.11378E+00 0.29648E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29425E+04    2160   0.45071E-02   0.38949E+00 
c  VelocityY    0.29425E+04    2160   0.45071E-02   0.00000E+00 
c  VelocityZ    0.29425E+04    2160   0.45071E-02   0.00000E+00 
c  Pressure     0.42837E+00    7123   0.37879E-01   0.20235E+00 
c  k            0.21801E+04    1246   0.84492E-04   0.60950E+00 
c  omega        0.59419E+08     226   0.42368E-04   0.61490E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1565e+05                             1
a  Local Time Step      1.0558e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2164         0.95209       0.0016037     -2.3092e-06
v  Velocity[Y]                 -17.695          30.701          6.6967          20.056
v  Velocity[Z]                  -28.38          28.596        0.045201      -0.0068351
v  ǁVelocityǁ                 0.011567          33.301          10.594          20.213
v  Pressure                    -411.76          345.56         -55.633          31.438
v  k                        7.2755e-08          56.825           4.198          1.6646
v  omega                         1e-24      1.1074e+08          9278.7          11.986
v  turbulent_viscosity      1.9047e-14          1.3292        0.015787         0.10997
v  CourantNb                  0.066312          2904.8          44.658          1.3755
v  FourierNb                  0.010879           15525            94.4         0.69073
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14773        0.010821        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15578          139.06          2.0662


 TIME FOR THE TIME STEP              531:        0.47047E+02

===============================================================


 INSTANT    0.532000000E+02   TIME STEP NUMBER             532
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.405678837E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30934E+02 0.13795E+02
   Friction velocity        uet   :  0.11240E-02 0.27465E+01
   Friction velocity        uk    :  0.88339E-02 0.31027E+01
   Dimensionless distance   yplus :  0.11245E+00 0.28114E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2204   0.43814E-02   0.40242E+00 
c  VelocityY    0.29424E+04    2204   0.43814E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2204   0.43814E-02   0.00000E+00 
c  Pressure     0.44978E+00    7124   0.33783E-01   0.21351E+00 
c  k            0.21789E+04    1354   0.73390E-04   0.53674E+00 
c  omega        0.10202E+09     229   0.25450E-04   0.34287E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -48127                             1
a  Local Time Step      1.1581e-05                         44317


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2076          1.1777       0.0014303     -3.8236e-06
v  Velocity[Y]                 -17.333          32.261          6.7305          20.056
v  Velocity[Z]                 -28.652          28.957        0.030573      -0.0070395
v  ǁVelocityǁ                 0.010219          33.854          10.578          20.214
v  Pressure                    -412.66          345.83         -56.948          31.393
v  k                        6.3307e-09          48.632          4.2579          1.6667
v  omega                         1e-24      5.5434e+07          9419.8          11.987
v  turbulent_viscosity      1.6092e-15          1.3306        0.015826         0.11012
v  CourantNb                  0.030343          2228.3          44.381          1.3755
v  FourierNb                  0.010878           15497          96.339         0.69226
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1475         0.01082        0.045691


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15554          140.72          2.0678


 TIME FOR THE TIME STEP              532:        0.47441E+02

===============================================================


 INSTANT    0.533000000E+02   TIME STEP NUMBER             533
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.197491551E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30367E+02 0.13572E+02
   Friction velocity        uet   :  0.10463E-02 0.29120E+01
   Friction velocity        uk    :  0.20016E-01 0.28902E+01
   Dimensionless distance   yplus :  0.14543E+00 0.28820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2194   0.43994E-02   0.41923E+00 
c  VelocityY    0.29424E+04    2194   0.43994E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2194   0.43994E-02   0.00000E+00 
c  Pressure     0.42356E+00    6993   0.30062E-01   0.20094E+00 
c  k            0.21783E+04    1383   0.68140E-04   0.61453E+00 
c  omega        0.34629E+08     375   0.35469E-04   0.88708E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.4473e+05                             1
a  Local Time Step      1.1493e-05                         44327


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4095          1.4146      0.00034776     -3.6814e-06
v  Velocity[Y]                 -15.466          33.094          6.7554          20.055
v  Velocity[Z]                 -28.686          28.628         0.02094      -0.0072854
v  ǁVelocityǁ                 0.017067          33.748           10.55          20.213
v  Pressure                    -408.39          345.61         -57.672           31.05
v  k                        2.5189e-08          52.264          4.2504           1.669
v  omega                         1e-24       2.787e+07          8662.2          11.911
v  turbulent_viscosity      2.7059e-16          1.3312        0.015863         0.11028
v  CourantNb                 0.0067281            2062          44.136          1.3757
v  FourierNb                  0.010878           15483          99.607         0.69415
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010819        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15545          143.74          2.0699


 TIME FOR THE TIME STEP              533:        0.47600E+02

===============================================================


 INSTANT    0.534000000E+02   TIME STEP NUMBER             534
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.243550626E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29972E+02 0.14075E+02
   Friction velocity        uet   :  0.11494E-02 0.28466E+01
   Friction velocity        uk    :  0.22609E-01 0.31425E+01
   Dimensionless distance   yplus :  0.19198E+00 0.33728E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2198   0.44277E-02   0.43107E+00 
c  VelocityY    0.29423E+04    2198   0.44277E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2198   0.44277E-02   0.00000E+00 
c  Pressure     0.41920E+00    6958   0.30547E-01   0.19887E+00 
c  k            0.21763E+04    1362   0.61749E-04   0.56054E+00 
c  omega        0.13710E+08     301   0.46905E-04   0.28702E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0737e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6011           1.615      -0.0015846      -2.566e-06
v  Velocity[Y]                 -15.119          33.745          6.7391          20.055
v  Velocity[Z]                 -28.436          28.613       0.0028343      -0.0073814
v  ǁVelocityǁ                 0.013115          34.107          10.546          20.212
v  Pressure                    -391.17          343.82         -58.927          30.519
v  k                        7.2442e-10          41.198          4.2069          1.6714
v  omega                         1e-24      1.5001e+07          8407.9          11.877
v  turbulent_viscosity      1.2176e-14          1.3314        0.015873         0.11045
v  CourantNb                  0.033691          2072.2          43.862           1.376
v  FourierNb                  0.010878           15521          99.637         0.69522
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14873        0.010818        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15572           143.5          2.0712


 TIME FOR THE TIME STEP              534:        0.47068E+02

===============================================================


 INSTANT    0.535000000E+02   TIME STEP NUMBER             535
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.516956913E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30886E+02 0.22944E+02
   Friction velocity        uet   :  0.48140E-03 0.27531E+01
   Friction velocity        uk    :  0.16583E-01 0.31338E+01
   Dimensionless distance   yplus :  0.11685E+00 0.36008E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        524
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2186   0.44833E-02   0.43649E+00 
c  VelocityY    0.29422E+04    2186   0.44833E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2186   0.44833E-02   0.00000E+00 
c  Pressure     0.41412E+00    6982   0.29877E-01   0.19591E+00 
c  k            0.21756E+04    1330   0.59699E-04   0.52471E+00 
c  omega        0.10803E+08     275   0.36959E-04   0.19028E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -24008                             1
a  Local Time Step      1.1066e-05                         44367


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6668          1.7621       -0.003626      4.3806e-07
v  Velocity[Y]                 -15.072          31.526           6.726          20.056
v  Velocity[Z]                 -28.776          28.933      -0.0043846      -0.0071241
v  ǁVelocityǁ                 0.011457          33.131          10.545          20.213
v  Pressure                    -378.51          343.53         -59.267          30.277
v  k                        7.5357e-10          37.768          4.1428          1.6739
v  omega                         1e-24      1.1861e+07          8290.1          11.866
v  turbulent_viscosity      4.3088e-16          1.3308        0.015851         0.11064
v  CourantNb                  0.035113          2072.7          43.748          1.3765
v  FourierNb                  0.010879           15603          98.642         0.69562
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14946        0.010817        0.045658


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15655          142.39          2.0721


 TIME FOR THE TIME STEP              535:        0.46976E+02

===============================================================


 INSTANT    0.536000000E+02   TIME STEP NUMBER             536
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.552726056E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30747E+02 0.21158E+02
   Friction velocity        uet   :  0.33034E-02 0.25736E+01
   Friction velocity        uk    :  0.14364E-01 0.32021E+01
   Dimensionless distance   yplus :  0.15392E+00 0.28269E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :        943
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2260   0.45046E-02   0.43389E+00 
c  VelocityY    0.29422E+04    2260   0.45046E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2260   0.45046E-02   0.00000E+00 
c  Pressure     0.41958E+00    7038   0.27138E-01   0.19792E+00 
c  k            0.21762E+04    1299   0.59073E-04   0.61911E+00 
c  omega        0.10602E+08     246   0.20629E-04   0.75848E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1105e+05                             2
a  Local Time Step      1.1635e-05                         44400


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6483          1.7965      -0.0049838      1.0531e-06
v  Velocity[Y]                 -15.143          30.488          6.7403          20.057
v  Velocity[Z]                 -30.185          28.993       -0.008857      -0.0070641
v  ǁVelocityǁ                 0.011202          36.691          10.551          20.214
v  Pressure                    -355.42          345.52         -58.269          30.318
v  k                        4.6312e-08          44.137          4.0666          1.6766
v  omega                         1e-24      1.1844e+07          7998.1          11.826
v  turbulent_viscosity      6.0719e-16          1.3299        0.015809         0.11085
v  CourantNb                  0.039478          2068.4          44.029          1.3769
v  FourierNb                  0.010881           15669          98.332         0.69594
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14873        0.010816        0.045626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15726          142.36          2.0729


 TIME FOR THE TIME STEP              536:        0.49689E+02

===============================================================


 INSTANT    0.537000000E+02   TIME STEP NUMBER             537
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.391812361E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30188E+02 0.19765E+02
   Friction velocity        uet   :  0.22450E-02 0.29380E+01
   Friction velocity        uk    :  0.17076E-01 0.28401E+01
   Dimensionless distance   yplus :  0.68508E-01 0.28246E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :        973
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    2275   0.43727E-02   0.42767E+00 
c  VelocityY    0.29421E+04    2275   0.43727E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    2275   0.43727E-02   0.00000E+00 
c  Pressure     0.44334E+00    7103   0.29263E-01   0.20958E+00 
c  k            0.21798E+04    1396   0.60912E-04   0.76029E+00 
c  omega        0.10475E+08     278   0.39555E-04   0.71859E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -22160                             1
a  Local Time Step      1.1658e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6265          1.7888      -0.0057043      2.2219e-07
v  Velocity[Y]                 -15.022          30.434          6.7868          20.057
v  Velocity[Z]                 -30.992          28.858      -0.0041974      -0.0065655
v  ǁVelocityǁ                 0.016746          36.438          10.595          20.214
v  Pressure                    -391.03          347.91          -56.13          30.921
v  k                        2.4342e-08           56.83          4.0029          1.6795
v  omega                         1e-24      1.1778e+07          7988.9          11.826
v  turbulent_viscosity      6.2064e-14          1.3286         0.01575         0.11106
v  CourantNb                  0.056178          2062.5          44.221           1.377
v  FourierNb                  0.010883           15717          97.156         0.69594
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010815         0.04561


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15781          141.38           2.073


 TIME FOR THE TIME STEP              537:        0.49625E+02

===============================================================


 INSTANT    0.538000000E+02   TIME STEP NUMBER             538
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.415601654E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31234E+02 0.13706E+02
   Friction velocity        uet   :  0.57123E-03 0.30773E+01
   Friction velocity        uk    :  0.13446E-01 0.28956E+01
   Dimensionless distance   yplus :  0.16470E+00 0.28075E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    2227   0.44949E-02   0.42779E+00 
c  VelocityY    0.29419E+04    2227   0.44949E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    2227   0.44949E-02   0.00000E+00 
c  Pressure     0.43291E+00    7117   0.34650E-01   0.20486E+00 
c  k            0.21890E+04    1504   0.63769E-04   0.88973E+00 
c  omega        0.10455E+08     238   0.80528E-03   0.42393E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.912e+05                             1
a  Local Time Step      1.1566e-05                         44451


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6393          1.7839      -0.0058348       4.328e-06
v  Velocity[Y]                 -15.882          32.087          6.8628          20.056
v  Velocity[Z]                 -32.777          28.782         0.01701      -0.0061117
v  ǁVelocityǁ                0.0068252           35.46          10.651          20.214
v  Pressure                    -431.17          349.32          -53.94          31.281
v  k                        6.3509e-08          65.742          3.9596          1.6825
v  omega                         1e-24      4.6043e+08          9249.7          11.916
v  turbulent_viscosity      1.4939e-13          1.3267        0.015699         0.11129
v  CourantNb                  0.021013          2358.1          44.553          1.3771
v  FourierNb                  0.010885           15670          95.291           0.696
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010814         0.04563


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15740          139.84          2.0731


 TIME FOR THE TIME STEP              538:        0.48804E+02

===============================================================


 INSTANT    0.539000000E+02   TIME STEP NUMBER             539
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.259459493E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31222E+02 0.13894E+02
   Friction velocity        uet   :  0.20015E-02 0.31878E+01
   Friction velocity        uk    :  0.20592E-01 0.31467E+01
   Dimensionless distance   yplus :  0.10371E+00 0.27615E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        358
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    2132   0.43200E-02   0.42807E+00 
c  VelocityY    0.29418E+04    2132   0.43200E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    2132   0.43200E-02   0.00000E+00 
c  Pressure     0.44178E+00    7116   0.37892E-01   0.20762E+00 
c  k            0.22039E+04    1516   0.64331E-04   0.94569E+00 
c  omega        0.12681E+10      57   0.42723E-05   0.13267E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1875e+05                             1
a  Local Time Step      1.1345e-05                         44437


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5473          1.7547      -0.0052963      5.0974e-06
v  Velocity[Y]                 -20.223            30.2          6.9289          20.056
v  Velocity[Z]                 -31.106          28.971        0.058332      -0.0057548
v  ǁVelocityǁ                 0.008152           32.96          10.683          20.214
v  Pressure                    -444.68          349.49         -52.371          31.443
v  k                        6.1649e-08          65.345          3.9183          1.6853
v  omega                         1e-24      2.3019e+08          9566.2          11.947
v  turbulent_viscosity      1.1809e-13          1.3262        0.015668         0.11152
v  CourantNb                  0.035674          2793.9          44.903          1.3771
v  FourierNb                  0.010888           15476          93.903          0.6965
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010814        0.045649


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98738           15551          138.81          2.0736


 TIME FOR THE TIME STEP              539:        0.47807E+02

===============================================================


 INSTANT    0.540000000E+02   TIME STEP NUMBER             540
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.604353045E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30402E+02 0.14165E+02
   Friction velocity        uet   :  0.25830E-02 0.28683E+01
   Friction velocity        uk    :  0.22284E-01 0.31635E+01
   Dimensionless distance   yplus :  0.16015E+00 0.27054E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        365
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    2036   0.45236E-02   0.39479E+00 
c  VelocityY    0.29418E+04    2036   0.45236E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    2036   0.45236E-02   0.00000E+00 
c  Pressure     0.41262E+00    7061   0.36881E-01   0.19496E+00 
c  k            0.22198E+04    1433   0.65007E-04   0.99707E+00 
c  omega        0.31901E+09      65   0.12060E-04   0.92760E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6568e+05                             2
a  Local Time Step      1.1573e-05                         44444


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3026          1.7395      -0.0043811      7.2109e-06
v  Velocity[Y]                 -23.216          30.022          6.9189          20.056
v  Velocity[Z]                 -32.209           29.21          0.1145       -0.005125
v  ǁVelocityǁ                 0.011338           33.24          10.641          20.214
v  Pressure                    -436.88          349.25         -51.109          31.614
v  k                        1.6368e-07          54.505          3.8911          1.6878
v  omega                         1e-24      1.6709e+08          9473.3          11.956
v  turbulent_viscosity      6.5258e-14          1.3251        0.015656         0.11177
v  CourantNb                  0.030714          2577.6          45.173          1.3771
v  FourierNb                  0.010891           15010          92.989         0.69733
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010813        0.045656


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97306           15087          138.16          2.0745


 TIME FOR THE TIME STEP              540:        0.46969E+02

===============================================================


 INSTANT    0.541000000E+02   TIME STEP NUMBER             541
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.196189755E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31309E+02 0.15996E+02
   Friction velocity        uet   :  0.24888E-02 0.28175E+01
   Friction velocity        uk    :  0.25674E-01 0.31665E+01
   Dimensionless distance   yplus :  0.95257E-01 0.27390E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        346
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1978   0.45855E-02   0.35342E+00 
c  VelocityY    0.29417E+04    1978   0.45855E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1978   0.45855E-02   0.00000E+00 
c  Pressure     0.43725E+00    7067   0.32233E-01   0.20681E+00 
c  k            0.22317E+04    1235   0.71271E-04   0.10021E+01 
c  omega        0.18581E+09      73   0.10468E-04   0.27278E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2233e+05                             1
a  Local Time Step      1.1549e-05                         44462


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9098          1.7795      -0.0038579      6.2457e-06
v  Velocity[Y]                 -32.225          29.838          6.8283          20.056
v  Velocity[Z]                 -30.534           28.85          0.1403      -0.0046442
v  ǁVelocityǁ                0.0028713          33.057            10.6          20.214
v  Pressure                    -415.15          349.04         -50.306          31.585
v  k                        1.4079e-07          63.167          3.9124          1.6899
v  omega                         1e-24      8.3589e+07          9046.4          11.935
v  turbulent_viscosity      3.5263e-14          1.3229        0.015642         0.11201
v  CourantNb                  0.035675          2038.7          45.017           1.377
v  FourierNb                  0.010894           14851          91.821         0.69819
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814        0.010813        0.045655


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85033           14903          136.84          2.0752


 TIME FOR THE TIME STEP              541:        0.44461E+02

===============================================================


 INSTANT    0.542000000E+02   TIME STEP NUMBER             542
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.155563519E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30437E+02 0.22180E+02
   Friction velocity        uet   :  0.17869E-02 0.29185E+01
   Friction velocity        uk    :  0.11577E-01 0.29709E+01
   Dimensionless distance   yplus :  0.61040E-01 0.27567E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        369
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1941   0.45869E-02   0.32832E+00 
c  VelocityY    0.29416E+04    1941   0.45869E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1941   0.45869E-02   0.00000E+00 
c  Pressure     0.44295E+00    7027   0.30987E-01   0.21012E+00 
c  k            0.22343E+04    1071   0.87171E-04   0.90962E+00 
c  omega        0.49434E+08     193   0.41704E-04   0.37440E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -43386                             1
a  Local Time Step      1.1295e-05                         44439


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4482          1.8345      -0.0034988       5.218e-06
v  Velocity[Y]                 -23.636          29.789          6.7323          20.056
v  Velocity[Z]                 -28.599          28.859         0.14228      -0.0040441
v  ǁVelocityǁ                0.0045818          33.156          10.589          20.215
v  Pressure                    -404.03          348.88         -50.463          31.492
v  k                        5.1951e-08           87.36               4          1.6919
v  omega                         1e-24      8.1476e+07          9402.5          11.997
v  turbulent_viscosity      1.9153e-14          1.3198        0.015636         0.11225
v  CourantNb                 0.0056298          2027.6          44.889          1.3768
v  FourierNb                  0.010897           14802          91.386         0.69963
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010813        0.045653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14855          136.28          2.0764


 TIME FOR THE TIME STEP              542:        0.43159E+02

===============================================================


 INSTANT    0.543000000E+02   TIME STEP NUMBER             543
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.262442256E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44312E+02 0.13676E+02
   Friction velocity        uet   :  0.23059E-02 0.28272E+01
   Friction velocity        uk    :  0.91551E-02 0.39554E+01
   Dimensionless distance   yplus :  0.13370E+00 0.28565E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1920   0.47136E-02   0.32150E+00 
c  VelocityY    0.29415E+04    1920   0.47136E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1920   0.47136E-02   0.00000E+00 
c  Pressure     0.45480E+00    7119   0.34665E-01   0.21557E+00 
c  k            0.22288E+04    1257   0.89625E-04   0.74113E+00 
c  omega        0.51395E+08     305   0.20741E-04   0.11509E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8929e+05                             1
a  Local Time Step      1.0545e-05                         44412


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4103          1.8966      -0.0025933      3.0988e-06
v  Velocity[Y]                 -36.473           30.09          6.6879          20.056
v  Velocity[Z]                 -29.102          28.552         0.13485      -0.0034672
v  ǁVelocityǁ                 0.006747           37.36          10.585          20.214
v  Pressure                    -407.05          348.78         -51.193          31.593
v  k                        5.2981e-09          64.738          4.0621          1.6936
v  omega                         1e-24       4.083e+07          8842.2          11.948
v  turbulent_viscosity      5.7079e-14          1.3159        0.015647         0.11248
v  CourantNb                  0.033885          2014.5          44.767          1.3768
v  FourierNb                  0.010899           14781          91.899         0.70155
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14772        0.010813        0.045669


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14836          136.67          2.0783


 TIME FOR THE TIME STEP              543:        0.44069E+02

===============================================================


 INSTANT    0.544000000E+02   TIME STEP NUMBER             544
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.301084809E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38137E+02 0.14498E+02
   Friction velocity        uet   :  0.34106E-03 0.34761E+01
   Friction velocity        uk    :  0.15358E-01 0.31854E+01
   Dimensionless distance   yplus :  0.98210E-01 0.28003E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1883   0.45391E-02   0.31030E+00 
c  VelocityY    0.29414E+04    1883   0.45391E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1883   0.45391E-02   0.00000E+00 
c  Pressure     0.41707E+00    7127   0.37811E-01   0.19813E+00 
c  k            0.22206E+04    1371   0.69203E-04   0.62976E+00 
c  omega        0.16979E+08     326   0.32449E-04   0.58858E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -58034                             1
a  Local Time Step       1.092e-05                         44373


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2384          1.9486      -0.0012129      5.0316e-06
v  Velocity[Y]                 -19.946          30.662          6.6689          20.056
v  Velocity[Z]                 -28.467          28.442         0.11038      -0.0028207
v  ǁVelocityǁ                0.0028951          33.522          10.566          20.214
v  Pressure                    -408.84          347.38         -52.709          31.618
v  k                        1.1359e-09          43.463          4.1114           1.695
v  omega                         1e-24      2.0634e+07          8594.6          11.935
v  turbulent_viscosity      2.1349e-14          1.3114        0.015672         0.11271
v  CourantNb                  0.029391          3163.3          44.974          1.3768
v  FourierNb                  0.010901           14821          91.888         0.70327
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010814        0.045676


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14880          136.86          2.0801


 TIME FOR THE TIME STEP              544:        0.44304E+02

===============================================================


 INSTANT    0.545000000E+02   TIME STEP NUMBER             545
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.167097631E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30390E+02 0.13230E+02
   Friction velocity        uet   :  0.10153E-02 0.28575E+01
   Friction velocity        uk    :  0.11800E-01 0.29437E+01
   Dimensionless distance   yplus :  0.87818E-01 0.27442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        501
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1962   0.47139E-02   0.31493E+00 
c  VelocityY    0.29413E+04    1962   0.47139E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1962   0.47139E-02   0.00000E+00 
c  Pressure     0.41330E+00    7121   0.36362E-01   0.19514E+00 
c  k            0.22131E+04    1410   0.53272E-04   0.50791E+00 
c  omega        0.11855E+08     279   0.33896E-04   0.60073E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.0876e+05                             1
a  Local Time Step      1.1103e-05                         44338


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0146          2.0085      6.3872e-05       2.342e-06
v  Velocity[Y]                 -17.361          33.197          6.6713          20.056
v  Velocity[Z]                 -28.412          28.467        0.076411      -0.0024278
v  ǁVelocityǁ                0.0039057          33.881          10.545          20.214
v  Pressure                    -408.97          345.57          -53.77          31.704
v  k                        8.3757e-09           49.79          4.1765           1.696
v  omega                         1e-24      1.7757e+07          8387.4          11.918
v  turbulent_viscosity      2.2136e-15          1.3061        0.015715         0.11292
v  CourantNb                  0.045358          2540.5          44.617          1.3767
v  FourierNb                  0.010902           14943          92.993          0.7052
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14885        0.010814        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15007          137.61          2.0819


 TIME FOR THE TIME STEP              545:        0.46178E+02

===============================================================


 INSTANT    0.546000000E+02   TIME STEP NUMBER             546
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.698245770E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29843E+02 0.13650E+02
   Friction velocity        uet   :  0.22516E-02 0.29709E+01
   Friction velocity        uk    :  0.14953E-01 0.30937E+01
   Dimensionless distance   yplus :  0.14943E+00 0.27516E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        506
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1994   0.47570E-02   0.32881E+00 
c  VelocityY    0.29413E+04    1994   0.47570E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1994   0.47570E-02   0.00000E+00 
c  Pressure     0.46887E+00    7105   0.35286E-01   0.22257E+00 
c  k            0.22063E+04    1371   0.61024E-04   0.56427E+00 
c  omega        0.13358E+08     273   0.29207E-04   0.25041E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -3829.7                             1
a  Local Time Step      1.0652e-05                         44329


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.336          2.0041      0.00062758      1.6299e-06
v  Velocity[Y]                 -16.482          34.063          6.6924          20.057
v  Velocity[Z]                 -28.753          28.718        0.035937      -0.0023565
v  ǁVelocityǁ                 0.015642          34.175           10.53          20.215
v  Pressure                    -405.23          344.37         -54.757          31.548
v  k                        5.8061e-09          53.418          4.2001          1.6968
v  omega                         1e-24      1.1683e+07          8332.4          11.898
v  turbulent_viscosity      4.8659e-15          1.3009        0.015794         0.11312
v  CourantNb                  0.051502          2001.8          44.085          1.3766
v  FourierNb                  0.010903           15082          95.443         0.70768
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14845        0.010814        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15151          139.53          2.0843


 TIME FOR THE TIME STEP              546:        0.45714E+02

===============================================================


 INSTANT    0.547000000E+02   TIME STEP NUMBER             547
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.298714573E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30636E+02 0.15016E+02
   Friction velocity        uet   :  0.42743E-03 0.29335E+01
   Friction velocity        uk    :  0.14085E-01 0.31882E+01
   Dimensionless distance   yplus :  0.13484E+00 0.31708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        493
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1961   0.43312E-02   0.35096E+00 
c  VelocityY    0.29413E+04    1961   0.43312E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1961   0.43312E-02   0.00000E+00 
c  Pressure     0.45180E+00    7034   0.32628E-01   0.21498E+00 
c  k            0.21996E+04    1295   0.62107E-04   0.60613E+00 
c  omega        0.10626E+08     391   0.33863E-04   0.25594E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1154e-05                         44360


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5955          1.9614      0.00052128      5.5987e-07
v  Velocity[Y]                  -17.74           33.57          6.7105          20.057
v  Velocity[Z]                 -28.645          28.763       -0.003328       -0.002015
v  ǁVelocityǁ                0.0089058          33.642          10.533          20.215
v  Pressure                    -390.54          343.71         -56.062          31.061
v  k                         1.252e-10          43.701          4.1526          1.6971
v  omega                         1e-24      1.1682e+07            8459           11.92
v  turbulent_viscosity      2.9491e-15          1.2948        0.015841         0.11329
v  CourantNb                  0.034149          2035.9          43.751          1.3767
v  FourierNb                  0.010902           15135          97.149         0.70969
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14832        0.010813        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15207           140.9          2.0864


 TIME FOR THE TIME STEP              547:        0.44181E+02

===============================================================


 INSTANT    0.548000000E+02   TIME STEP NUMBER             548
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.217427137E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30689E+02 0.23255E+02
   Friction velocity        uet   :  0.20446E-02 0.27917E+01
   Friction velocity        uk    :  0.16371E-01 0.31312E+01
   Dimensionless distance   yplus :  0.11192E+00 0.39355E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        503
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2010   0.44406E-02   0.35918E+00 
c  VelocityY    0.29411E+04    2010   0.44406E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2010   0.44406E-02   0.00000E+00 
c  Pressure     0.41851E+00    6967   0.29275E-01   0.19789E+00 
c  k            0.21922E+04    1081   0.59670E-04   0.58132E+00 
c  omega        0.10447E+08     331   0.28459E-04   0.13070E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step        1.09e-05                         44353


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7847          1.9728      0.00023275     -1.0173e-06
v  Velocity[Y]                 -17.474          32.477          6.6934          20.056
v  Velocity[Z]                 -29.068          29.243       -0.034882      -0.0014937
v  ǁVelocityǁ                0.0091183          32.888          10.531          20.214
v  Pressure                    -377.58          343.74         -56.608          30.546
v  k                        1.4974e-10          36.546          4.0914          1.6971
v  omega                         1e-24      1.1726e+07          8247.6          11.887
v  turbulent_viscosity      9.1198e-17          1.2885        0.015826         0.11344
v  CourantNb                  0.050201          2070.9          43.701          1.3771
v  FourierNb                  0.010901           15162          97.066         0.71053
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488        0.010814        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15216          140.77          2.0876


 TIME FOR THE TIME STEP              548:        0.44161E+02

===============================================================


 INSTANT    0.549000000E+02   TIME STEP NUMBER             549
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.209951939E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30174E+02 0.20229E+02
   Friction velocity        uet   :  0.30796E-03 0.25825E+01
   Friction velocity        uk    :  0.24343E-01 0.32490E+01
   Dimensionless distance   yplus :  0.10952E+00 0.30399E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2012   0.44635E-02   0.37039E+00 
c  VelocityY    0.29412E+04    2012   0.44635E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2012   0.44635E-02   0.00000E+00 
c  Pressure     0.40826E+00    6952   0.27683E-01   0.19313E+00 
c  k            0.21852E+04    1151   0.61434E-04   0.66936E+00 
c  omega        0.25593E+28       2   0.21481E-15   0.13940E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5083e+05                             1
a  Local Time Step      1.1534e-05                         44331


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8944          2.1381     -0.00026638     -1.3603e-06
v  Velocity[Y]                  -17.08          30.408          6.6978          20.056
v  Velocity[Z]                 -30.059          29.041       -0.052189      -0.0014249
v  ǁVelocityǁ                 0.017599          35.493          10.532          20.214
v  Pressure                    -359.77          344.75         -55.894           30.58
v  k                        1.2743e-08           46.01          4.0378          1.6969
v  omega                         1e-24      1.6849e+07          8130.5          11.859
v  turbulent_viscosity      2.8898e-16          1.2824        0.015796         0.11357
v  CourantNb                  0.020173          2092.9          43.779          1.3774
v  FourierNb                  0.010899           15304          96.168         0.71083
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1486        0.010815        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87166           15366          139.95          2.0883


 TIME FOR THE TIME STEP              549:        0.44219E+02

===============================================================


 INSTANT    0.550000000E+02   TIME STEP NUMBER             550
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.188950113E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31466E+02 0.20529E+02
   Friction velocity        uet   :  0.32760E-02 0.29040E+01
   Friction velocity        uk    :  0.24424E-01 0.29468E+01
   Dimensionless distance   yplus :  0.57331E-01 0.27594E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :        955
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1962   0.46037E-02   0.38383E+00 
c  VelocityY    0.29412E+04    1962   0.46037E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1962   0.46037E-02   0.00000E+00 
c  Pressure     0.44716E+00    7054   0.29626E-01   0.21265E+00 
c  k            0.21795E+04    1427   0.64669E-04   0.86070E+00 
c  omega        0.10353E+08     295   0.16724E-03   0.10862E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -5.7809e-05                             1
a  omega          
a  Local Time Step       1.137e-05                         44369


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2619          2.1931     -0.00072496       1.339e-06
v  Velocity[Y]                 -15.418          32.258          6.7303          20.056
v  Velocity[Z]                 -32.328           29.31       -0.074979       -0.001232
v  ǁVelocityǁ                 0.013633          37.148          10.537          20.215
v  Pressure                    -372.08          346.68         -53.821          30.971
v  k                        8.5198e-09          55.562          4.0039          1.6965
v  omega                         1e-24      8.0236e+07            8185          11.856
v  turbulent_viscosity      2.3026e-14          1.2775        0.015763         0.11366
v  CourantNb                  0.074052            2105          44.093          1.3776
v  FourierNb                  0.010896           15334          94.085         0.71086
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010815        0.045676


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15404          138.18          2.0885


 TIME FOR THE TIME STEP              550:        0.44719E+02

===============================================================


 INSTANT    0.551000000E+02   TIME STEP NUMBER             551
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.119526192E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31571E+02 0.18139E+02
   Friction velocity        uet   :  0.31827E-02 0.31645E+01
   Friction velocity        uk    :  0.22182E-01 0.32169E+01
   Dimensionless distance   yplus :  0.14898E+00 0.27429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        417
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1887   0.45257E-02   0.39974E+00 
c  VelocityY    0.29412E+04    1887   0.45257E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1887   0.45257E-02   0.00000E+00 
c  Pressure     0.43010E+00    7116   0.34528E-01   0.20272E+00 
c  k            0.21782E+04    1403   0.69688E-04   0.97845E+00 
c  omega        0.31502E+08     153   0.31783E-04   0.71730E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -3.2196e-05                             1
a  omega               -2.3565e+05                             1
a  Local Time Step      1.2078e-05                         44436


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3178          2.1116      -0.0014227     -1.4092e-07
v  Velocity[Y]                 -15.139          33.591          6.7822          20.057
v  Velocity[Z]                 -33.433          29.203       -0.075715      -0.0010682
v  ǁVelocityǁ                 0.018694          36.089          10.569          20.215
v  Pressure                    -423.93          347.75         -52.021          31.318
v  k                        7.0815e-08          66.753          3.9667          1.6959
v  omega                         1e-24      4.0468e+07          8035.9          11.852
v  turbulent_viscosity      1.0185e-14          1.2713        0.015756         0.11373
v  CourantNb                  0.026792          2382.5          44.194          1.3775
v  FourierNb                  0.010893           15376          92.521          0.7111
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14933        0.010815        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15437          136.72          2.0886


 TIME FOR THE TIME STEP              551:        0.43528E+02

===============================================================


 INSTANT    0.552000000E+02   TIME STEP NUMBER             552
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.712082070E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31778E+02 0.15562E+02
   Friction velocity        uet   :  0.59458E-03 0.32535E+01
   Friction velocity        uk    :  0.21754E-01 0.31371E+01
   Dimensionless distance   yplus :  0.15045E+00 0.27063E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1898   0.44278E-02   0.41853E+00 
c  VelocityY    0.29412E+04    1898   0.44278E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1898   0.44278E-02   0.00000E+00 
c  Pressure     0.41525E+00    7132   0.38437E-01   0.19650E+00 
c  k            0.21818E+04    1380   0.72979E-04   0.10598E+01 
c  omega        0.20340E+08     182   0.13206E-03   0.24548E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2158e+05                             1
a  Local Time Step      1.0967e-05                         44485


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4015          1.8682      -0.0023614      2.7374e-06
v  Velocity[Y]                 -18.215          31.234           6.831          20.057
v  Velocity[Z]                 -33.382          29.284       -0.039649     -0.00072677
v  ǁVelocityǁ                 0.020893          34.628          10.593          20.215
v  Pressure                    -444.98          347.92         -50.457          31.642
v  k                        1.4786e-06            68.8          3.9425           1.695
v  omega                         1e-24      6.8145e+07          8829.8          11.914
v  turbulent_viscosity      2.0165e-13          1.2664        0.015753         0.11378
v  CourantNb                   0.03701          2824.9           44.23          1.3773
v  FourierNb                  0.010889           15489          91.673         0.71134
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14933        0.010817        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15545           135.9          2.0886


 TIME FOR THE TIME STEP              552:        0.43255E+02

===============================================================


 INSTANT    0.553000000E+02   TIME STEP NUMBER             553
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.262891399E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30691E+02 0.15814E+02
   Friction velocity        uet   :  0.92238E-03 0.31210E+01
   Friction velocity        uk    :  0.96150E-02 0.31268E+01
   Dimensionless distance   yplus :  0.12178E+00 0.27092E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1923   0.46069E-02   0.41513E+00 
c  VelocityY    0.29412E+04    1923   0.46069E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1923   0.46069E-02   0.00000E+00 
c  Pressure     0.40577E+00    7119   0.36571E-01   0.19160E+00 
c  k            0.21871E+04    1328   0.74943E-04   0.11178E+01 
c  omega        0.69090E+08     129   0.62131E-04   0.56761E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -45069                             2
a  Local Time Step      1.1452e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4502          1.4758      -0.0028119      4.4466e-06
v  Velocity[Y]                  -25.22          29.994          6.8337          20.056
v  Velocity[Z]                 -32.942          29.021        0.015734     -0.00071341
v  ǁVelocityǁ                 0.026768          34.212          10.588          20.215
v  Pressure                    -443.97          349.09         -49.537          31.644
v  k                        7.7522e-07           59.68          3.9255          1.6938
v  omega                         1e-24      1.4735e+08            9562          11.976
v  turbulent_viscosity      1.6454e-13          1.2616        0.015747          0.1138
v  CourantNb                 0.0087824          2788.6          44.349           1.377
v  FourierNb                  0.010885           15443          91.203         0.71172
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947         0.01082        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9553           15498          135.55          2.0888


 TIME FOR THE TIME STEP              553:        0.43335E+02

===============================================================


 INSTANT    0.554000000E+02   TIME STEP NUMBER             554
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.729072227E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30483E+02 0.13523E+02
   Friction velocity        uet   :  0.55703E-03 0.28935E+01
   Friction velocity        uk    :  0.14892E-01 0.30837E+01
   Dimensionless distance   yplus :  0.14586E+00 0.27359E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1971   0.45466E-02   0.39299E+00 
c  VelocityY    0.29413E+04    1971   0.45466E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1971   0.45466E-02   0.00000E+00 
c  Pressure     0.45469E+00    6851   0.32603E-01   0.21550E+00 
c  k            0.21900E+04    1357   0.73632E-04   0.11652E+01 
c  omega        0.91764E+08      91   0.23209E-04   0.17996E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0616e-05                         44484


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5366          1.0518       -0.002321      4.5971e-06
v  Velocity[Y]                 -30.468          29.836          6.7692          20.056
v  Velocity[Z]                 -31.383           29.04        0.054811     -0.00055027
v  ǁVelocityǁ                 0.022816           32.95           10.57          20.215
v  Pressure                    -425.61          349.88         -48.724          31.729
v  k                         1.134e-07          59.134           3.947          1.6922
v  omega                         1e-24      7.4066e+07          8887.8          11.944
v  turbulent_viscosity      2.6588e-13          1.2569        0.015734          0.1138
v  CourantNb                  0.050507          2174.6           44.53          1.3769
v  FourierNb                  0.010883           15278          91.073         0.71212
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14862        0.010822        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15334           135.6           2.089


 TIME FOR THE TIME STEP              554:        0.45211E+02

===============================================================


 INSTANT    0.555000000E+02   TIME STEP NUMBER             555
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.364102274E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30440E+02 0.21183E+02
   Friction velocity        uet   :  0.22260E-02 0.28328E+01
   Friction velocity        uk    :  0.25667E-01 0.30712E+01
   Dimensionless distance   yplus :  0.16140E+00 0.27450E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        402
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2060   0.45400E-02   0.37294E+00 
c  VelocityY    0.29413E+04    2060   0.45400E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2060   0.45400E-02   0.00000E+00 
c  Pressure     0.42190E+00    7072   0.30974E-01   0.19971E+00 
c  k            0.21870E+04    1402   0.97701E-04   0.11064E+01 
c  omega        0.26098E+08     238   0.42223E-04   0.10845E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1069e-05                         44478


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4629          1.0958      -0.0016109      7.6631e-06
v  Velocity[Y]                 -28.201          29.712          6.6712          20.056
v  Velocity[Z]                 -29.257          28.738        0.071509        -0.00053
v  ǁVelocityǁ                0.0030242          33.105          10.594          20.215
v  Pressure                    -403.62          349.32         -49.055          31.692
v  k                        4.4157e-08          101.32          4.0345          1.6906
v  omega                         1e-24      3.7844e+07          8502.8           11.92
v  turbulent_viscosity      3.5328e-14          1.2526        0.015728         0.11377
v  CourantNb                  0.056297          2014.2          44.573          1.3766
v  FourierNb                   0.01088           15015          91.736         0.71264
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14924        0.010823        0.045726


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15077          136.31          2.0893


 TIME FOR THE TIME STEP              555:        0.46771E+02

===============================================================


 INSTANT    0.556000000E+02   TIME STEP NUMBER             556
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.226263610E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30755E+02 0.20345E+02
   Friction velocity        uet   :  0.17059E-02 0.24917E+01
   Friction velocity        uk    :  0.12323E-01 0.35424E+01
   Dimensionless distance   yplus :  0.81794E-01 0.36029E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        994
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2084   0.44288E-02   0.37306E+00 
c  VelocityY    0.29412E+04    2084   0.44288E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2084   0.44288E-02   0.00000E+00 
c  Pressure     0.45156E+00    7040   0.34501E-01   0.21243E+00 
c  k            0.21776E+04    1428   0.14527E-03   0.97866E+00 
c  omega        0.18116E+08     445   0.29347E-04   0.30537E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0592e-05                         44455


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4641          1.2972      -0.0015509      7.4327e-06
v  Velocity[Y]                 -35.855          30.162          6.6349          20.056
v  Velocity[Z]                 -28.504          28.426        0.089341     -0.00058966
v  ǁVelocityǁ                 0.011508          36.205          10.618          20.215
v  Pressure                    -405.25           347.6         -50.742          31.645
v  k                        2.2663e-09          105.76          4.1333          1.6889
v  omega                         1e-24      2.0542e+07          8086.8          11.875
v  turbulent_viscosity      6.2848e-15          1.2484        0.015733         0.11373
v  CourantNb                  0.070548          2029.6          44.631          1.3766
v  FourierNb                  0.010876           14845          92.521         0.71326
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010822        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14912          137.15          2.0898


 TIME FOR THE TIME STEP              556:        0.49490E+02

===============================================================


 INSTANT    0.557000000E+02   TIME STEP NUMBER             557
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.145712034E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41204E+02 0.14062E+02
   Friction velocity        uet   :  0.16037E-02 0.33422E+01
   Friction velocity        uk    :  0.25993E-01 0.46661E+01
   Dimensionless distance   yplus :  0.15693E+00 0.42708E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :        990
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2063   0.46571E-02   0.37917E+00 
c  VelocityY    0.29412E+04    2063   0.46571E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2063   0.46571E-02   0.00000E+00 
c  Pressure     0.44042E+00    7101   0.37593E-01   0.20691E+00 
c  k            0.21663E+04    1377   0.12795E-03   0.89655E+00 
c  omega        0.11052E+08     441   0.32768E-03   0.37903E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2391e+05                             1
a  Local Time Step      1.0935e-05                         44417


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5568          1.4152       -0.002509      4.2146e-06
v  Velocity[Y]                 -24.364          30.618          6.6452          20.055
v  Velocity[Z]                 -28.542          28.522         0.10318     -0.00084915
v  ǁVelocityǁ                0.0035774          33.525           10.63          20.215
v  Pressure                    -406.11          345.24         -53.067           31.79
v  k                         2.217e-08          49.057          4.1601          1.6872
v  omega                         1e-24       6.344e+07          9662.4          11.956
v  turbulent_viscosity      2.0161e-16          1.2446        0.015762         0.11366
v  CourantNb                   0.01218          2951.5          44.751          1.3766
v  FourierNb                  0.010873           14847          93.191         0.71377
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14894        0.010822        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14902          137.94          2.0903


 TIME FOR THE TIME STEP              557:        0.48072E+02

===============================================================


 INSTANT    0.558000000E+02   TIME STEP NUMBER             558
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.184657021E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30109E+02 0.13647E+02
   Friction velocity        uet   :  0.58204E-03 0.27019E+01
   Friction velocity        uk    :  0.13144E-01 0.31143E+01
   Dimensionless distance   yplus :  0.11591E+00 0.27014E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        488
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2032   0.45133E-02   0.39103E+00 
c  VelocityY    0.29413E+04    2032   0.45133E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2032   0.45133E-02   0.00000E+00 
c  Pressure     0.43359E+00    7133   0.36000E-01   0.20528E+00 
c  k            0.21562E+04    1308   0.65417E-04   0.74123E+00 
c  omega        0.36516E+08     214   0.46467E-04   0.13334E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0408e-05                         44375


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5469          1.4749      -0.0032699      1.2953e-06
v  Velocity[Y]                 -17.741          30.924          6.6714          20.056
v  Velocity[Z]                 -28.631          28.304         0.10892      -0.0010151
v  ǁVelocityǁ                0.0081069          33.694           10.62          20.216
v  Pressure                    -406.44          343.47         -54.651          32.008
v  k                        6.3951e-08          48.959          4.2146          1.6856
v  omega                         1e-24      3.6245e+07          8969.9          11.929
v  turbulent_viscosity      1.2062e-14          1.2414        0.015796         0.11358
v  CourantNb                  0.050862          2771.5          44.612          1.3765
v  FourierNb                   0.01087           14928          94.485          0.7141
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14906        0.010822        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14976           139.1          2.0906


 TIME FOR THE TIME STEP              558:        0.46288E+02

===============================================================


 INSTANT    0.559000000E+02   TIME STEP NUMBER             559
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.238765179E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30362E+02 0.13323E+02
   Friction velocity        uet   :  0.32708E-03 0.28409E+01
   Friction velocity        uk    :  0.24099E-01 0.32356E+01
   Dimensionless distance   yplus :  0.13046E+00 0.27500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        538
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2064   0.45408E-02   0.40886E+00 
c  VelocityY    0.29413E+04    2064   0.45408E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2064   0.45408E-02   0.00000E+00 
c  Pressure     0.40540E+00    7061   0.32164E-01   0.19017E+00 
c  k            0.21486E+04    1194   0.73364E-04   0.76709E+00 
c  omega        0.24031E+08     372   0.38060E-04   0.43137E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1516e-05                         44361


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4836           1.515      -0.0030647     -5.1429e-07
v  Velocity[Y]                 -16.658            32.5          6.6988          20.056
v  Velocity[Z]                  -28.89          28.596         0.11264      -0.0010233
v  ǁVelocityǁ                 0.018776          33.392          10.597          20.216
v  Pressure                     -405.5          344.96         -55.426          31.866
v  k                        1.2252e-07          50.204          4.2407           1.684
v  omega                         1e-24      1.8384e+07          8500.9          11.906
v  turbulent_viscosity      9.2586e-15            1.24        0.015843         0.11349
v  CourantNb                  0.071726            2046          44.299          1.3766
v  FourierNb                  0.010867           15083           97.56         0.71469
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010821        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15131          141.86          2.0913


 TIME FOR THE TIME STEP              559:        0.46807E+02

===============================================================


 INSTANT    0.560000000E+02   TIME STEP NUMBER             560
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.290724232E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31189E+02 0.14596E+02
   Friction velocity        uet   :  0.74771E-03 0.28729E+01
   Friction velocity        uk    :  0.24907E-01 0.31882E+01
   Dimensionless distance   yplus :  0.15111E+00 0.30365E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        519
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2039   0.44989E-02   0.42938E+00 
c  VelocityY    0.29412E+04    2039   0.44989E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2039   0.44989E-02   0.00000E+00 
c  Pressure     0.40832E+00    7024   0.31011E-01   0.19295E+00 
c  k            0.21407E+04    1242   0.69662E-04   0.84416E+00 
c  omega        0.41811E+12       3   0.39879E-08   0.16954E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.084e-05                         44361


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4372          1.4957      -0.0019412      1.3742e-09
v  Velocity[Y]                 -15.184          32.671          6.6972          20.056
v  Velocity[Z]                 -29.163          28.864         0.10922      -0.0013017
v  ǁVelocityǁ                 0.020416          33.463          10.573          20.216
v  Pressure                     -395.6          343.65         -56.338          31.419
v  k                          1.99e-07          47.505          4.2029          1.6824
v  omega                         1e-24      1.2627e+07          8273.1          11.894
v  turbulent_viscosity      7.9257e-15           1.239        0.015862         0.11339
v  CourantNb                  0.038285          2042.9           44.03          1.3767
v  FourierNb                  0.010864           15152          98.653         0.71459
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14815         0.01082        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15204          142.68          2.0913


 TIME FOR THE TIME STEP              560:        0.45393E+02

===============================================================


 INSTANT    0.561000000E+02   TIME STEP NUMBER             561
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.107736304E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31543E+02 0.17134E+02
   Friction velocity        uet   :  0.43200E-03 0.27670E+01
   Friction velocity        uk    :  0.83352E-02 0.30853E+01
   Dimensionless distance   yplus :  0.70649E-01 0.37890E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2008   0.46132E-02   0.43365E+00 
c  VelocityY    0.29410E+04    2008   0.46132E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2008   0.46132E-02   0.00000E+00 
c  Pressure     0.43418E+00    7055   0.31124E-01   0.20443E+00 
c  k            0.21341E+04    1409   0.64872E-04   0.82033E+00 
c  omega        0.45065E+11       9   0.10686E-07   0.25114E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1724e-05                         44373


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4433          1.4855     -0.00015495      1.7556e-06
v  Velocity[Y]                 -17.136          33.669          6.6688          20.056
v  Velocity[Z]                 -28.607          29.019         0.10286      -0.0017861
v  ǁVelocityǁ                 0.013071          33.923          10.557          20.216
v  Pressure                    -376.48          343.49         -56.774          31.093
v  k                        1.3788e-08          42.565          4.1536           1.681
v  omega                         1e-24      1.1698e+07            8248          11.877
v  turbulent_viscosity      1.0389e-13          1.2377        0.015837         0.11328
v  CourantNb                  0.024947          2033.5          43.864           1.377
v  FourierNb                  0.010862           15256          97.535         0.71332
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14797         0.01082        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90203           15316           141.4          2.0903


 TIME FOR THE TIME STEP              561:        0.46342E+02

===============================================================


 INSTANT    0.562000000E+02   TIME STEP NUMBER             562
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.481476353E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31863E+02 0.20301E+02
   Friction velocity        uet   :  0.58248E-03 0.26701E+01
   Friction velocity        uk    :  0.18322E-01 0.33515E+01
   Dimensionless distance   yplus :  0.17847E+00 0.31775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :        930
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1949   0.45367E-02   0.43570E+00 
c  VelocityY    0.29408E+04    1949   0.45367E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1949   0.45367E-02   0.00000E+00 
c  Pressure     0.45374E+00    7029   0.28896E-01   0.21614E+00 
c  k            0.21290E+04    1530   0.66000E-04   0.83909E+00 
c  omega        0.10868E+08     342   0.20446E-04   0.97058E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1466e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3541          1.4788       0.0012264      1.4642e-06
v  Velocity[Y]                 -15.221          30.494          6.6605          20.057
v  Velocity[Z]                 -29.786          29.255        0.098905      -0.0016646
v  ǁVelocityǁ                 0.013307          34.187          10.535          20.217
v  Pressure                    -359.41          344.29         -55.852          31.137
v  k                        4.8395e-10          42.849          4.0804            1.68
v  omega                         1e-24      1.1785e+07          8047.8          11.849
v  turbulent_viscosity      2.7241e-14          1.2384        0.015812         0.11317
v  CourantNb                   0.04176            2027          44.057          1.3776
v  FourierNb                  0.010859           15237          97.063         0.71211
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14816         0.01082        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15307          141.12          2.0897


 TIME FOR THE TIME STEP              562:        0.47229E+02

===============================================================


 INSTANT    0.563000000E+02   TIME STEP NUMBER             563
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.163928387E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30363E+02 0.20078E+02
   Friction velocity        uet   :  0.18689E-02 0.27530E+01
   Friction velocity        uk    :  0.15416E-01 0.29632E+01
   Dimensionless distance   yplus :  0.17146E+00 0.27498E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        399
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1757   0.44707E-02   0.43238E+00 
c  VelocityY    0.29406E+04    1757   0.44707E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1757   0.44707E-02   0.00000E+00 
c  Pressure     0.42205E+00    7096   0.28284E-01   0.19998E+00 
c  k            0.21268E+04    1476   0.60362E-04   0.92170E+00 
c  omega        0.10496E+08     260   0.21449E-04   0.65147E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1549e-05                         44412


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1345          1.5042       0.0021516      1.2188e-06
v  Velocity[Y]                 -15.922          30.345          6.6858          20.057
v  Velocity[Z]                 -31.141          29.192        0.086872      -0.0020689
v  ǁVelocityǁ                 0.008587          36.166          10.531          20.217
v  Pressure                    -348.21          345.48         -53.942          31.453
v  k                        8.4927e-08          47.318          3.9933           1.679
v  omega                         1e-24      1.1776e+07          7972.8          11.831
v  turbulent_viscosity      1.7435e-15          1.2402        0.015756         0.11305
v  CourantNb                  0.027171            2022          44.362          1.3778
v  FourierNb                  0.010858           15367          95.853         0.71047
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14743        0.010821        0.045756


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15422          140.21          2.0883


 TIME FOR THE TIME STEP              563:        0.46156E+02

===============================================================


 INSTANT    0.564000000E+02   TIME STEP NUMBER             564
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.282460077E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30278E+02 0.16079E+02
   Friction velocity        uet   :  0.14427E-02 0.30468E+01
   Friction velocity        uk    :  0.98583E-02 0.31829E+01
   Dimensionless distance   yplus :  0.12181E+00 0.27172E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        358
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1652   0.43408E-02   0.43629E+00 
c  VelocityY    0.29405E+04    1652   0.43408E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1652   0.43408E-02   0.00000E+00 
c  Pressure     0.42748E+00    7064   0.32031E-01   0.20308E+00 
c  k            0.21299E+04    1348   0.63342E-04   0.10628E+01 
c  omega        0.10439E+08     233   0.61192E-04   0.13297E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3926e+05                             1
a  Local Time Step      1.1565e-05                         44423


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7884          1.5512       0.0029196      6.5832e-07
v  Velocity[Y]                 -15.219          30.249          6.7504          20.057
v  Velocity[Z]                 -33.107          29.325        0.076981      -0.0026174
v  ǁVelocityǁ                0.0033822          36.259          10.567          20.217
v  Pressure                    -400.15          346.77         -51.836          31.731
v  k                        1.2401e-07          60.217          3.9441          1.6782
v  omega                         1e-24      1.5714e+07          8103.8          11.838
v  turbulent_viscosity      9.3946e-14          1.2422        0.015719         0.11293
v  CourantNb                  0.020961          2020.5          44.439          1.3778
v  FourierNb                  0.010857           15537          93.901         0.70866
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14886         0.01082         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15589          138.34          2.0865


 TIME FOR THE TIME STEP              564:        0.42647E+02

===============================================================


 INSTANT    0.565000000E+02   TIME STEP NUMBER             565
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.433670744E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31044E+02 0.13374E+02
   Friction velocity        uet   :  0.15477E-02 0.31591E+01
   Friction velocity        uk    :  0.14044E-01 0.30128E+01
   Dimensionless distance   yplus :  0.16057E+00 0.27655E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        401
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1729   0.43344E-02   0.43988E+00 
c  VelocityY    0.29404E+04    1729   0.43344E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1729   0.43344E-02   0.00000E+00 
c  Pressure     0.42664E+00    7103   0.36541E-01   0.20266E+00 
c  k            0.21396E+04     995   0.66755E-04   0.11573E+01 
c  omega        0.16197E+08     210   0.11516E-03   0.10625E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1028e-05                         44428


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3657          1.6105       0.0036106      2.7714e-07
v  Velocity[Y]                 -15.092          30.857          6.8276          20.056
v  Velocity[Z]                  -32.58          29.159         0.09538      -0.0027614
v  ǁVelocityǁ                 0.011472          33.736          10.612          20.217
v  Pressure                    -429.36          348.63         -50.013          31.964
v  k                        1.3234e-07          66.361          3.9221          1.6776
v  omega                         1e-24       7.872e+07          8354.5          11.863
v  turbulent_viscosity      1.0829e-13          1.2481        0.015714          0.1128
v  CourantNb                  0.017035          2613.1          44.614          1.3777
v  FourierNb                  0.010857           15670          92.794         0.70723
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14894         0.01082        0.045743


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15723          137.41          2.0849


 TIME FOR THE TIME STEP              565:        0.43844E+02

===============================================================


 INSTANT    0.566000000E+02   TIME STEP NUMBER             566
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.124283680E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30668E+02 0.14260E+02
   Friction velocity        uet   :  0.15493E-02 0.30886E+01
   Friction velocity        uk    :  0.18087E-01 0.31779E+01
   Dimensionless distance   yplus :  0.13733E+00 0.27923E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        356
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1736   0.44834E-02   0.43306E+00 
c  VelocityY    0.29404E+04    1736   0.44834E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1736   0.44834E-02   0.00000E+00 
c  Pressure     0.43820E+00    7101   0.37467E-01   0.20776E+00 
c  k            0.21537E+04    1278   0.67490E-04   0.12194E+01 
c  omega        0.28457E+08     144   0.57211E-04   0.92329E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4529e+05                             1
a  Local Time Step       1.169e-05                         44435


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.91891          1.6722       0.0035312      2.0353e-07
v  Velocity[Y]                 -23.442          29.906          6.8712          20.057
v  Velocity[Z]                 -32.617          29.135         0.13414      -0.0032154
v  ǁVelocityǁ                 0.010072          34.015          10.607          20.217
v  Pressure                    -434.11          349.11         -48.726          32.087
v  k                        8.0451e-07          61.139          3.9052          1.6769
v  omega                         1e-24      5.3534e+07          8490.6          11.906
v  turbulent_viscosity      1.4742e-14          1.2568        0.015731         0.11269
v  CourantNb                  0.020599            2772           44.76          1.3776
v  FourierNb                  0.010857           15660          92.332         0.70622
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14746        0.010819        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15718          137.09          2.0838


 TIME FOR THE TIME STEP              566:        0.44651E+02

===============================================================


 INSTANT    0.567000000E+02   TIME STEP NUMBER             567
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.488556875E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30729E+02 0.14481E+02
   Friction velocity        uet   :  0.18582E-02 0.28939E+01
   Friction velocity        uk    :  0.24067E-01 0.29155E+01
   Dimensionless distance   yplus :  0.17257E+00 0.28052E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        383
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1686   0.44266E-02   0.39178E+00 
c  VelocityY    0.29404E+04    1686   0.44266E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1686   0.44266E-02   0.00000E+00 
c  Pressure     0.44049E+00    6447   0.35456E-01   0.20892E+00 
c  k            0.21675E+04    1413   0.69510E-04   0.12824E+01 
c  omega        0.17743E+08     171   0.52724E-04   0.68851E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1434e-05                         44399


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94625          1.7219        0.003052     -4.4442e-07
v  Velocity[Y]                 -25.684          29.702          6.8304          20.057
v  Velocity[Z]                 -30.729          28.782         0.17887       -0.003302
v  ǁVelocityǁ                 0.013808          32.393          10.558          20.218
v  Pressure                    -420.53          348.98         -47.893          32.028
v  k                        1.1226e-07          48.707           3.913          1.6762
v  omega                         1e-24      2.7761e+07          8590.2          11.926
v  turbulent_viscosity      1.2659e-13          1.2648        0.015745         0.11257
v  CourantNb                  0.046433          2279.2          44.827          1.3775
v  FourierNb                  0.010857           15557          91.624         0.70563
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14897        0.010819        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15623          136.45          2.0832


 TIME FOR THE TIME STEP              567:        0.40734E+02

===============================================================


 INSTANT    0.568000000E+02   TIME STEP NUMBER             568
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.488678156E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29906E+02 0.18514E+02
   Friction velocity        uet   :  0.59213E-03 0.26687E+01
   Friction velocity        uk    :  0.16795E-01 0.31131E+01
   Dimensionless distance   yplus :  0.56579E-01 0.27620E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1544   0.44573E-02   0.35304E+00 
c  VelocityY    0.29403E+04    1544   0.44573E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1544   0.44573E-02   0.00000E+00 
c  Pressure     0.41836E+00    6977   0.31799E-01   0.19807E+00 
c  k            0.21757E+04    1419   0.87162E-04   0.12617E+01 
c  omega        0.11873E+08     223   0.79659E-04   0.98896E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1599e-05                         44381


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1747          1.7694       0.0029109     -2.9882e-07
v  Velocity[Y]                 -28.538          29.581          6.7284          20.056
v  Velocity[Z]                 -30.057          28.686         0.17782      -0.0036393
v  ǁVelocityǁ                 0.012348          32.963          10.546          20.217
v  Pressure                    -393.78          347.71         -47.519          31.892
v  k                        3.9999e-09          77.615          3.9873          1.6754
v  omega                         1e-24      3.3789e+07          8683.3          11.938
v  turbulent_viscosity      1.0546e-13          1.2728         0.01576         0.11246
v  CourantNb                  0.040699          2004.8          44.626          1.3773
v  FourierNb                  0.010857           15418          91.143         0.70533
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14927         0.01082         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15491          135.77          2.0826


 TIME FOR THE TIME STEP              568:        0.41049E+02

===============================================================


 INSTANT    0.569000000E+02   TIME STEP NUMBER             569
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.147225841E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30508E+02 0.19075E+02
   Friction velocity        uet   :  0.11993E-02 0.25870E+01
   Friction velocity        uk    :  0.22173E-01 0.31017E+01
   Dimensionless distance   yplus :  0.17854E+00 0.28317E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1579   0.44579E-02   0.33446E+00 
c  VelocityY    0.29403E+04    1579   0.44579E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1579   0.44579E-02   0.00000E+00 
c  Pressure     0.40896E+00    7103   0.32446E-01   0.19434E+00 
c  k            0.21754E+04    1390   0.10287E-03   0.11588E+01 
c  omega        0.15217E+08     391   0.11867E-03   0.17002E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0751e-05                         44347


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4997          1.7662       0.0023534     -5.2676e-08
v  Velocity[Y]                 -38.607          29.811          6.6599          20.057
v  Velocity[Z]                 -28.442          28.354           0.172      -0.0042096
v  ǁVelocityǁ                0.0039209          40.359          10.548          20.218
v  Pressure                    -397.97          345.61         -48.157          32.016
v  k                        6.0192e-09          93.533          4.0988          1.6748
v  omega                         1e-24      5.0324e+07          8984.8           11.98
v  turbulent_viscosity      2.1965e-15          1.2793        0.015779         0.11235
v  CourantNb                  0.054537          1992.7          44.537          1.3771
v  FourierNb                  0.010858           15437          91.476         0.70523
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14793         0.01082        0.045742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99722           15490          136.01          2.0823


 TIME FOR THE TIME STEP              569:        0.43767E+02

===============================================================


 INSTANT    0.570000000E+02   TIME STEP NUMBER             570
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.783044240E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53643E+02 0.13060E+02
   Friction velocity        uet   :  0.96175E-03 0.35612E+01
   Friction velocity        uk    :  0.15559E-01 0.41682E+01
   Dimensionless distance   yplus :  0.13698E+00 0.38301E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1664   0.44604E-02   0.32973E+00 
c  VelocityY    0.29402E+04    1664   0.44604E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1664   0.44604E-02   0.00000E+00 
c  Pressure     0.43001E+00    7117   0.35989E-01   0.20371E+00 
c  k            0.21708E+04    1282   0.11000E-03   0.10261E+01 
c  omega        0.22595E+08     329   0.39511E-04   0.10710E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1186e-05                         44350


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7112          1.7267       0.0010665     -2.9794e-06
v  Velocity[Y]                  -29.68          30.208          6.6325          20.056
v  Velocity[Z]                 -28.436          28.404         0.15411      -0.0043275
v  ǁVelocityǁ                0.0040809          33.299          10.546          20.218
v  Pressure                    -401.21          344.28         -49.936          31.907
v  k                        7.8992e-10          43.984          4.1512          1.6742
v  omega                         1e-24      2.5324e+07          8669.4          11.967
v  turbulent_viscosity      1.5775e-14          1.2847        0.015826         0.11225
v  CourantNb                  0.032004          2207.2          44.575          1.3771
v  FourierNb                  0.010858           15489           92.83         0.70559
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14812         0.01082        0.045754


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15538           137.4          2.0827


 TIME FOR THE TIME STEP              570:        0.44748E+02

===============================================================


 INSTANT    0.571000000E+02   TIME STEP NUMBER             571
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.165198366E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29989E+02 0.12720E+02
   Friction velocity        uet   :  0.50934E-03 0.29234E+01
   Friction velocity        uk    :  0.13762E-01 0.29665E+01
   Dimensionless distance   yplus :  0.12760E+00 0.27653E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1787   0.44855E-02   0.32389E+00 
c  VelocityY    0.29401E+04    1787   0.44855E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1787   0.44855E-02   0.00000E+00 
c  Pressure     0.43189E+00    7127   0.37045E-01   0.20517E+00 
c  k            0.21656E+04    1275   0.63857E-04   0.89668E+00 
c  omega        0.16088E+08     308   0.30250E-04   0.10068E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1139e-05                         44297


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8573          1.7176     -0.00049864     -3.5705e-06
v  Velocity[Y]                 -17.445          31.731          6.6274          20.055
v  Velocity[Z]                  -28.62          28.631         0.12995      -0.0043847
v  ǁVelocityǁ                 0.012532          33.162          10.538          20.217
v  Pressure                     -403.4          344.41         -51.617          31.891
v  k                        1.8277e-11          48.251          4.2112          1.6737
v  omega                         1e-24      2.1723e+07            8452          11.952
v  turbulent_viscosity      1.0836e-15          1.2905        0.015882         0.11215
v  CourantNb                  0.037461          3023.2          44.541          1.3771
v  FourierNb                  0.010857           15559           94.24           0.706
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823         0.01082        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15608          138.78          2.0831


 TIME FOR THE TIME STEP              571:        0.44774E+02

===============================================================


 INSTANT    0.572000000E+02   TIME STEP NUMBER             572
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.920879496E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29712E+02 0.13327E+02
   Friction velocity        uet   :  0.63322E-03 0.29293E+01
   Friction velocity        uk    :  0.14479E-01 0.32157E+01
   Dimensionless distance   yplus :  0.12226E+00 0.28394E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        556
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1861   0.44980E-02   0.33286E+00 
c  VelocityY    0.29401E+04    1861   0.44980E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1861   0.44980E-02   0.00000E+00 
c  Pressure     0.43525E+00    7087   0.35001E-01   0.20700E+00 
c  k            0.21615E+04    1348   0.63756E-04   0.85005E+00 
c  omega        0.35204E+08     156   0.19311E-04   0.12272E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.323e+05                             1
a  Local Time Step      1.1417e-05                         44305


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9151          1.8906      -0.0017256     -1.4753e-06
v  Velocity[Y]                 -17.155           33.06          6.6425          20.056
v  Velocity[Z]                 -29.121          29.164         0.10074      -0.0045594
v  ǁVelocityǁ                 0.029551           33.79          10.529          20.217
v  Pressure                    -403.48          344.54         -52.836          31.922
v  k                        1.2671e-08          49.491          4.2603          1.6733
v  omega                         1e-24      2.1461e+07          8515.3          11.968
v  turbulent_viscosity      1.7847e-17           1.295        0.015943         0.11206
v  CourantNb                  0.042175          2102.6          44.144           1.377
v  FourierNb                  0.010857           15680          95.942         0.70618
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14832        0.010819        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15732          140.09          2.0832


 TIME FOR THE TIME STEP              572:        0.45260E+02

===============================================================


 INSTANT    0.573000000E+02   TIME STEP NUMBER             573
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.467971542E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31212E+02 0.14719E+02
   Friction velocity        uet   :  0.17547E-02 0.29358E+01
   Friction velocity        uk    :  0.21881E-01 0.28782E+01
   Dimensionless distance   yplus :  0.17727E+00 0.32232E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        554
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1831   0.47082E-02   0.34789E+00 
c  VelocityY    0.29401E+04    1831   0.47082E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1831   0.47082E-02   0.00000E+00 
c  Pressure     0.46123E+00    6979   0.32633E-01   0.21758E+00 
c  k            0.21582E+04    1421   0.70035E-04   0.96564E+00 
c  omega        0.21019E+08     312   0.22387E-04   0.63697E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -60810                             2
a  Local Time Step      1.1703e-05                         44300


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3862          1.9638      -0.0020506      -2.956e-07
v  Velocity[Y]                 -17.157           33.07          6.6674          20.056
v  Velocity[Z]                 -28.343          28.747        0.072813      -0.0048658
v  ǁVelocityǁ                 0.015461           33.72          10.529          20.218
v  Pressure                    -396.87          344.15         -54.046          31.598
v  k                        1.1493e-07          51.727          4.2397          1.6729
v  omega                         1e-24      1.5961e+07          8337.5          11.937
v  turbulent_viscosity      3.8316e-15          1.2971        0.015983         0.11197
v  CourantNb                  0.030616          2126.3          43.693           1.377
v  FourierNb                  0.010857           15816          97.554          0.7062
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14776        0.010817        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15876          141.25          2.0832


 TIME FOR THE TIME STEP              573:        0.44996E+02

===============================================================


 INSTANT    0.574000000E+02   TIME STEP NUMBER             574
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.332132736E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31619E+02 0.14392E+02
   Friction velocity        uet   :  0.43065E-03 0.28717E+01
   Friction velocity        uk    :  0.18827E-01 0.30720E+01
   Dimensionless distance   yplus :  0.15706E+00 0.36618E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        499
   Nb of faces within the viscous sub-layer     :        933
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1704   0.46478E-02   0.36561E+00 
c  VelocityY    0.29401E+04    1704   0.46478E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1704   0.46478E-02   0.00000E+00 
c  Pressure     0.42670E+00    6916   0.30431E-01   0.20237E+00 
c  k            0.21552E+04    1458   0.71539E-04   0.93784E+00 
c  omega        0.13328E+08     341   0.25172E-04   0.26217E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3286e+05                             2
a  Local Time Step      1.1893e-05                         44290


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.436           1.907      -0.0017013     -8.7754e-07
v  Velocity[Y]                 -17.522            32.8          6.6637          20.056
v  Velocity[Z]                 -28.446          29.199        0.036731      -0.0052949
v  ǁVelocityǁ                0.0053998          33.329           10.53          20.218
v  Pressure                    -379.97          343.16         -55.084          31.069
v  k                        8.8091e-08          39.251          4.1808          1.6726
v  omega                         1e-24       1.169e+07          8119.5          11.893
v  turbulent_viscosity      1.0539e-13          1.2984         0.01598         0.11188
v  CourantNb                  0.023467          2132.1          43.568          1.3773
v  FourierNb                  0.010858           15904          98.578         0.70587
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010817        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15974          142.15          2.0831


 TIME FOR THE TIME STEP              574:        0.44388E+02

===============================================================


 INSTANT    0.575000000E+02   TIME STEP NUMBER             575
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.165587455E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31503E+02 0.21276E+02
   Friction velocity        uet   :  0.16488E-02 0.27321E+01
   Friction velocity        uk    :  0.21184E-01 0.31005E+01
   Dimensionless distance   yplus :  0.18065E+00 0.38882E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        471
   Nb of faces within the viscous sub-layer     :        939
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1764   0.44243E-02   0.37722E+00 
c  VelocityY    0.29399E+04    1764   0.44243E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1764   0.44243E-02   0.00000E+00 
c  Pressure     0.43213E+00    6958   0.29488E-01   0.20632E+00 
c  k            0.21528E+04    1449   0.67079E-04   0.95736E+00 
c  omega        0.10486E+08     279   0.26718E-04   0.94511E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2437e+05                             2
a  Local Time Step      1.0886e-05                         44276


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3441          1.7015     -0.00063133      1.6726e-06
v  Velocity[Y]                 -18.005          30.958          6.6537          20.056
v  Velocity[Z]                 -28.458          29.072        0.012935      -0.0051847
v  ǁVelocityǁ                0.0087823          32.958          10.518          20.218
v  Pressure                    -366.27          342.55         -55.269          30.873
v  k                        8.8567e-11          38.417          4.1089          1.6725
v  omega                         1e-24       1.173e+07            7929          11.849
v  turbulent_viscosity      1.2755e-14          1.2968        0.015936          0.1118
v  CourantNb                  0.035144          2116.8           43.55          1.3777
v  FourierNb                  0.010857           15940          97.547         0.70456
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14746        0.010817         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16019           141.1          2.0822


 TIME FOR THE TIME STEP              575:        0.45724E+02

===============================================================


 INSTANT    0.576000000E+02   TIME STEP NUMBER             576
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.237795992E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30098E+02 0.20401E+02
   Friction velocity        uet   :  0.11345E-02 0.26186E+01
   Friction velocity        uk    :  0.22847E-01 0.31988E+01
   Dimensionless distance   yplus :  0.15809E+00 0.31515E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :        946
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1893   0.43899E-02   0.40176E+00 
c  VelocityY    0.29397E+04    1893   0.43899E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1893   0.43899E-02   0.00000E+00 
c  Pressure     0.41420E+00    7056   0.28343E-01   0.19616E+00 
c  k            0.21520E+04    1345   0.67605E-04   0.10585E+01 
c  omega        0.58516E+27       2   0.34629E-23   0.93186E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3812e+05                             2
a  Local Time Step      1.1805e-05                         44317


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3974          1.3557      0.00085547      1.8656e-06
v  Velocity[Y]                 -18.926          30.456          6.6769          20.056
v  Velocity[Z]                 -31.354          29.417       -0.016098      -0.0051457
v  ǁVelocityǁ                 0.015279          36.255          10.504          20.217
v  Pressure                    -356.18          343.94         -53.812          30.829
v  k                        3.0634e-09          49.698          4.0584          1.6726
v  omega                         1e-24      1.1922e+07          7866.6          11.823
v  turbulent_viscosity      2.6127e-17          1.2959        0.015891         0.11172
v  CourantNb                  0.050789          2089.8          43.851          1.3779
v  FourierNb                  0.010857           16020           95.89         0.70298
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14795        0.010816        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16069          139.74          2.0809


 TIME FOR THE TIME STEP              576:        0.45648E+02

===============================================================


 INSTANT    0.577000000E+02   TIME STEP NUMBER             577
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.265690413E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30163E+02 0.18334E+02
   Friction velocity        uet   :  0.11762E-02 0.30430E+01
   Friction velocity        uk    :  0.29545E-01 0.27528E+01
   Dimensionless distance   yplus :  0.14971E+00 0.28462E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1901   0.42651E-02   0.41847E+00 
c  VelocityY    0.29397E+04    1901   0.42651E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1901   0.42651E-02   0.00000E+00 
c  Pressure     0.40644E+00    7114   0.31331E-01   0.19189E+00 
c  k            0.21547E+04    1265   0.72941E-04   0.12340E+01 
c  omega        0.99158E+07     242   0.42669E-04   0.92128E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5851e+05                             2
a  Local Time Step      1.1726e-05                         44328


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4781          1.2167       0.0024948      2.8232e-06
v  Velocity[Y]                 -15.109          32.852           6.725          20.056
v  Velocity[Z]                 -32.144          29.048        -0.04368      -0.0049502
v  ǁVelocityǁ                 0.012333          36.573          10.515          20.218
v  Pressure                    -392.17          347.07         -52.226           31.13
v  k                        7.0911e-10          57.809          4.0238           1.673
v  omega                         1e-24      1.1721e+07          7786.4          11.827
v  turbulent_viscosity      1.8005e-15          1.2992        0.015869         0.11166
v  CourantNb                  0.071192          2052.4          44.055          1.3778
v  FourierNb                  0.010856           16208          94.076         0.70178
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14907        0.010815        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16262          138.13          2.0796


 TIME FOR THE TIME STEP              577:        0.45631E+02

===============================================================


 INSTANT    0.578000000E+02   TIME STEP NUMBER             578
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.417824586E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30817E+02 0.15878E+02
   Friction velocity        uet   :  0.59131E-03 0.31930E+01
   Friction velocity        uk    :  0.25135E-01 0.29155E+01
   Dimensionless distance   yplus :  0.98669E-01 0.28442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        380
   Nb of faces within the viscous sub-layer     :        958
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1914   0.43789E-02   0.44174E+00 
c  VelocityY    0.29398E+04    1914   0.43789E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1914   0.43789E-02   0.00000E+00 
c  Pressure     0.41249E+00    7110   0.35672E-01   0.19446E+00 
c  k            0.21624E+04    1492   0.75444E-04   0.13007E+01 
c  omega        0.97867E+07     230   0.19456E-03   0.14262E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5245e+05                             2
a  Local Time Step      1.1499e-05                         44339


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6318          1.4026       0.0037367      4.3298e-06
v  Velocity[Y]                 -15.222          33.611          6.7835          20.057
v  Velocity[Z]                  -32.55           29.09       -0.040066      -0.0045479
v  ǁVelocityǁ                 0.020245          34.776           10.54          20.218
v  Pressure                    -427.25          349.23         -50.493          31.518
v  k                        1.1417e-08          64.997          3.9919          1.6734
v  omega                         1e-24      5.6864e+07          8326.9          11.874
v  turbulent_viscosity      2.2934e-15          1.2961        0.015853         0.11158
v  CourantNb                  0.064987          2538.8          44.118          1.3776
v  FourierNb                  0.010856           16187          93.273         0.70067
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010815        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16248          137.39          2.0782


 TIME FOR THE TIME STEP              578:        0.46092E+02

===============================================================


 INSTANT    0.579000000E+02   TIME STEP NUMBER             579
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.171815736E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30729E+02 0.14988E+02
   Friction velocity        uet   :  0.77721E-03 0.33219E+01
   Friction velocity        uk    :  0.10730E-01 0.29151E+01
   Dimensionless distance   yplus :  0.14152E+00 0.28383E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1871   0.43865E-02   0.45391E+00 
c  VelocityY    0.29398E+04    1871   0.43865E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1871   0.43865E-02   0.00000E+00 
c  Pressure     0.41300E+00    7115   0.37401E-01   0.19468E+00 
c  k            0.21738E+04    1641   0.79059E-04   0.13357E+01 
c  omega        0.23046E+08     176   0.17223E-03   0.38901E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6557e+05                             2
a  Local Time Step      1.1294e-05                         44374


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7686          1.5526       0.0041267      6.7354e-06
v  Velocity[Y]                 -20.291          30.014          6.8255          20.057
v  Velocity[Z]                  -33.07          28.821      -0.0033745      -0.0041849
v  ǁVelocityǁ                0.0067262          34.676          10.553          20.218
v  Pressure                    -438.76          349.57         -49.445          31.668
v  k                        6.4918e-07          62.799          3.9765          1.6736
v  omega                         1e-24      8.5277e+07          9417.9          11.957
v  turbulent_viscosity      5.4203e-14          1.2911        0.015847         0.11151
v  CourantNb                  0.025657          2823.6          44.255          1.3772
v  FourierNb                  0.010856           16030          92.703         0.69963
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14886        0.010816         0.04573


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0108           16100          136.96          2.0769


 TIME FOR THE TIME STEP              579:        0.45944E+02

===============================================================


 INSTANT    0.580000000E+02   TIME STEP NUMBER             580
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.519041190E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29983E+02 0.15576E+02
   Friction velocity        uet   :  0.47443E-03 0.29567E+01
   Friction velocity        uk    :  0.23745E-01 0.31875E+01
   Dimensionless distance   yplus :  0.15396E+00 0.27767E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :        975
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1861   0.45666E-02   0.43963E+00 
c  VelocityY    0.29399E+04    1861   0.45666E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1861   0.45666E-02   0.00000E+00 
c  Pressure     0.43912E+00    7066   0.34203E-01   0.20681E+00 
c  k            0.21832E+04    1632   0.76889E-04   0.13515E+01 
c  omega        0.44171E+08     115   0.39952E-04   0.13784E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0017e+05                             3
a  Local Time Step       1.154e-05                         44394


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9909          1.5955       0.0032638      6.4821e-06
v  Velocity[Y]                 -24.212          29.861          6.8098          20.056
v  Velocity[Z]                 -32.723          28.805         0.03041      -0.0037504
v  ǁVelocityǁ                 0.010487           33.77          10.539          20.217
v  Pressure                    -431.23          348.76         -48.743          31.598
v  k                        4.0685e-07          51.727          3.9706          1.6737
v  omega                         1e-24      4.3272e+07          8781.4          11.923
v  turbulent_viscosity      6.5588e-14          1.2863        0.015829         0.11145
v  CourantNb                  0.016756            2581          44.412          1.3771
v  FourierNb                  0.010857           15641          91.981         0.69876
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010817        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15719          136.39          2.0758


 TIME FOR THE TIME STEP              580:        0.47242E+02

===============================================================


 INSTANT    0.581000000E+02   TIME STEP NUMBER             581
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.902404417E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31678E+02 0.15412E+02
   Friction velocity        uet   :  0.21429E-03 0.28561E+01
   Friction velocity        uk    :  0.26648E-01 0.31374E+01
   Dimensionless distance   yplus :  0.16075E+00 0.27196E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1855   0.45318E-02   0.41564E+00 
c  VelocityY    0.29399E+04    1855   0.45318E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1855   0.45318E-02   0.00000E+00 
c  Pressure     0.42322E+00    7059   0.30596E-01   0.20011E+00 
c  k            0.21874E+04    1535   0.81363E-04   0.13228E+01 
c  omega        0.19495E+08     191   0.51469E-04   0.75862E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3843e+05                             2
a  Local Time Step      1.1611e-05                         44411


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0516          1.4618       0.0014361      4.3547e-06
v  Velocity[Y]                 -36.111          29.695          6.7278          20.056
v  Velocity[Z]                 -29.218          28.465        0.050875      -0.0030259
v  ǁVelocityǁ                0.0096392          36.209          10.542          20.217
v  Pressure                    -408.27          347.26         -48.675          31.542
v  k                        1.0467e-08          72.483          4.0269          1.6736
v  omega                         1e-24      2.3643e+07            8512          11.905
v  turbulent_viscosity      2.0608e-13          1.2805        0.015808         0.11138
v  CourantNb                  0.015008          2087.7          44.509          1.3769
v  FourierNb                  0.010857           15541          91.547         0.69847
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1492        0.010818        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15594          136.06          2.0753


 TIME FOR THE TIME STEP              581:        0.45328E+02

===============================================================


 INSTANT    0.582000000E+02   TIME STEP NUMBER             582
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.819417688E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30957E+02 0.24887E+02
   Friction velocity        uet   :  0.17109E-02 0.31411E+01
   Friction velocity        uk    :  0.28324E-01 0.29094E+01
   Dimensionless distance   yplus :  0.17979E+00 0.27616E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1963   0.44973E-02   0.40333E+00 
c  VelocityY    0.29400E+04    1963   0.44973E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1963   0.44973E-02   0.00000E+00 
c  Pressure     0.43017E+00    7033   0.31263E-01   0.20262E+00 
c  k            0.21842E+04    1363   0.11032E-03   0.11939E+01 
c  omega        0.12838E+08     364   0.15284E-03   0.12284E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3141e+05                             2
a  Local Time Step       1.156e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.0279          1.2374     -0.00071844      2.3068e-06
v  Velocity[Y]                 -27.397           29.83          6.6486          20.057
v  Velocity[Z]                 -28.432          28.581        0.057431      -0.0025433
v  ǁVelocityǁ                 0.018236          36.333          10.579          20.218
v  Pressure                    -406.73             346         -49.924          31.536
v  k                         9.491e-10          105.73          4.1273          1.6734
v  omega                         1e-24      4.4437e+07          8669.9          11.901
v  turbulent_viscosity      1.1646e-15          1.2764        0.015808         0.11132
v  CourantNb                 0.0089767          2101.6           44.43          1.3767
v  FourierNb                  0.010859           15462          92.171         0.69879
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14796        0.010818        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15510           136.6          2.0755


 TIME FOR THE TIME STEP              582:        0.48720E+02

===============================================================


 INSTANT    0.583000000E+02   TIME STEP NUMBER             583
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.286155391E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.44823E+02 0.16340E+02
   Friction velocity        uet   :  0.70910E-03 0.31384E+01
   Friction velocity        uk    :  0.15726E-01 0.45092E+01
   Dimensionless distance   yplus :  0.84554E-01 0.37941E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    2039   0.45942E-02   0.40768E+00 
c  VelocityY    0.29400E+04    2039   0.45942E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    2039   0.45942E-02   0.00000E+00 
c  Pressure     0.41492E+00    6953   0.35700E-01   0.19555E+00 
c  k            0.21752E+04    1228   0.13304E-03   0.10419E+01 
c  omega        0.18097E+08     468   0.90543E-04   0.10930E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9386e+05                             2
a  Local Time Step      1.0906e-05                         44426


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9993          1.1064      -0.0019303      2.5182e-06
v  Velocity[Y]                 -32.272          30.219          6.6401          20.056
v  Velocity[Z]                 -29.094          28.419         0.07203      -0.0015252
v  ǁVelocityǁ                 0.012529          33.357          10.616          20.217
v  Pressure                     -408.3          345.72         -52.615          31.462
v  k                        2.6472e-08          79.745          4.1885          1.6733
v  omega                         1e-24      4.5943e+07          8623.2          11.893
v  turbulent_viscosity      2.8935e-15          1.2699        0.015828         0.11126
v  CourantNb                   0.02377          2073.9          44.374          1.3767
v  FourierNb                   0.01086           15320          93.423         0.69924
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14863        0.010817         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15369           137.8          2.0759


 TIME FOR THE TIME STEP              583:        0.47441E+02

===============================================================


 INSTANT    0.584000000E+02   TIME STEP NUMBER             584
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.618574761E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31943E+02 0.14124E+02
   Friction velocity        uet   :  0.83664E-03 0.31059E+01
   Friction velocity        uk    :  0.19008E-01 0.35475E+01
   Dimensionless distance   yplus :  0.11831E+00 0.32115E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        409
   Nb of faces within the viscous sub-layer     :        945
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2087   0.45719E-02   0.41431E+00 
c  VelocityY    0.29399E+04    2087   0.45719E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2087   0.45719E-02   0.00000E+00 
c  Pressure     0.40984E+00    7124   0.37552E-01   0.19345E+00 
c  k            0.21649E+04    1171   0.91936E-04   0.94371E+00 
c  omega        0.17103E+08     335   0.16365E-03   0.20662E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7617e+05                             1
a  Local Time Step      1.1115e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1185          1.0069       -0.002218      1.0875e-06
v  Velocity[Y]                 -18.344          30.668          6.6646          20.056
v  Velocity[Z]                 -28.423          28.509        0.085804     -0.00088957
v  ǁVelocityǁ                 0.016306          33.394          10.628          20.218
v  Pressure                     -409.3          345.36         -55.396          31.605
v  k                        1.5573e-08          49.944          4.2094          1.6731
v  omega                         1e-24      9.7746e+07          8732.3          11.895
v  turbulent_viscosity      1.5805e-14          1.2645        0.015866          0.1112
v  CourantNb                  0.022086          2975.4          44.469          1.3768
v  FourierNb                  0.010861           15253          94.333         0.69972
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010817        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15307           138.8          2.0765


 TIME FOR THE TIME STEP              584:        0.48027E+02

===============================================================


 INSTANT    0.585000000E+02   TIME STEP NUMBER             585
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.325504610E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30415E+02 0.13990E+02
   Friction velocity        uet   :  0.93243E-03 0.26683E+01
   Friction velocity        uk    :  0.24446E-01 0.29568E+01
   Dimensionless distance   yplus :  0.99400E-01 0.28344E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        458
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2190   0.44440E-02   0.42171E+00 
c  VelocityY    0.29399E+04    2190   0.44440E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2190   0.44440E-02   0.00000E+00 
c  Pressure     0.42509E+00    7105   0.34451E-01   0.20219E+00 
c  k            0.21561E+04    1367   0.71678E-04   0.83250E+00 
c  omega        0.42391E+08     257   0.32098E-04   0.66671E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3318e+05                             1
a  Local Time Step        1.12e-05                         44363


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2592          0.9569      -0.0025785     -2.0928e-06
v  Velocity[Y]                 -17.561          31.748          6.7002          20.056
v  Velocity[Z]                 -28.525          28.855        0.097741      -0.0002312
v  ǁVelocityǁ                  0.01336           33.81          10.622          20.217
v  Pressure                    -409.17           345.3          -57.14          31.556
v  k                        5.2696e-09          51.313          4.2417          1.6729
v  omega                         1e-24      4.9377e+07          8438.8          11.885
v  turbulent_viscosity      2.4382e-14          1.2593        0.015914         0.11115
v  CourantNb                   0.02843          2440.8          44.219          1.3768
v  FourierNb                  0.010861           15261          96.167          0.7004
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010816        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15320          140.39          2.0772


 TIME FOR THE TIME STEP              585:        0.50788E+02

===============================================================


 INSTANT    0.586000000E+02   TIME STEP NUMBER             586
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.629221072E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30270E+02 0.13993E+02
   Friction velocity        uet   :  0.18275E-02 0.28899E+01
   Friction velocity        uk    :  0.27896E-01 0.31998E+01
   Dimensionless distance   yplus :  0.13633E+00 0.27908E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        490
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2149   0.46538E-02   0.42969E+00 
c  VelocityY    0.29399E+04    2149   0.46538E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2149   0.46538E-02   0.00000E+00 
c  Pressure     0.44146E+00    6687   0.30746E-01   0.20911E+00 
c  k            0.21488E+04    1434   0.76650E-04   0.88737E+00 
c  omega        0.14870E+08     438   0.57339E-04   0.26554E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2256e+05                             3
a  Local Time Step      1.1055e-05                         44322


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -3.312         0.94991      -0.0032318     -1.0576e-06
v  Velocity[Y]                 -15.772          32.897          6.7325          20.056
v  Velocity[Z]                 -28.775          28.921         0.10688      0.00049377
v  ǁVelocityǁ                0.0089263          33.631          10.589          20.217
v  Pressure                    -404.88          345.07             -58          31.511
v  k                        7.8907e-08          53.195          4.2062          1.6726
v  omega                         1e-24      2.5702e+07          8258.1          11.884
v  turbulent_viscosity      7.1489e-16          1.2532        0.015926          0.1111
v  CourantNb                  0.026569          2078.1          44.068           1.377
v  FourierNb                  0.010862           15316          98.642         0.70078
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010815        0.045736


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15382          142.71          2.0778


 TIME FOR THE TIME STEP              586:        0.47564E+02

===============================================================


 INSTANT    0.587000000E+02   TIME STEP NUMBER             587
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.248135556E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31533E+02 0.15109E+02
   Friction velocity        uet   :  0.33063E-03 0.28713E+01
   Friction velocity        uk    :  0.28583E-01 0.32129E+01
   Dimensionless distance   yplus :  0.96735E-01 0.31801E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :        951
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2085   0.45003E-02   0.43876E+00 
c  VelocityY    0.29399E+04    2085   0.45003E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2085   0.45003E-02   0.00000E+00 
c  Pressure     0.42867E+00    7028   0.30454E-01   0.20359E+00 
c  k            0.21402E+04    1429   0.70410E-04   0.86175E+00 
c  omega        0.10693E+08     357   0.57157E-04   0.21281E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8309e+05                             3
a  Local Time Step       1.168e-05                         44383


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.2713         0.93458      -0.0042628     -3.0436e-06
v  Velocity[Y]                 -15.235          33.155          6.7235          20.056
v  Velocity[Z]                 -28.645          29.245         0.10417      0.00086972
v  ǁVelocityǁ                0.0079378          33.312           10.57          20.216
v  Pressure                    -388.34          344.03          -58.63          31.071
v  k                        4.4827e-08          42.253          4.1218          1.6722
v  omega                         1e-24      1.4871e+07          8213.2          11.876
v  turbulent_viscosity      3.2025e-14          1.2454        0.015888         0.11106
v  CourantNb                 0.0071895          2088.2           43.98          1.3772
v  FourierNb                  0.010864           15350          98.736         0.70016
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010815         0.04573


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15423          142.72          2.0774


 TIME FOR THE TIME STEP              587:        0.47982E+02

===============================================================


 INSTANT    0.588000000E+02   TIME STEP NUMBER             588
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.503896029E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31004E+02 0.22782E+02
   Friction velocity        uet   :  0.10268E-02 0.27355E+01
   Friction velocity        uk    :  0.31165E-01 0.31514E+01
   Dimensionless distance   yplus :  0.11221E+00 0.37214E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :        923
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2057   0.45401E-02   0.44690E+00 
c  VelocityY    0.29399E+04    2057   0.45401E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2057   0.45401E-02   0.00000E+00 
c  Pressure     0.45486E+00    7021   0.29617E-01   0.21668E+00 
c  k            0.21328E+04    1374   0.62540E-04   0.81502E+00 
c  omega        0.14202E+08     269   0.13078E-03   0.88518E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1202e+05                             2
a  Local Time Step      1.1648e-05                         44417


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -3.1578         0.86988      -0.0054932     -2.8139e-06
v  Velocity[Y]                 -16.538          31.954          6.7144          20.056
v  Velocity[Z]                 -28.659          29.158          0.0922       0.0014125
v  ǁVelocityǁ                0.0055086          32.834          10.549          20.216
v  Pressure                    -371.46          344.63         -58.216          30.837
v  k                        1.3966e-07           38.94          4.0219           1.672
v  omega                         1e-24      1.7259e+08          8596.4          11.905
v  turbulent_viscosity      2.6583e-13          1.2414        0.015802         0.11101
v  CourantNb                   0.02246          2101.9          43.929          1.3775
v  FourierNb                  0.010865           15285          97.094         0.69863
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010815        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15365          141.02          2.0762


 TIME FOR THE TIME STEP              588:        0.46385E+02

===============================================================


 INSTANT    0.589000000E+02   TIME STEP NUMBER             589
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.782213222E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31136E+02 0.20752E+02
   Friction velocity        uet   :  0.15297E-02 0.25473E+01
   Friction velocity        uk    :  0.14393E-01 0.30541E+01
   Dimensionless distance   yplus :  0.20485E+00 0.29510E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2066   0.44895E-02   0.44844E+00 
c  VelocityY    0.29398E+04    2066   0.44895E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2066   0.44895E-02   0.00000E+00 
c  Pressure     0.42827E+00    7035   0.27413E-01   0.20386E+00 
c  k            0.21275E+04    1218   0.61749E-04   0.88677E+00 
c  omega        0.25994E+09      76   0.34709E-05   0.22991E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0111e+05                             2
a  Local Time Step      1.1293e-05                         44403


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.9982         0.80175       -0.006047     -3.4583e-06
v  Velocity[Y]                 -15.141          30.324          6.7385          20.056
v  Velocity[Z]                 -30.135          29.283        0.068774        0.001961
v  ǁVelocityǁ                0.0076983          35.836          10.541          20.216
v  Pressure                    -349.96          347.96         -56.199          31.084
v  k                        9.5019e-09          42.134          3.9224          1.6717
v  omega                         1e-24       8.629e+07          8265.4          11.861
v  turbulent_viscosity      5.5702e-14          1.2395        0.015716         0.11097
v  CourantNb                  0.010662          2117.1          44.288           1.378
v  FourierNb                  0.010866           15218          95.451         0.69712
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14928        0.010816        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15270          139.74          2.0751


 TIME FOR THE TIME STEP              589:        0.45229E+02

===============================================================


 INSTANT    0.590000000E+02   TIME STEP NUMBER             590
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.901214601E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30687E+02 0.19915E+02
   Friction velocity        uet   :  0.61020E-03 0.29053E+01
   Friction velocity        uk    :  0.20093E-01 0.31455E+01
   Dimensionless distance   yplus :  0.84068E-01 0.28494E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        381
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2104   0.44561E-02   0.44103E+00 
c  VelocityY    0.29398E+04    2104   0.44561E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2104   0.44561E-02   0.00000E+00 
c  Pressure     0.43010E+00    7098   0.28862E-01   0.20394E+00 
c  k            0.21258E+04    1187   0.62106E-04   0.10167E+01 
c  omega        0.65736E+08     122   0.28781E-04   0.29660E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.226e+05                             2
a  Local Time Step      1.1598e-05                         44455


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.8263         0.76465      -0.0061161      -2.498e-06
v  Velocity[Y]                 -15.196          30.307          6.7867          20.057
v  Velocity[Z]                 -30.653          29.357        0.046016       0.0027322
v  ǁVelocityǁ                 0.013168            36.4          10.561          20.216
v  Pressure                    -372.02          350.67         -53.627          31.526
v  k                        5.6805e-09          53.718           3.863          1.6715
v  omega                         1e-24      1.0677e+08          8504.8          11.882
v  turbulent_viscosity      2.1588e-14          1.2384        0.015656         0.11093
v  CourantNb                  0.017201          2128.6          44.654           1.378
v  FourierNb                  0.010868           15438          92.943         0.69546
v  total_pressure           1.0095e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14768        0.010817        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15500           137.6          2.0734


 TIME FOR THE TIME STEP              590:        0.47694E+02

===============================================================


 INSTANT    0.591000000E+02   TIME STEP NUMBER             591
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.627462817E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31232E+02 0.14209E+02
   Friction velocity        uet   :  0.16923E-02 0.30584E+01
   Friction velocity        uk    :  0.11845E-01 0.32411E+01
   Dimensionless distance   yplus :  0.15002E+00 0.28310E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        410
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2079   0.43500E-02   0.43305E+00 
c  VelocityY    0.29398E+04    2079   0.43500E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2079   0.43500E-02   0.00000E+00 
c  Pressure     0.40760E+00    7092   0.33264E-01   0.19391E+00 
c  k            0.21303E+04    1472   0.65500E-04   0.11548E+01 
c  omega        0.71276E+08     143   0.89413E-04   0.15099E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74347                             2
a  Local Time Step      1.0775e-05                         44478


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6612         0.75137       -0.006054     -8.2454e-07
v  Velocity[Y]                 -15.059          31.144          6.8528          20.057
v  Velocity[Z]                 -32.868          29.242        0.049232       0.0031123
v  ǁVelocityǁ                 0.007314          36.159          10.615          20.216
v  Pressure                    -418.06          352.01         -50.968          31.933
v  k                        1.0242e-08           63.72          3.8548          1.6714
v  omega                         1e-24      2.9258e+08          9777.4          11.984
v  turbulent_viscosity      2.3867e-14           1.238        0.015633         0.11089
v  CourantNb                  0.035157          2272.4          44.876          1.3777
v  FourierNb                   0.01087           15468          91.408         0.69418
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14754        0.010818        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15541          136.28          2.0719


 TIME FOR THE TIME STEP              591:        0.48342E+02

===============================================================


 INSTANT    0.592000000E+02   TIME STEP NUMBER             592
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.115812929E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30865E+02 0.14256E+02
   Friction velocity        uet   :  0.14292E-02 0.31252E+01
   Friction velocity        uk    :  0.18205E-01 0.31537E+01
   Dimensionless distance   yplus :  0.15650E+00 0.27615E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2050   0.44496E-02   0.42665E+00 
c  VelocityY    0.29398E+04    2050   0.44496E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2050   0.44496E-02   0.00000E+00 
c  Pressure     0.41502E+00    7104   0.37016E-01   0.19601E+00 
c  k            0.21411E+04    1523   0.67210E-04   0.12221E+01 
c  omega        0.34143E+09      69   0.97785E-05   0.50003E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9319e+05                             4
a  Local Time Step      1.1548e-05                         44470


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.5138         0.74603      -0.0060021     -3.5592e-07
v  Velocity[Y]                  -18.33           29.98          6.9149          20.056
v  Velocity[Z]                 -32.206          29.024        0.078985       0.0031893
v  ǁVelocityǁ                 0.018204          33.992           10.66          20.215
v  Pressure                    -435.11          351.67         -48.877          32.127
v  k                        7.1936e-09          65.291          3.8648          1.6712
v  omega                         1e-24       1.465e+08          9489.1          11.956
v  turbulent_viscosity      4.6129e-14          1.2382        0.015634         0.11085
v  CourantNb                  0.022486            2741          45.097          1.3773
v  FourierNb                  0.010871           15430          90.144         0.69315
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14807        0.010818        0.045763


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87834           15490          135.24          2.0705


 TIME FOR THE TIME STEP              592:        0.48393E+02

===============================================================


 INSTANT    0.593000000E+02   TIME STEP NUMBER             593
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.667992549E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30041E+02 0.14235E+02
   Friction velocity        uet   :  0.25539E-02 0.29399E+01
   Friction velocity        uk    :  0.16514E-01 0.30739E+01
   Dimensionless distance   yplus :  0.14539E+00 0.27327E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1983   0.44841E-02   0.39817E+00 
c  VelocityY    0.29399E+04    1983   0.44841E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1983   0.44841E-02   0.00000E+00 
c  Pressure     0.44079E+00    6986   0.37941E-01   0.20920E+00 
c  k            0.21542E+04    1488   0.69737E-04   0.12587E+01 
c  omega        0.89023E+08     109   0.18626E-04   0.14674E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1689e+05                             4
a  Local Time Step      1.0596e-05                         44438


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.392          0.7486      -0.0053235     -5.5119e-08
v  Velocity[Y]                 -24.393          29.795          6.9152          20.056
v  Velocity[Z]                 -31.296          28.817         0.13172       0.0035152
v  ǁVelocityǁ                0.0034978          32.698          10.648          20.215
v  Pressure                    -430.09          350.84         -47.487           32.31
v  k                         2.176e-08          55.511           3.883          1.6708
v  omega                         1e-24      7.3655e+07          8824.7          11.906
v  turbulent_viscosity      8.0845e-14          1.2397        0.015651         0.11082
v  CourantNb                  0.010116          2633.1           45.27          1.3771
v  FourierNb                  0.010872           15418          89.854         0.69266
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14851        0.010819        0.045763


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90523           15469          135.12          2.0697


 TIME FOR THE TIME STEP              593:        0.47234E+02

===============================================================


 INSTANT    0.594000000E+02   TIME STEP NUMBER             594
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.431050170E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31354E+02 0.13908E+02
   Friction velocity        uet   :  0.11951E-02 0.27699E+01
   Friction velocity        uk    :  0.13368E-01 0.31759E+01
   Dimensionless distance   yplus :  0.85935E-01 0.27664E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1957   0.45029E-02   0.35030E+00 
c  VelocityY    0.29400E+04    1957   0.45029E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1957   0.45029E-02   0.00000E+00 
c  Pressure     0.43892E+00    6946   0.33893E-01   0.20684E+00 
c  k            0.21647E+04    1362   0.74150E-04   0.12539E+01 
c  omega        0.25214E+08     175   0.47006E-04   0.75732E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0036127                             4
a  omega               -2.0355e+05                             8
a  Local Time Step      1.1351e-05                         44410


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3022         0.77535      -0.0048888      5.1232e-07
v  Velocity[Y]                 -30.884          29.619          6.8294          20.056
v  Velocity[Z]                 -30.328          28.725         0.16616        0.003495
v  ǁVelocityǁ                 0.013245          32.729          10.618          20.214
v  Pressure                    -410.16          351.62         -46.826          32.279
v  k                        3.4495e-08          61.433          3.9253          1.6702
v  omega                         1e-24        4.04e+07          8597.9          11.886
v  turbulent_viscosity       3.482e-16          1.2412        0.015651         0.11079
v  CourantNb                  0.032923          2107.7          45.121          1.3768
v  FourierNb                  0.010873           15284          89.323         0.69209
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14867        0.010821        0.045773


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15332          134.44          2.0689


 TIME FOR THE TIME STEP              594:        0.45243E+02

===============================================================


 INSTANT    0.595000000E+02   TIME STEP NUMBER             595
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.107950312E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30998E+02 0.21396E+02
   Friction velocity        uet   :  0.21074E-02 0.28133E+01
   Friction velocity        uk    :  0.39149E-02 0.28506E+01
   Dimensionless distance   yplus :  0.44849E-01 0.27887E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1936   0.44578E-02   0.31612E+00 
c  VelocityY    0.29401E+04    1936   0.44578E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1936   0.44578E-02   0.00000E+00 
c  Pressure     0.43211E+00    7105   0.30434E-01   0.20445E+00 
c  k            0.21677E+04    1115   0.92806E-04   0.11418E+01 
c  omega        0.13951E+08     285   0.48817E-04   0.37102E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                     -0.000191                             1
a  omega               -1.0275e+05                             1
a  Local Time Step      1.1328e-05                         44373


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2338         0.78609       -0.005027      2.4387e-06
v  Velocity[Y]                     -24           29.53          6.7228          20.056
v  Velocity[Z]                 -29.476          28.508         0.17859       0.0031874
v  ǁVelocityǁ                0.0086301          32.873           10.62          20.214
v  Pressure                     -392.4          351.44         -47.284          32.211
v  k                         3.952e-08          90.448          4.0312          1.6696
v  omega                         1e-24      2.1703e+07          8404.6          11.893
v  turbulent_viscosity      1.0798e-15          1.2472        0.015667         0.11075
v  CourantNb                  0.025703          2079.3          44.837          1.3765
v  FourierNb                  0.010874           15099          89.974         0.69231
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14838        0.010821        0.045765


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98653           15149          134.81          2.0688


 TIME FOR THE TIME STEP              595:        0.45028E+02

===============================================================


 INSTANT    0.596000000E+02   TIME STEP NUMBER             596
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.115569473E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29816E+02 0.14639E+02
   Friction velocity        uet   :  0.12053E-02 0.24887E+01
   Friction velocity        uk    :  0.10931E-01 0.35316E+01
   Dimensionless distance   yplus :  0.98287E-01 0.28330E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1860   0.44954E-02   0.30317E+00 
c  VelocityY    0.29403E+04    1860   0.44954E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1860   0.44954E-02   0.00000E+00 
c  Pressure     0.41830E+00    7114   0.32603E-01   0.19749E+00 
c  k            0.21640E+04    1233   0.10453E-03   0.97039E+00 
c  omega        0.10804E+08     485   0.35548E-04   0.30586E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2066e+05                             1
a  Local Time Step      1.1085e-05                         44355


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.187         0.79062      -0.0047453      1.0469e-06
v  Velocity[Y]                 -37.204          29.791          6.6711          20.056
v  Velocity[Z]                 -28.489          28.561         0.19003       0.0025545
v  ǁVelocityǁ                0.0082575          37.714          10.624          20.213
v  Pressure                    -395.19          350.75         -48.657          32.343
v  k                        3.1753e-09          80.291          4.1129          1.6689
v  omega                         1e-24      1.3741e+07          8323.2          11.889
v  turbulent_viscosity      5.4794e-15          1.2558        0.015706         0.11073
v  CourantNb                  0.018849          2049.9           44.58          1.3764
v  FourierNb                  0.010875           15002          91.675         0.69313
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14897         0.01082        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15059          136.26          2.0695


 TIME FOR THE TIME STEP              596:        0.45920E+02

===============================================================


 INSTANT    0.597000000E+02   TIME STEP NUMBER             597
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.532562982E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.40707E+02 0.14324E+02
   Friction velocity        uet   :  0.12249E-02 0.34814E+01
   Friction velocity        uk    :  0.10531E-01 0.33157E+01
   Dimensionless distance   yplus :  0.10419E+00 0.31737E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1864   0.46494E-02   0.29544E+00 
c  VelocityY    0.29406E+04    1864   0.46494E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1864   0.46494E-02   0.00000E+00 
c  Pressure     0.42042E+00    7130   0.35817E-01   0.19836E+00 
c  k            0.21590E+04    1376   0.93871E-04   0.86821E+00 
c  omega        0.10643E+08     396   0.94927E-04   0.63567E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3727e+05                             2
a  Local Time Step      1.1117e-05                         44342


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1584         0.79484      -0.0035508      2.8451e-06
v  Velocity[Y]                 -22.798          30.381          6.6532          20.056
v  Velocity[Z]                   -28.5          28.531         0.19584       0.0017611
v  ǁVelocityǁ                 0.014961          33.257          10.616          20.214
v  Pressure                    -397.33          349.15         -50.951          32.452
v  k                        7.2106e-10          43.388          4.1414          1.6683
v  omega                         1e-24       4.669e+07          8422.4          11.894
v  turbulent_viscosity      7.1711e-15          1.2681        0.015756          0.1107
v  CourantNb                  0.033988          3117.8          44.739          1.3764
v  FourierNb                  0.010875           14998          92.883         0.69374
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14804         0.01082        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15062          137.62          2.0702


 TIME FOR THE TIME STEP              597:        0.47423E+02

===============================================================


 INSTANT    0.598000000E+02   TIME STEP NUMBER             598
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.298420560E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31155E+02 0.14362E+02
   Friction velocity        uet   :  0.13414E-02 0.27417E+01
   Friction velocity        uk    :  0.20351E-01 0.32250E+01
   Dimensionless distance   yplus :  0.13406E+00 0.27495E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        463
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    1897   0.45544E-02   0.28805E+00 
c  VelocityY    0.29409E+04    1897   0.45544E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    1897   0.45544E-02   0.00000E+00 
c  Pressure     0.41246E+00    7128   0.35305E-01   0.19480E+00 
c  k            0.21554E+04    1413   0.65883E-04   0.70853E+00 
c  omega        0.16633E+08     254   0.47684E-04   0.83457E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4041e+05                             3
a  Local Time Step      1.1603e-05                         44349


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1327          0.7953      -0.0020726      1.5176e-06
v  Velocity[Y]                 -17.401          32.612          6.6586          20.056
v  Velocity[Z]                 -28.614            28.7         0.18958      0.00096928
v  ǁVelocityǁ                 0.010653           33.47          10.593          20.214
v  Pressure                    -398.02          347.12         -52.786          32.473
v  k                         3.039e-09           52.82          4.1752          1.6678
v  omega                         1e-24      2.3525e+07          8444.2          11.928
v  turbulent_viscosity      4.3205e-16          1.2789        0.015781         0.11068
v  CourantNb                  0.025451          2715.7          44.501          1.3764
v  FourierNb                  0.010875           14990          93.776         0.69388
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14812        0.010819        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15061          138.28          2.0703


 TIME FOR THE TIME STEP              598:        0.46469E+02

===============================================================


 INSTANT    0.599000000E+02   TIME STEP NUMBER             599
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.343836719E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31294E+02 0.14281E+02
   Friction velocity        uet   :  0.13224E-02 0.29595E+01
   Friction velocity        uk    :  0.21710E-01 0.31172E+01
   Dimensionless distance   yplus :  0.15149E+00 0.27198E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        548
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1979   0.45900E-02   0.29779E+00 
c  VelocityY    0.29411E+04    1979   0.45900E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1979   0.45900E-02   0.00000E+00 
c  Pressure     0.44226E+00    7092   0.33600E-01   0.20898E+00 
c  k            0.21540E+04    1387   0.71476E-04   0.72518E+00 
c  omega        0.20687E+08     255   0.23480E-04   0.11497E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1421e+05                             2
a  Local Time Step      1.1378e-05                         44331


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0999         0.80498      -0.0010418      3.3539e-06
v  Velocity[Y]                  -16.64          33.302           6.683          20.056
v  Velocity[Z]                 -28.665          28.952         0.17258      0.00023999
v  ǁVelocityǁ                0.0028176          33.572          10.578          20.214
v  Pressure                    -396.26          345.04             -54          32.323
v  k                        1.2723e-08          50.441          4.1755          1.6672
v  omega                         1e-24      2.6668e+07          8273.2          11.926
v  turbulent_viscosity      9.1485e-16          1.2895        0.015803         0.11066
v  CourantNb                  0.048757          2053.4          44.158          1.3764
v  FourierNb                  0.010874           14943          95.169          0.6942
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14875         0.01082        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15020          139.33          2.0706


 TIME FOR THE TIME STEP              599:        0.47310E+02

===============================================================


 INSTANT    0.600000000E+02   TIME STEP NUMBER             600
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.604907918E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30557E+02 0.16564E+02
   Friction velocity        uet   :  0.48371E-03 0.29087E+01
   Friction velocity        uk    :  0.13806E-01 0.29971E+01
   Dimensionless distance   yplus :  0.20266E+00 0.30494E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2043   0.47050E-02   0.32241E+00 
c  VelocityY    0.29413E+04    2043   0.47050E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2043   0.47050E-02   0.00000E+00 
c  Pressure     0.44079E+00    7006   0.31319E-01   0.20818E+00 
c  k            0.21535E+04    1300   0.73283E-04   0.79773E+00 
c  omega        0.21569E+08     357   0.20071E-04   0.57017E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0192e+05                             2
a  Local Time Step      1.1118e-05                         44346


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0567         0.79567     -0.00072112      2.7556e-06
v  Velocity[Y]                 -17.937          32.964          6.7104          20.057
v  Velocity[Z]                 -28.834           29.09         0.13725      -0.0008293
v  ǁVelocityǁ                0.0075484          33.739          10.565          20.214
v  Pressure                    -384.82          344.17         -55.051           31.87
v  k                        1.7398e-07          45.787          4.1027          1.6668
v  omega                         1e-24      1.3334e+07          8255.9          11.922
v  turbulent_viscosity      1.0781e-14          1.2997        0.015785         0.11064
v  CourantNb                  0.023171          2064.5          43.906          1.3765
v  FourierNb                  0.010873           14900          95.773         0.69407
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1481         0.01082        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14980          139.68          2.0706


 TIME FOR THE TIME STEP              600:        0.47663E+02

===============================================================


 INSTANT    0.601000000E+02   TIME STEP NUMBER             601
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.736496603E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29828E+02 0.20423E+02
   Friction velocity        uet   :  0.14891E-02 0.27304E+01
   Friction velocity        uk    :  0.22580E-01 0.31806E+01
   Dimensionless distance   yplus :  0.99871E-01 0.38035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    2044   0.44437E-02   0.33882E+00 
c  VelocityY    0.29415E+04    2044   0.44437E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    2044   0.44437E-02   0.00000E+00 
c  Pressure     0.45588E+00    7042   0.29673E-01   0.21617E+00 
c  k            0.21534E+04    1006   0.64309E-04   0.73252E+00 
c  omega        0.11865E+08     352   0.28162E-04   0.25890E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3003e+05                             2
a  Local Time Step      1.0972e-05                         44352


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9854         0.78214     -0.00019667      4.8377e-06
v  Velocity[Y]                 -16.941          32.327          6.7071          20.057
v  Velocity[Z]                 -29.485          29.327        0.088732      -0.0017707
v  ǁVelocityǁ                 0.019551          33.024          10.545          20.215
v  Pressure                    -367.72          344.83         -55.225          31.323
v  k                        3.5197e-08           43.08          4.0153          1.6665
v  omega                         1e-24      1.1696e+07          8159.3          11.888
v  turbulent_viscosity      2.3048e-14          1.3108         0.01573         0.11064
v  CourantNb                  0.021743          2075.6          43.975          1.3768
v  FourierNb                  0.010871           14976          94.578         0.69323
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010819        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15026          138.55            2.07


 TIME FOR THE TIME STEP              601:        0.48010E+02

===============================================================


 INSTANT    0.602000000E+02   TIME STEP NUMBER             602
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.708093868E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30989E+02 0.20096E+02
   Friction velocity        uet   :  0.12613E-02 0.26712E+01
   Friction velocity        uk    :  0.28818E-01 0.30907E+01
   Dimensionless distance   yplus :  0.13825E+00 0.30096E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1983   0.44732E-02   0.35641E+00 
c  VelocityY    0.29416E+04    1983   0.44732E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1983   0.44732E-02   0.00000E+00 
c  Pressure     0.43332E+00    7022   0.27513E-01   0.20521E+00 
c  k            0.21545E+04    1273   0.60786E-04   0.76146E+00 
c  omega        0.10267E+08     225   0.34440E-04   0.26293E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -59320                             1
a  Local Time Step      1.1768e-05                         44333


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8734               1     -0.00043717      6.9612e-06
v  Velocity[Y]                 -16.107          30.458          6.7128          20.056
v  Velocity[Z]                 -30.103           29.18        0.041648      -0.0027174
v  ǁVelocityǁ                 0.010489          34.503           10.52          20.213
v  Pressure                     -361.3          346.14          -54.06           31.22
v  k                        1.0642e-09          42.744          3.9486          1.6666
v  omega                         1e-24      1.7576e+07          8067.3          11.855
v  turbulent_viscosity      1.4828e-13          1.3194        0.015686         0.11063
v  CourantNb                  0.034961          2081.6          44.084          1.3771
v  FourierNb                   0.01087           15092          92.911         0.69224
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14798        0.010818         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15154             137          2.0693


 TIME FOR THE TIME STEP              602:        0.47040E+02

===============================================================


 INSTANT    0.603000000E+02   TIME STEP NUMBER             603
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.810333260E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31295E+02 0.19781E+02
   Friction velocity        uet   :  0.37070E-03 0.28010E+01
   Friction velocity        uk    :  0.22475E-01 0.32437E+01
   Dimensionless distance   yplus :  0.16341E+00 0.28317E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        399
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1860   0.45556E-02   0.37958E+00 
c  VelocityY    0.29416E+04    1860   0.45556E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1860   0.45556E-02   0.00000E+00 
c  Pressure     0.43044E+00    7010   0.27629E-01   0.20302E+00 
c  k            0.21581E+04    1427   0.59878E-04   0.87091E+00 
c  omega        0.13541E+28       2   0.11097E-22   0.98240E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6356e+05                             2
a  Local Time Step      1.1365e-05                         44349


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7139          1.2691      -0.0013096      7.4196e-06
v  Velocity[Y]                  -15.12          31.667          6.7364          20.056
v  Velocity[Z]                 -31.044          29.041       -0.014985      -0.0037807
v  ǁVelocityǁ                0.0089133          36.365          10.504          20.213
v  Pressure                    -360.69          347.86         -51.677          31.531
v  k                        7.1081e-09          51.866          3.9319           1.667
v  omega                         1e-24      5.6487e+07          8334.2          11.855
v  turbulent_viscosity      8.2744e-15          1.3258        0.015688         0.11064
v  CourantNb                  0.014579          2081.5          44.366          1.3771
v  FourierNb                  0.010868           15147          91.821         0.69165
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.148        0.010817        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15220          136.19          2.0687


 TIME FOR THE TIME STEP              603:        0.45299E+02

===============================================================


 INSTANT    0.604000000E+02   TIME STEP NUMBER             604
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.253098519E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31686E+02 0.16431E+02
   Friction velocity        uet   :  0.43122E-03 0.31051E+01
   Friction velocity        uk    :  0.99430E-02 0.30819E+01
   Dimensionless distance   yplus :  0.89779E-01 0.27529E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1791   0.44388E-02   0.40270E+00 
c  VelocityY    0.29418E+04    1791   0.44388E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1791   0.44388E-02   0.00000E+00 
c  Pressure     0.41725E+00    7095   0.32032E-01   0.19633E+00 
c  k            0.21651E+04    1516   0.66831E-04   0.10522E+01 
c  omega        0.18786E+08     211   0.23078E-03   0.40982E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74987                             4
a  Local Time Step      1.1083e-05                         44355


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5036           1.485      -0.0030471      6.6749e-06
v  Velocity[Y]                 -15.205          33.864          6.7747          20.055
v  Velocity[Z]                 -33.221          29.021       -0.056502      -0.0048957
v  ǁVelocityǁ                 0.017699          36.212          10.529          20.213
v  Pressure                     -402.2          347.82         -49.886          31.596
v  k                         1.218e-07          60.844          3.9489          1.6677
v  omega                         1e-24       8.975e+07          9322.5          11.925
v  turbulent_viscosity      8.0285e-15          1.3302        0.015726         0.11062
v  CourantNb                  0.049151            2248          44.389          1.3767
v  FourierNb                  0.010867           15314          90.504         0.69127
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14805        0.010817        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15370          134.89           2.068


 TIME FOR THE TIME STEP              604:        0.45040E+02

===============================================================


 INSTANT    0.605000000E+02   TIME STEP NUMBER             605
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.229600192E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30647E+02 0.14407E+02
   Friction velocity        uet   :  0.33908E-03 0.32814E+01
   Friction velocity        uk    :  0.22960E-01 0.32143E+01
   Dimensionless distance   yplus :  0.18745E+00 0.27490E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29420E+04    1904   0.44169E-02   0.43039E+00 
c  VelocityY    0.29420E+04    1904   0.44169E-02   0.00000E+00 
c  VelocityZ    0.29420E+04    1904   0.44169E-02   0.00000E+00 
c  Pressure     0.43664E+00    7074   0.36443E-01   0.20478E+00 
c  k            0.21784E+04    1374   0.69332E-04   0.11100E+01 
c  omega        0.52116E+08     159   0.58413E-04   0.28430E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3722e+05                             6
a  Local Time Step      1.1372e-05                         44390


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6085          1.5238      -0.0052822      6.4065e-06
v  Velocity[Y]                 -16.032          32.923          6.8199          20.056
v  Velocity[Z]                 -33.266          28.867       -0.056052      -0.0058327
v  ǁVelocityǁ                 0.020966          35.528          10.573          20.214
v  Pressure                    -431.72          347.17         -48.383           31.88
v  k                        1.1879e-06          65.948           3.964          1.6685
v  omega                         1e-24      6.8575e+07            9267          11.917
v  turbulent_viscosity      2.1387e-13          1.3367        0.015762         0.11065
v  CourantNb                  0.030275          2755.3          44.332          1.3762
v  FourierNb                  0.010865           15521          90.072         0.69085
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14738        0.010816          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15571           134.4          2.0671


 TIME FOR THE TIME STEP              605:        0.46138E+02

===============================================================


 INSTANT    0.606000000E+02   TIME STEP NUMBER             606
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.254382804E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30439E+02 0.14925E+02
   Friction velocity        uet   :  0.11895E-02 0.32612E+01
   Friction velocity        uk    :  0.61263E-02 0.31831E+01
   Dimensionless distance   yplus :  0.54418E-01 0.27944E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1948   0.43936E-02   0.43195E+00 
c  VelocityY    0.29422E+04    1948   0.43936E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1948   0.43936E-02   0.00000E+00 
c  Pressure     0.43298E+00    7025   0.36276E-01   0.20325E+00 
c  k            0.21935E+04    1141   0.71961E-04   0.11309E+01 
c  omega        0.32634E+08     134   0.46689E-04   0.90621E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0014746                             1
a  omega                -2.075e+05                             5
a  Local Time Step      1.1833e-05                         44413


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6966          1.4605      -0.0071354      2.4463e-06
v  Velocity[Y]                 -23.658          29.844          6.8307          20.057
v  Velocity[Z]                 -32.293          28.685       -0.027905       -0.006721
v  ǁVelocityǁ                 0.015054          33.412           10.59          20.214
v  Pressure                    -438.47          347.67         -48.194          31.736
v  k                        2.1181e-08          59.952          3.9868          1.6695
v  omega                         1e-24      3.5035e+07          8651.7          11.899
v  turbulent_viscosity      1.9905e-13          1.3422        0.015797         0.11068
v  CourantNb                  0.041666          2860.5          44.418          1.3759
v  FourierNb                  0.010864           15555          89.857          0.6908
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14841        0.010817        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15603          134.27          2.0667


 TIME FOR THE TIME STEP              606:        0.45111E+02

===============================================================


 INSTANT    0.607000000E+02   TIME STEP NUMBER             607
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.205666073E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31042E+02 0.14335E+02
   Friction velocity        uet   :  0.52541E-03 0.28352E+01
   Friction velocity        uk    :  0.17982E-01 0.29116E+01
   Dimensionless distance   yplus :  0.13990E+00 0.28248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1971   0.45545E-02   0.40455E+00 
c  VelocityY    0.29423E+04    1971   0.45545E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1971   0.45545E-02   0.00000E+00 
c  Pressure     0.42322E+00    6739   0.33085E-01   0.19963E+00 
c  k            0.22055E+04     997   0.70565E-04   0.11273E+01 
c  omega        0.17246E+08     176   0.60127E-04   0.63424E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                    -0.0011012                             1
a  omega               -2.3992e+05                             4
a  Local Time Step      1.1665e-05                         44400


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.677           1.166      -0.0073722      3.4059e-06
v  Velocity[Y]                 -27.987          29.711          6.7824          20.056
v  Velocity[Z]                 -31.771          28.625        0.003399      -0.0072393
v  ǁVelocityǁ                0.0092797          33.146          10.585          20.214
v  Pressure                    -426.62          348.16         -48.649          31.531
v  k                        5.5906e-09          45.649          4.0245          1.6705
v  omega                         1e-24      2.3086e+07          8536.6          11.917
v  turbulent_viscosity      1.0853e-15          1.3468        0.015813         0.11073
v  CourantNb                  0.022671          2392.8          44.456          1.3757
v  FourierNb                  0.010863           15497          90.141         0.69089
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14805        0.010819        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15549           134.6          2.0666


 TIME FOR THE TIME STEP              607:        0.45025E+02

===============================================================


 INSTANT    0.608000000E+02   TIME STEP NUMBER             608
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.660134466E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30771E+02 0.17624E+02
   Friction velocity        uet   :  0.10410E-02 0.28018E+01
   Friction velocity        uk    :  0.17351E-01 0.31900E+01
   Dimensionless distance   yplus :  0.16857E+00 0.28429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :        987
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1980   0.45283E-02   0.37933E+00 
c  VelocityY    0.29423E+04    1980   0.45283E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1980   0.45283E-02   0.00000E+00 
c  Pressure     0.42722E+00    7073   0.30300E-01   0.20184E+00 
c  k            0.22120E+04    1306   0.88067E-04   0.10706E+01 
c  omega        0.12405E+08     253   0.24567E-03   0.25948E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -66314                             1
a  Local Time Step      1.0598e-05                         44420


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5076          1.1939      -0.0063047      2.1009e-06
v  Velocity[Y]                 -32.473          29.624           6.689          20.056
v  Velocity[Z]                 -30.407           28.39        0.016956      -0.0076394
v  ǁVelocityǁ                0.0087236          32.936           10.61          20.213
v  Pressure                    -402.57          347.68          -50.17          31.297
v  k                        1.7522e-08          87.877          4.1134          1.6717
v  omega                         1e-24      7.9495e+07          9006.8           11.93
v  turbulent_viscosity      4.6813e-16          1.3499        0.015829         0.11079
v  CourantNb                  0.018045          2038.9          44.362          1.3755
v  FourierNb                  0.010862           15414          91.435          0.6915
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1484        0.010819        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15472           135.8           2.067


 TIME FOR THE TIME STEP              608:        0.46359E+02

===============================================================


 INSTANT    0.609000000E+02   TIME STEP NUMBER             609
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.439322026E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30092E+02 0.22298E+02
   Friction velocity        uet   :  0.14109E-02 0.27923E+01
   Friction velocity        uk    :  0.24309E-01 0.30870E+01
   Dimensionless distance   yplus :  0.16885E+00 0.32160E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1943   0.45139E-02   0.36996E+00 
c  VelocityY    0.29423E+04    1943   0.45139E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1943   0.45139E-02   0.00000E+00 
c  Pressure     0.40963E+00    7009   0.33345E-01   0.19263E+00 
c  k            0.22121E+04    1418   0.13106E-03   0.94432E+00 
c  omega        0.40261E+08     324   0.34454E-04   0.70765E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0046e+05                             1
a  Local Time Step       1.043e-05                         44387


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2624          1.3442      -0.0050615     -3.0447e-07
v  Velocity[Y]                 -36.245          29.997          6.6442          20.056
v  Velocity[Z]                 -28.598          28.379        0.041435      -0.0080706
v  ǁVelocityǁ                 0.013322          38.172          10.646          20.214
v  Pressure                    -406.14          346.18         -52.938          31.166
v  k                        8.8764e-09          112.58          4.2173           1.673
v  omega                         1e-24      4.0489e+07            8487          11.882
v  turbulent_viscosity      3.7185e-14          1.3523         0.01586         0.11087
v  CourantNb                  0.022203          2031.2          44.238          1.3755
v  FourierNb                  0.010861           15384          93.501         0.69285
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14854        0.010818        0.045661


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15449          137.74          2.0683


 TIME FOR THE TIME STEP              609:        0.46014E+02

===============================================================


 INSTANT    0.610000000E+02   TIME STEP NUMBER             610
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.135627180E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.50481E+02 0.14244E+02
   Friction velocity        uet   :  0.20426E-02 0.33722E+01
   Friction velocity        uk    :  0.24249E-01 0.47947E+01
   Dimensionless distance   yplus :  0.16650E+00 0.41026E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        422
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1976   0.44235E-02   0.37280E+00 
c  VelocityY    0.29423E+04    1976   0.44235E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1976   0.44235E-02   0.00000E+00 
c  Pressure     0.43511E+00    7106   0.37821E-01   0.20574E+00 
c  k            0.22092E+04    1474   0.14193E-03   0.82726E+00 
c  omega        0.14582E+08     469   0.48565E-04   0.24573E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -19996                             1
a  Local Time Step      1.1067e-05                         44356


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0882          1.4747      -0.0042221     -9.7934e-07
v  Velocity[Y]                 -28.223          30.424            6.66          20.057
v  Velocity[Z]                 -28.647          28.523        0.068931      -0.0084985
v  ǁVelocityǁ                 0.020804          33.454          10.666          20.215
v  Pressure                    -407.45          344.21         -56.161          31.271
v  k                        6.9009e-09          56.001          4.2425          1.6746
v  omega                         1e-24      2.1743e+07          8203.1          11.869
v  turbulent_viscosity      1.1937e-14           1.353        0.015889         0.11096
v  CourantNb                  0.017271          2214.9          44.171          1.3756
v  FourierNb                  0.010861           15395          94.622         0.69407
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010818        0.045639


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15467          138.79          2.0697


 TIME FOR THE TIME STEP              610:        0.47954E+02

===============================================================


 INSTANT    0.611000000E+02   TIME STEP NUMBER             611
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.291919946E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30923E+02 0.13857E+02
   Friction velocity        uet   :  0.21805E-02 0.27206E+01
   Friction velocity        uk    :  0.94616E-02 0.29557E+01
   Dimensionless distance   yplus :  0.10135E+00 0.27562E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :        956
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2107   0.45981E-02   0.37137E+00 
c  VelocityY    0.29423E+04    2107   0.45981E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2107   0.45981E-02   0.00000E+00 
c  Pressure     0.43902E+00    7108   0.37252E-01   0.20706E+00 
c  k            0.22069E+04    1458   0.72894E-04   0.67333E+00 
c  omega        0.10513E+08     297   0.21281E-03   0.10686E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5203e+05                             1
a  Local Time Step       1.104e-05                         44304


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1232          1.5737      -0.0027146      3.5318e-08
v  Velocity[Y]                 -17.842          30.678          6.6958          20.057
v  Velocity[Z]                 -28.771          28.595        0.089607      -0.0085741
v  ǁVelocityǁ                0.0085767          33.374           10.66          20.215
v  Pressure                     -408.7          342.75         -58.336          31.372
v  k                        2.9211e-08          58.095          4.2623          1.6762
v  omega                         1e-24      6.7674e+07          8412.7           11.88
v  turbulent_viscosity      3.4193e-15          1.3546          0.0159         0.11107
v  CourantNb                  0.016683          2846.3          44.262          1.3758
v  FourierNb                  0.010861           15431          95.854         0.69502
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14824        0.010816        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15507          140.12          2.0709


 TIME FOR THE TIME STEP              611:        0.49082E+02

===============================================================


 INSTANT    0.612000000E+02   TIME STEP NUMBER             612
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.535710429E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31032E+02 0.13128E+02
   Friction velocity        uet   :  0.60778E-03 0.27744E+01
   Friction velocity        uk    :  0.17709E-01 0.29934E+01
   Dimensionless distance   yplus :  0.67625E-01 0.28011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        501
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2164   0.47103E-02   0.37750E+00 
c  VelocityY    0.29422E+04    2164   0.47103E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2164   0.47103E-02   0.00000E+00 
c  Pressure     0.44534E+00    7035   0.33504E-01   0.21083E+00 
c  k            0.22058E+04    1398   0.77011E-04   0.65632E+00 
c  omega        0.22481E+08     373   0.16234E-03   0.26617E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -64186                             2
a  Local Time Step      1.0879e-05                         44272


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0418          1.6495      0.00013673      1.4467e-06
v  Velocity[Y]                   -16.8          32.447          6.7282          20.056
v  Velocity[Z]                 -29.152          28.794        0.092198      -0.0081554
v  ǁVelocityǁ                 0.011172          33.504          10.618          20.215
v  Pressure                    -408.81          344.18         -58.994          31.418
v  k                        4.4405e-08          58.354          4.2496           1.678
v  omega                         1e-24      1.1124e+08          8821.4          11.928
v  turbulent_viscosity      1.1289e-14           1.354        0.015903         0.11119
v  CourantNb                   0.01901          2050.9          44.284          1.3761
v  FourierNb                  0.010862           15431          97.925         0.69616
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889        0.010817        0.045647


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15508          142.21          2.0723


 TIME FOR THE TIME STEP              612:        0.48101E+02

===============================================================


 INSTANT    0.613000000E+02   TIME STEP NUMBER             613
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.184369559E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30052E+02 0.13511E+02
   Friction velocity        uet   :  0.88269E-03 0.28563E+01
   Friction velocity        uk    :  0.30178E-01 0.31822E+01
   Dimensionless distance   yplus :  0.18669E+00 0.30296E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        494
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    2162   0.46253E-02   0.39169E+00 
c  VelocityY    0.29421E+04    2162   0.46253E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    2162   0.46253E-02   0.00000E+00 
c  Pressure     0.45638E+00    7041   0.31302E-01   0.21611E+00 
c  k            0.22037E+04    1161   0.67241E-04   0.74287E+00 
c  omega        0.54034E+08     316   0.27241E-04   0.75855E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2766e+05                             3
a  Local Time Step      1.1201e-05                         44237


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0356          1.7443       0.0034689      5.5695e-07
v  Velocity[Y]                 -16.194          32.574          6.7348          20.056
v  Velocity[Z]                 -29.588          28.896        0.079317      -0.0080347
v  ǁVelocityǁ                 0.015616          33.604          10.562          20.214
v  Pressure                    -401.87          345.72         -59.103          31.136
v  k                        6.6045e-09          49.906          4.1616          1.6799
v  omega                         1e-24      5.6082e+07          8455.4          11.895
v  turbulent_viscosity      5.9889e-14          1.3513        0.015872         0.11132
v  CourantNb                  0.019793          2045.4          44.199          1.3764
v  FourierNb                  0.010863           15615          98.505         0.69693
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14792        0.010818        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15664           142.7          2.0734


 TIME FOR THE TIME STEP              613:        0.48289E+02

===============================================================


 INSTANT    0.614000000E+02   TIME STEP NUMBER             614
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.407626036E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29637E+02 0.14120E+02
   Friction velocity        uet   :  0.66320E-03 0.27516E+01
   Friction velocity        uk    :  0.20244E-01 0.30470E+01
   Dimensionless distance   yplus :  0.14782E+00 0.34588E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :        932
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    2207   0.43789E-02   0.40058E+00 
c  VelocityY    0.29418E+04    2207   0.43789E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    2207   0.43789E-02   0.00000E+00 
c  Pressure     0.42064E+00    7041   0.31766E-01   0.19898E+00 
c  k            0.22005E+04    1330   0.58682E-04   0.64440E+00 
c  omega        0.17218E+08     261   0.55025E-04   0.46718E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -87065                             1
a  Local Time Step      1.1051e-05                         44244


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0005          1.9543       0.0065751      6.7011e-07
v  Velocity[Y]                 -15.254          33.162           6.713          20.055
v  Velocity[Z]                 -28.739          29.264        0.043606      -0.0079172
v  ǁVelocityǁ                  0.01744          33.443          10.527          20.213
v  Pressure                    -383.74          346.49         -58.831          30.604
v  k                         4.611e-09          48.086          4.0695          1.6819
v  omega                         1e-24      2.8956e+07            8333          11.864
v  turbulent_viscosity      2.5909e-14          1.3469        0.015805         0.11146
v  CourantNb                   0.02374          2035.4          44.062          1.3766
v  FourierNb                  0.010865           15844          97.122         0.69695
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14878        0.010819        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15905          141.18          2.0736


 TIME FOR THE TIME STEP              614:        0.48212E+02

===============================================================


 INSTANT    0.615000000E+02   TIME STEP NUMBER             615
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240378289E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31450E+02 0.21378E+02
   Friction velocity        uet   :  0.13786E-02 0.26927E+01
   Friction velocity        uk    :  0.16150E-01 0.37253E+01
   Dimensionless distance   yplus :  0.10352E+00 0.35645E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :        918
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    2146   0.45620E-02   0.40901E+00 
c  VelocityY    0.29417E+04    2146   0.45620E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    2146   0.45620E-02   0.00000E+00 
c  Pressure     0.44131E+00    7045   0.29671E-01   0.20878E+00 
c  k            0.21986E+04    1544   0.56983E-04   0.64866E+00 
c  omega        0.11540E+08     262   0.83345E-04   0.40548E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5745e+05                             2
a  Local Time Step      1.1974e-05                         44267


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8285          2.1091       0.0089088      3.6917e-07
v  Velocity[Y]                 -15.601          30.719           6.713          20.056
v  Velocity[Z]                 -28.741           29.07        0.010249      -0.0072739
v  ǁVelocityǁ                 0.017034          33.482          10.508          20.213
v  Pressure                    -368.09          347.89         -57.436          30.637
v  k                        1.1856e-08          37.173          3.9678           1.684
v  omega                         1e-24      3.5389e+07          8256.5          11.834
v  turbulent_viscosity      3.7986e-15          1.3433        0.015736         0.11162
v  CourantNb                  0.051223          2029.3          44.169           1.377
v  FourierNb                  0.010867           15902          95.353         0.69681
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14819        0.010818        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15976          139.52          2.0738


 TIME FOR THE TIME STEP              615:        0.48369E+02

===============================================================


 INSTANT    0.616000000E+02   TIME STEP NUMBER             616
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.308510972E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31998E+02 0.20334E+02
   Friction velocity        uet   :  0.94894E-03 0.26904E+01
   Friction velocity        uk    :  0.87421E-02 0.30729E+01
   Dimensionless distance   yplus :  0.11072E+00 0.28722E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    2056   0.45043E-02   0.40825E+00 
c  VelocityY    0.29417E+04    2056   0.45043E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    2056   0.45043E-02   0.00000E+00 
c  Pressure     0.43863E+00    7041   0.27878E-01   0.20835E+00 
c  k            0.21981E+04    1572   0.54509E-04   0.73914E+00 
c  omega        0.17491E+08     207   0.62488E-04   0.53730E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7012e+05                             2
a  Local Time Step      1.1309e-05                         44281


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.62344          2.1967       0.0098927       3.389e-06
v  Velocity[Y]                 -15.252          30.401          6.7433          20.056
v  Velocity[Z]                 -30.446          29.058       -0.027402      -0.0065741
v  ǁVelocityǁ                0.0045245          36.395           10.51          20.214
v  Pressure                       -344           349.3         -55.128          30.901
v  k                        3.2779e-08          46.755          3.9078          1.6864
v  omega                         1e-24      5.0048e+07          8256.3          11.835
v  turbulent_viscosity        2.45e-15          1.3398        0.015694         0.11178
v  CourantNb                  0.033584          2031.6          44.544          1.3772
v  FourierNb                   0.01087           15793          94.136         0.69707
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14818        0.010816        0.045659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15876          138.68          2.0742


 TIME FOR THE TIME STEP              616:        0.47685E+02

===============================================================


 INSTANT    0.617000000E+02   TIME STEP NUMBER             617
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.131506870E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32001E+02 0.17091E+02
   Friction velocity        uet   :  0.29920E-02 0.30293E+01
   Friction velocity        uk    :  0.11116E-01 0.32248E+01
   Dimensionless distance   yplus :  0.14392E+00 0.27765E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :        970
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    2011   0.45417E-02   0.40198E+00 
c  VelocityY    0.29417E+04    2011   0.45417E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    2011   0.45417E-02   0.00000E+00 
c  Pressure     0.44088E+00    7001   0.30466E-01   0.20924E+00 
c  k            0.22008E+04    1546   0.57528E-04   0.88568E+00 
c  omega        0.15843E+08     182   0.44546E-04   0.38432E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -88880                             2
a  Local Time Step       1.206e-05                         44296


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.57283          2.2143       0.0097895      6.0922e-06
v  Velocity[Y]                 -15.216          30.389           6.795          20.056
v  Velocity[Z]                 -32.524          28.845       -0.042568      -0.0059209
v  ǁVelocityǁ                0.0062214          36.269          10.552          20.214
v  Pressure                    -398.23          349.93         -52.673          31.285
v  k                        2.0569e-08          59.661          3.8948          1.6888
v  omega                         1e-24       2.621e+07          8202.4           11.83
v  turbulent_viscosity      4.7144e-14          1.3364        0.015683         0.11196
v  CourantNb                  0.026232          2044.1          44.672           1.377
v  FourierNb                  0.010873           15764          92.126         0.69742
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010815        0.045665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97163           15815           136.8          2.0744


 TIME FOR THE TIME STEP              617:        0.46835E+02

===============================================================


 INSTANT    0.618000000E+02   TIME STEP NUMBER             618
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.487080274E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29997E+02 0.13897E+02
   Friction velocity        uet   :  0.17555E-02 0.30818E+01
   Friction velocity        uk    :  0.20728E-01 0.29338E+01
   Dimensionless distance   yplus :  0.68947E-01 0.28067E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        460
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1965   0.43877E-02   0.40160E+00 
c  VelocityY    0.29417E+04    1965   0.43877E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1965   0.43877E-02   0.00000E+00 
c  Pressure     0.44177E+00    7084   0.34620E-01   0.20872E+00 
c  k            0.22095E+04    1497   0.61181E-04   0.97976E+00 
c  omega        0.11526E+08     245   0.14448E-03   0.10582E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7898e+05                             2
a  Local Time Step      1.1365e-05                         44308


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.53329           2.169       0.0089431       9.308e-06
v  Velocity[Y]                 -14.438          32.169           6.852          20.056
v  Velocity[Z]                 -32.734          29.084       -0.030711      -0.0051215
v  ǁVelocityǁ                 0.011202          35.049          10.609          20.214
v  Pressure                     -429.2          351.54         -50.899          31.542
v  k                        5.0073e-08          67.107          3.9133          1.6911
v  omega                         1e-24      6.4038e+07          8456.6          11.852
v  turbulent_viscosity      6.9433e-14          1.3345         0.01569         0.11214
v  CourantNb                  0.062716          2596.2           44.74          1.3767
v  FourierNb                  0.010875           15729          90.927         0.69813
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010814        0.045642


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15781          135.67          2.0748


 TIME FOR THE TIME STEP              618:        0.47101E+02

===============================================================


 INSTANT    0.619000000E+02   TIME STEP NUMBER             619
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.466330474E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30684E+02 0.13990E+02
   Friction velocity        uet   :  0.15105E-02 0.31763E+01
   Friction velocity        uk    :  0.17312E-01 0.28775E+01
   Dimensionless distance   yplus :  0.94596E-01 0.28308E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1894   0.44573E-02   0.39551E+00 
c  VelocityY    0.29418E+04    1894   0.44573E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1894   0.44573E-02   0.00000E+00 
c  Pressure     0.41520E+00    7020   0.37076E-01   0.19663E+00 
c  k            0.22227E+04    1505   0.61890E-04   0.10193E+01 
c  omega        0.20916E+08     241   0.11433E-03   0.18932E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -82232                             2
a  Local Time Step      1.1603e-05                         44307


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.60491          2.0611       0.0070737      1.0835e-05
v  Velocity[Y]                 -19.812          30.083          6.8798          20.057
v  Velocity[Z]                 -31.677          28.706       0.0070746      -0.0041018
v  ǁVelocityǁ                 0.015649          33.057           10.64          20.215
v  Pressure                    -437.08          352.57         -50.069          31.631
v  k                        2.4352e-07          63.274          3.9335          1.6933
v  omega                         1e-24       8.423e+07          8737.3            11.9
v  turbulent_viscosity      1.3514e-13          1.3314        0.015708         0.11233
v  CourantNb                  0.024404          2775.2          44.766          1.3764
v  FourierNb                  0.010878           15543          90.796         0.69921
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14905        0.010815        0.045615


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15598          135.56          2.0756


 TIME FOR THE TIME STEP              619:        0.46361E+02

===============================================================


 INSTANT    0.620000000E+02   TIME STEP NUMBER             620
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.298670832E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30869E+02 0.14097E+02
   Friction velocity        uet   :  0.92083E-03 0.28256E+01
   Friction velocity        uk    :  0.11269E-01 0.28990E+01
   Dimensionless distance   yplus :  0.49024E-01 0.28386E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        449
   Nb of faces within the viscous sub-layer     :        956
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1872   0.43473E-02   0.36030E+00 
c  VelocityY    0.29418E+04    1872   0.43473E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1872   0.43473E-02   0.00000E+00 
c  Pressure     0.42435E+00    7010   0.35550E-01   0.20078E+00 
c  k            0.22357E+04    1498   0.63548E-04   0.10635E+01 
c  omega        0.33021E+08     166   0.31744E-04   0.60324E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2195e+05                             2
a  Local Time Step      1.1511e-05                         44281


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.6771          1.9044       0.0050502      9.1494e-06
v  Velocity[Y]                 -23.937          29.917          6.8282          20.057
v  Velocity[Z]                 -31.594          28.621        0.058835      -0.0033487
v  ǁVelocityǁ                0.0029163           32.35          10.617          20.215
v  Pressure                    -427.72          352.54         -50.154          31.469
v  k                        1.5784e-07          68.149          3.9646          1.6951
v  omega                         1e-24      4.2774e+07          8359.9          11.869
v  turbulent_viscosity      3.5709e-14          1.3271        0.015715         0.11252
v  CourantNb                 0.0083668          2416.1          44.785          1.3764
v  FourierNb                  0.010882           15296          91.163         0.70045
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010815        0.045637


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15357          135.95          2.0769


 TIME FOR THE TIME STEP              620:        0.46957E+02

===============================================================


 INSTANT    0.621000000E+02   TIME STEP NUMBER             621
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.238849262E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30722E+02 0.14811E+02
   Friction velocity        uet   :  0.71032E-03 0.27519E+01
   Friction velocity        uk    :  0.22877E-01 0.31771E+01
   Dimensionless distance   yplus :  0.13506E+00 0.27684E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        382
   Nb of faces within the viscous sub-layer     :        961
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1784   0.44389E-02   0.32583E+00 
c  VelocityY    0.29417E+04    1784   0.44389E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1784   0.44389E-02   0.00000E+00 
c  Pressure     0.41438E+00    6846   0.31442E-01   0.19593E+00 
c  k            0.22434E+04    1464   0.77087E-04   0.10332E+01 
c  omega        0.13277E+08     206   0.68003E-04   0.46944E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5696e+05                             2
a  Local Time Step       1.119e-05                         44255


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.72822          1.6979        0.003933       4.003e-06
v  Velocity[Y]                 -31.753          29.768           6.715          20.056
v  Velocity[Z]                 -30.307          28.433        0.087227      -0.0026064
v  ǁVelocityǁ                 0.010527          33.089          10.621          20.214
v  Pressure                    -404.38           351.2         -50.824          31.237
v  k                        3.3486e-07          79.533          4.0387          1.6965
v  omega                         1e-24       2.264e+07          8378.8          11.873
v  turbulent_viscosity      3.9338e-14          1.3217        0.015738          0.1127
v  CourantNb                  0.026848          2080.5          44.436          1.3763
v  FourierNb                  0.010886           15007           91.69           0.702
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14777        0.010815        0.045655


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15076          136.13          2.0783


 TIME FOR THE TIME STEP              621:        0.44646E+02

===============================================================


 INSTANT    0.622000000E+02   TIME STEP NUMBER             622
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.142206376E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29802E+02 0.21439E+02
   Friction velocity        uet   :  0.75897E-03 0.27635E+01
   Friction velocity        uk    :  0.11227E-01 0.29412E+01
   Dimensionless distance   yplus :  0.14247E+00 0.26839E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        367
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1753   0.45168E-02   0.30951E+00 
c  VelocityY    0.29415E+04    1753   0.45168E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1753   0.45168E-02   0.00000E+00 
c  Pressure     0.44894E+00    7035   0.30738E-01   0.21087E+00 
c  k            0.22418E+04    1416   0.97045E-04   0.92176E+00 
c  omega        0.10993E+08     405   0.70349E-04   0.43728E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5729e+05                             2
a  Local Time Step       1.104e-05                         44260


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79014          1.4969       0.0030786      2.8163e-06
v  Velocity[Y]                 -34.243          30.031           6.635          20.055
v  Velocity[Z]                 -28.525          28.545         0.11895      -0.0016203
v  ǁVelocityǁ                 0.011882          40.014          10.635          20.213
v  Pressure                    -407.08          348.64         -52.291          31.202
v  k                        8.8053e-09           92.82          4.1403          1.6977
v  omega                         1e-24      1.6799e+07            8376          11.909
v  turbulent_viscosity       4.844e-14          1.3151         0.01578         0.11289
v  CourantNb                  0.049494          2063.7          44.267          1.3764
v  FourierNb                   0.01089           14763          93.008         0.70433
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14813        0.010816        0.045692


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14840          137.28          2.0807


 TIME FOR THE TIME STEP              622:        0.44204E+02

===============================================================


 INSTANT    0.623000000E+02   TIME STEP NUMBER             623
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.550910560E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55397E+02 0.13867E+02
   Friction velocity        uet   :  0.12015E-02 0.34548E+01
   Friction velocity        uk    :  0.16351E-01 0.44058E+01
   Dimensionless distance   yplus :  0.78945E-01 0.35427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1890   0.45262E-02   0.30410E+00 
c  VelocityY    0.29415E+04    1890   0.45262E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1890   0.45262E-02   0.00000E+00 
c  Pressure     0.43388E+00    7123   0.34457E-01   0.20569E+00 
c  k            0.22338E+04    1343   0.10322E-03   0.76414E+00 
c  omega        0.10854E+08     457   0.60599E-04   0.25271E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2864e+05                             3
a  Local Time Step       1.143e-05                         44279


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.81435          1.4487       0.0019452      3.5255e-06
v  Velocity[Y]                 -31.948           30.33          6.6077          20.056
v  Velocity[Z]                   -28.6          28.617          0.1491     -0.00068065
v  ǁVelocityǁ                 0.010829          33.437          10.637          20.215
v  Pressure                    -409.05          346.08         -54.249          31.522
v  k                        1.4897e-09          51.685           4.173          1.6986
v  omega                         1e-24      1.3915e+07          8286.8          11.896
v  turbulent_viscosity      2.6409e-14          1.3076        0.015838         0.11306
v  CourantNb                  0.061034          2041.3          44.275          1.3767
v  FourierNb                  0.010893           14664          94.696         0.70675
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14813        0.010816         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14745          138.97          2.0834


 TIME FOR THE TIME STEP              623:        0.46614E+02

===============================================================


 INSTANT    0.624000000E+02   TIME STEP NUMBER             624
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.149148969E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30682E+02 0.13592E+02
   Friction velocity        uet   :  0.39108E-03 0.30733E+01
   Friction velocity        uk    :  0.25161E-01 0.31589E+01
   Dimensionless distance   yplus :  0.13760E+00 0.32446E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1949   0.44872E-02   0.29366E+00 
c  VelocityY    0.29415E+04    1949   0.44872E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1949   0.44872E-02   0.00000E+00 
c  Pressure     0.45073E+00    7120   0.35724E-01   0.21352E+00 
c  k            0.22237E+04    1276   0.66090E-04   0.63001E+00 
c  omega        0.14904E+08     334   0.26559E-04   0.22703E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4005e+05                             2
a  Local Time Step      1.0718e-05                         44288


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -0.822          1.3049      0.00064258      1.0358e-06
v  Velocity[Y]                 -17.454           30.77           6.608          20.056
v  Velocity[Z]                  -28.86          28.929         0.16213       0.0002001
v  ǁVelocityǁ                0.0053214          33.481          10.605          20.215
v  Pressure                    -409.52          346.18         -55.917          31.555
v  k                        2.3329e-09          49.551          4.1817          1.6991
v  omega                         1e-24      1.6599e+07          8086.5          11.883
v  turbulent_viscosity      1.6709e-15             1.3         0.01587         0.11322
v  CourantNb                  0.033984          3144.9          44.526           1.377
v  FourierNb                  0.010894           14566           95.29         0.70844
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488        0.010816        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14618          139.82          2.0855


 TIME FOR THE TIME STEP              624:        0.46259E+02

===============================================================


 INSTANT    0.625000000E+02   TIME STEP NUMBER             625
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.150122528E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30490E+02 0.13456E+02
   Friction velocity        uet   :  0.18736E-02 0.28799E+01
   Friction velocity        uk    :  0.11388E-01 0.31025E+01
   Dimensionless distance   yplus :  0.11378E+00 0.27954E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        458
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1984   0.45920E-02   0.30247E+00 
c  VelocityY    0.29414E+04    1984   0.45920E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1984   0.45920E-02   0.00000E+00 
c  Pressure     0.44399E+00    7056   0.33817E-01   0.20949E+00 
c  k            0.22137E+04    1261   0.61110E-04   0.54131E+00 
c  omega        0.11590E+08     267   0.38798E-04   0.25098E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9557e+05                             2
a  Local Time Step      1.1734e-05                         44295


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.83436          1.1102     -0.00040307     -3.3227e-07
v  Velocity[Y]                 -17.295          32.979          6.6298          20.055
v  Velocity[Z]                 -29.144           28.89          0.1536      0.00076307
v  ǁVelocityǁ                0.0079164          34.012          10.564          20.214
v  Pressure                    -408.47          346.44         -56.539          31.599
v  k                        9.2514e-09           49.12          4.1764          1.6993
v  omega                         1e-24       1.676e+07            8003          11.865
v  turbulent_viscosity      1.6207e-15          1.2939        0.015875         0.11337
v  CourantNb                  0.043626          2191.4          44.307          1.3772
v  FourierNb                  0.010894           14694          96.007         0.70972
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010817        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14743          140.31          2.0869


 TIME FOR THE TIME STEP              625:        0.45774E+02

===============================================================


 INSTANT    0.626000000E+02   TIME STEP NUMBER             626
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.383138545E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31854E+02 0.14108E+02
   Friction velocity        uet   :  0.68944E-03 0.29275E+01
   Friction velocity        uk    :  0.10798E-01 0.31017E+01
   Dimensionless distance   yplus :  0.14242E+00 0.29694E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2027   0.42663E-02   0.32338E+00 
c  VelocityY    0.29414E+04    2027   0.42663E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2027   0.42663E-02   0.00000E+00 
c  Pressure     0.44875E+00    7056   0.33709E-01   0.21274E+00 
c  k            0.22045E+04    1323   0.63859E-04   0.62572E+00 
c  omega        0.10671E+08     374   0.22156E-03   0.18442E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2685e+05                             2
a  Local Time Step      1.0676e-05                         44342


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.83238          1.0517     -0.00081224      9.1462e-08
v  Velocity[Y]                 -17.881          33.602           6.664          20.055
v  Velocity[Z]                 -29.097          29.048         0.12092        0.001334
v  ǁVelocityǁ                 0.010573          33.792          10.531          20.214
v  Pressure                    -402.34          345.95         -56.916          31.329
v  k                        1.7274e-07          54.485          4.1204          1.6991
v  omega                         1e-24      5.4413e+07          8716.3          11.908
v  turbulent_viscosity      1.1294e-14          1.2872        0.015867         0.11349
v  CourantNb                  0.037443          2014.2          44.008          1.3772
v  FourierNb                  0.010894           14852          96.558         0.71093
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010818         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92581           14910          140.57          2.0881


 TIME FOR THE TIME STEP              626:        0.46757E+02

===============================================================


 INSTANT    0.627000000E+02   TIME STEP NUMBER             627
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.159997096E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31434E+02 0.14311E+02
   Friction velocity        uet   :  0.82006E-03 0.28734E+01
   Friction velocity        uk    :  0.14019E-01 0.31389E+01
   Dimensionless distance   yplus :  0.12730E+00 0.34782E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        411
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1955   0.42470E-02   0.34729E+00 
c  VelocityY    0.29415E+04    1955   0.42470E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1955   0.42470E-02   0.00000E+00 
c  Pressure     0.42738E+00    7037   0.31175E-01   0.20243E+00 
c  k            0.21950E+04    1404   0.61482E-04   0.59345E+00 
c  omega        0.23890E+08     300   0.45638E-04   0.82273E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.1566e+05                             1
a  Local Time Step      1.1293e-05                         44410


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80557          1.0389      -0.0012159        1.66e-06
v  Velocity[Y]                 -16.373          33.609          6.6788          20.056
v  Velocity[Z]                 -28.516          29.133        0.067642       0.0019615
v  ǁVelocityǁ                 0.015377          34.086          10.512          20.215
v  Pressure                    -384.58          345.19          -56.67          31.021
v  k                        7.3422e-08          42.108          4.0381          1.6986
v  omega                         1e-24      2.8344e+07          8635.4          11.927
v  turbulent_viscosity      5.9981e-14          1.2806         0.01584          0.1136
v  CourantNb                  0.017476          2027.9          43.999          1.3774
v  FourierNb                  0.010892           14965          96.852          0.7118
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889        0.010818        0.045657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89801           15033          140.85          2.0892


 TIME FOR THE TIME STEP              627:        0.45943E+02

===============================================================


 INSTANT    0.628000000E+02   TIME STEP NUMBER             628
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.387687509E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30961E+02 0.22769E+02
   Friction velocity        uet   :  0.98070E-03 0.27429E+01
   Friction velocity        uk    :  0.24015E-01 0.30546E+01
   Dimensionless distance   yplus :  0.16746E+00 0.37089E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1887   0.44289E-02   0.35670E+00 
c  VelocityY    0.29415E+04    1887   0.44289E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1887   0.44289E-02   0.00000E+00 
c  Pressure     0.42369E+00    6999   0.29422E-01   0.20121E+00 
c  k            0.21856E+04    1420   0.53814E-04   0.60173E+00 
c  omega        0.12675E+08     286   0.53374E-04   0.45195E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                  -2.5e+05                             1
a  Local Time Step      1.0863e-05                         44384


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0161          1.1321       -0.001258     -5.5071e-07
v  Velocity[Y]                 -15.124          32.492           6.667          20.056
v  Velocity[Z]                 -28.512          29.282        0.017032       0.0024283
v  ǁVelocityǁ                 0.020115          32.927          10.479          20.215
v  Pressure                    -370.13          344.55         -55.528          30.912
v  k                        1.4919e-08          36.512          3.9715          1.6979
v  omega                         1e-24       2.402e+07          8363.5          11.894
v  turbulent_viscosity      2.8142e-13          1.2743        0.015803         0.11368
v  CourantNb                  0.050738            2030          44.148          1.3776
v  FourierNb                   0.01089           14951          95.725         0.71197
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010818        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15029          139.87          2.0896


 TIME FOR THE TIME STEP              628:        0.45110E+02

===============================================================


 INSTANT    0.629000000E+02   TIME STEP NUMBER             629
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.380978214E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31625E+02 0.20819E+02
   Friction velocity        uet   :  0.56329E-03 0.25299E+01
   Friction velocity        uk    :  0.33843E-01 0.31632E+01
   Dimensionless distance   yplus :  0.17538E+00 0.29691E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1032
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1849   0.46400E-02   0.38080E+00 
c  VelocityY    0.29414E+04    1849   0.46400E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1849   0.46400E-02   0.00000E+00 
c  Pressure     0.43684E+00    7039   0.27336E-01   0.20724E+00 
c  k            0.21775E+04    1374   0.54753E-04   0.72148E+00 
c  omega        0.11448E+08     212   0.54508E-04   0.27262E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3325e+05                             2
a  Local Time Step      1.1411e-05                         44417


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3048          1.2482      -0.0013206      1.0096e-06
v  Velocity[Y]                 -15.238          30.559          6.6747          20.056
v  Velocity[Z]                 -30.112          29.142       -0.036199       0.0023965
v  ǁVelocityǁ                 0.028764          36.328          10.453          20.215
v  Pressure                     -354.1          344.74          -53.11          31.013
v  k                        2.0769e-08          48.139          3.9509           1.697
v  omega                         1e-24      1.5124e+07          8217.2          11.868
v  turbulent_viscosity       4.331e-14          1.2682        0.015786         0.11374
v  CourantNb                  0.056704          2021.8          44.381          1.3777
v  FourierNb                  0.010888           14906          94.505         0.71191
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010818        0.045631


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0039           14973          138.89          2.0896


 TIME FOR THE TIME STEP              629:        0.44564E+02

===============================================================


 INSTANT    0.630000000E+02   TIME STEP NUMBER             630
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.375408212E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31513E+02 0.19765E+02
   Friction velocity        uet   :  0.15743E-02 0.29686E+01
   Friction velocity        uk    :  0.26330E-01 0.29171E+01
   Dimensionless distance   yplus :  0.18965E+00 0.28087E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1876   0.44726E-02   0.39557E+00 
c  VelocityY    0.29415E+04    1876   0.44726E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1876   0.44726E-02   0.00000E+00 
c  Pressure     0.43657E+00    7055   0.29929E-01   0.20644E+00 
c  k            0.21721E+04    1251   0.61716E-04   0.89074E+00 
c  omega        0.10388E+08     211   0.36502E-03   0.38276E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -19332                             1
a  Local Time Step      1.1262e-05                         44498


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5578          1.4159      -0.0013342     -8.4614e-08
v  Velocity[Y]                 -15.251            33.3          6.7009          20.056
v  Velocity[Z]                 -31.418          29.204       -0.095376       0.0023917
v  ǁVelocityǁ                 0.007881          36.843          10.461          20.215
v  Pressure                    -388.39          347.51         -50.783          31.229
v  k                        1.0474e-08          58.915          3.9667           1.696
v  omega                         1e-24      7.3545e+07          9403.5           11.94
v  turbulent_viscosity      4.1284e-14          1.2622        0.015815         0.11377
v  CourantNb                  0.025618          2006.4          44.439          1.3775
v  FourierNb                  0.010885           15070          92.723         0.71201
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14816        0.010818        0.045635


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15118          137.16          2.0895


 TIME FOR THE TIME STEP              630:        0.45096E+02

===============================================================


 INSTANT    0.631000000E+02   TIME STEP NUMBER             631
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.478478125E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30684E+02 0.17472E+02
   Friction velocity        uet   :  0.11442E-02 0.32380E+01
   Friction velocity        uk    :  0.80246E-02 0.31920E+01
   Dimensionless distance   yplus :  0.68488E-01 0.28231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1059
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1959   0.45700E-02   0.41359E+00 
c  VelocityY    0.29414E+04    1959   0.45700E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1959   0.45700E-02   0.00000E+00 
c  Pressure     0.40834E+00    7046   0.34345E-01   0.19286E+00 
c  k            0.21718E+04    1016   0.69802E-04   0.10389E+01 
c  omega        0.47132E+08     130   0.36045E-04   0.10617E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3005e+05                             3
a  Local Time Step       1.172e-05                         44546


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7138          1.6618      -0.0013836      1.6653e-06
v  Velocity[Y]                 -15.083          33.746          6.7406          20.056
v  Velocity[Z]                 -32.882          28.964        -0.11688       0.0022903
v  ǁVelocityǁ                0.0092388          35.253          10.514          20.215
v  Pressure                    -429.58          349.28         -49.023          31.521
v  k                        4.9311e-08          66.789          3.9977          1.6949
v  omega                         1e-24      3.7436e+07          8649.7          11.891
v  turbulent_viscosity      3.3827e-14          1.2567         0.01585         0.11378
v  CourantNb                  0.025222          2524.2          44.346           1.377
v  FourierNb                  0.010882           15212          91.566          0.7121
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14834        0.010818        0.045673


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15266          135.91          2.0891


 TIME FOR THE TIME STEP              631:        0.44711E+02

===============================================================


 INSTANT    0.632000000E+02   TIME STEP NUMBER             632
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.283153151E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30749E+02 0.15082E+02
   Friction velocity        uet   :  0.97226E-03 0.32951E+01
   Friction velocity        uk    :  0.10864E-01 0.31857E+01
   Dimensionless distance   yplus :  0.11960E+00 0.28302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :       1072
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1940   0.46078E-02   0.42788E+00 
c  VelocityY    0.29414E+04    1940   0.46078E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1940   0.46078E-02   0.00000E+00 
c  Pressure     0.43990E+00    6938   0.37137E-01   0.20845E+00 
c  k            0.21767E+04    1346   0.72520E-04   0.11079E+01 
c  omega        0.19635E+08     272   0.13259E-03   0.21513E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.305e+05                             1
a  Local Time Step      1.0556e-05                         44522


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8013          1.8607      -0.0007405      6.3145e-09
v  Velocity[Y]                 -20.599          30.143          6.7747          20.057
v  Velocity[Z]                 -33.291           28.95       -0.094382       0.0019248
v  ǁVelocityǁ                 0.016661          34.804          10.562          20.216
v  Pressure                    -446.22          349.14         -48.424          31.443
v  k                        4.4484e-08          66.233          4.0325          1.6934
v  omega                         1e-24      7.2271e+07          8919.4           11.91
v  turbulent_viscosity      5.3709e-14          1.2519        0.015892         0.11377
v  CourantNb                  0.014712          2843.9           44.23          1.3765
v  FourierNb                  0.010879           15250          91.111         0.71228
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14815         0.01082        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99772           15313          135.34          2.0888


 TIME FOR THE TIME STEP              632:        0.45212E+02

===============================================================


 INSTANT    0.633000000E+02   TIME STEP NUMBER             633
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.296011545E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30921E+02 0.15059E+02
   Friction velocity        uet   :  0.30375E-02 0.29733E+01
   Friction velocity        uk    :  0.18688E-01 0.30458E+01
   Dimensionless distance   yplus :  0.15918E+00 0.27730E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1070
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1904   0.45935E-02   0.41607E+00 
c  VelocityY    0.29414E+04    1904   0.45935E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1904   0.45935E-02   0.00000E+00 
c  Pressure     0.42819E+00    7109   0.35395E-01   0.20270E+00 
c  k            0.21825E+04    1439   0.73074E-04   0.11497E+01 
c  omega        0.33540E+08     144   0.37647E-04   0.67642E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3835e+05                             1
a  Local Time Step      1.1617e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5571          1.9262     -3.6345e-05     -1.7877e-06
v  Velocity[Y]                 -23.435          29.977          6.7642          20.057
v  Velocity[Z]                 -33.082          28.717       -0.051702       0.0016222
v  ǁVelocityǁ                 0.002157          33.917          10.584          20.216
v  Pressure                    -441.37          347.83         -48.699          31.292
v  k                        7.1392e-07          54.823          4.0639          1.6917
v  omega                         1e-24      3.6885e+07          8509.5          11.911
v  turbulent_viscosity      2.6263e-15          1.2486        0.015935         0.11373
v  CourantNb                   0.03255          2662.5           44.25          1.3762
v  FourierNb                  0.010876           15220          91.581          0.7126
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14761        0.010822        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15291          135.83          2.0888


 TIME FOR THE TIME STEP              633:        0.45421E+02

===============================================================


 INSTANT    0.634000000E+02   TIME STEP NUMBER             634
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.454669473E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29977E+02 0.14214E+02
   Friction velocity        uet   :  0.91324E-03 0.28889E+01
   Friction velocity        uk    :  0.15676E-01 0.30871E+01
   Dimensionless distance   yplus :  0.14117E+00 0.27076E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        473
   Nb of faces within the viscous sub-layer     :       1058
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1859   0.45853E-02   0.39143E+00 
c  VelocityY    0.29414E+04    1859   0.45853E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1859   0.45853E-02   0.00000E+00 
c  Pressure     0.44162E+00    7062   0.32131E-01   0.20925E+00 
c  k            0.21856E+04    1441   0.75263E-04   0.11552E+01 
c  omega        0.13665E+08     230   0.63524E-04   0.49018E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4056e+05                             1
a  Local Time Step      1.0763e-05                         44490


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2425          1.7955     -0.00028755      -4.294e-06
v  Velocity[Y]                 -33.827          29.853          6.6908          20.057
v  Velocity[Z]                 -30.077          28.853      -0.0086563      0.00082476
v  ǁVelocityǁ                 0.010074          33.873          10.593          20.216
v  Pressure                    -420.23          346.15         -49.386          31.264
v  k                        2.5413e-08          69.003          4.1232          1.6896
v  omega                         1e-24      2.2979e+07          8557.5          11.919
v  turbulent_viscosity      6.7329e-14           1.248        0.015965         0.11367
v  CourantNb                  0.021613          2040.7          44.292           1.376
v  FourierNb                  0.010872           15014          92.333         0.71292
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14875        0.010822        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.8681           15092          136.63          2.0889


 TIME FOR THE TIME STEP              634:        0.44890E+02

===============================================================


 INSTANT    0.635000000E+02   TIME STEP NUMBER             635
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.133960775E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31000E+02 0.23527E+02
   Friction velocity        uet   :  0.41871E-02 0.30326E+01
   Friction velocity        uk    :  0.18330E-01 0.30849E+01
   Dimensionless distance   yplus :  0.13157E+00 0.27453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :       1057
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1929   0.45921E-02   0.38018E+00 
c  VelocityY    0.29413E+04    1929   0.45921E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1929   0.45921E-02   0.00000E+00 
c  Pressure     0.42317E+00    7064   0.31880E-01   0.19948E+00 
c  k            0.21823E+04    1369   0.10659E-03   0.10521E+01 
c  omega        0.29828E+12       3   0.31474E-08   0.24369E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5456e+05                             2
a  Local Time Step      1.1218e-05                         44486


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0282          1.5525     -0.00059776     -3.5298e-06
v  Velocity[Y]                 -24.662          29.839          6.6093          20.056
v  Velocity[Z]                 -28.594          28.692        0.027824      0.00026558
v  ǁVelocityǁ                 0.017614          33.553          10.635          20.216
v  Pressure                    -408.91          343.33         -51.427          31.084
v  k                        1.4428e-08          104.71          4.2055          1.6874
v  omega                         1e-24      1.4208e+07            8319          11.891
v  turbulent_viscosity      8.8206e-14          1.2483        0.015976          0.1136
v  CourantNb                  0.037632          2055.3          44.101          1.3759
v  FourierNb                  0.010869           15107          93.236         0.71311
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14856        0.010823        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15147          137.34           2.089


 TIME FOR THE TIME STEP              635:        0.44998E+02

===============================================================


 INSTANT    0.636000000E+02   TIME STEP NUMBER             636
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.351604154E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36093E+02 0.17545E+02
   Friction velocity        uet   :  0.24920E-02 0.29075E+01
   Friction velocity        uk    :  0.11091E-01 0.40765E+01
   Dimensionless distance   yplus :  0.12680E+00 0.36140E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2003   0.47190E-02   0.38732E+00 
c  VelocityY    0.29412E+04    2003   0.47190E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2003   0.47190E-02   0.00000E+00 
c  Pressure     0.43119E+00    7097   0.36457E-01   0.20374E+00 
c  k            0.21739E+04    1395   0.16566E-03   0.10563E+01 
c  omega        0.10315E+08     671   0.36799E-04   0.10802E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6306e+05                             2
a  Local Time Step      1.1137e-05                         44427


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.83364          1.2979     -0.00011856     -1.5565e-06
v  Velocity[Y]                 -33.791          30.106          6.6014          20.056
v  Velocity[Z]                 -28.599          28.735         0.07576     -0.00022006
v  ǁVelocityǁ                 0.012841          34.818           10.66          20.216
v  Pressure                    -409.02          343.24         -54.021          31.278
v  k                        9.5326e-09          108.63          4.2901          1.6853
v  omega                         1e-24      1.1805e+07          8119.4          11.886
v  turbulent_viscosity      8.8279e-15          1.2475        0.015974         0.11349
v  CourantNb                  0.030725          2013.2          44.109          1.3761
v  FourierNb                  0.010865           15363          94.959         0.71333
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010821         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15405          139.07          2.0894


 TIME FOR THE TIME STEP              636:        0.47385E+02

===============================================================


 INSTANT    0.637000000E+02   TIME STEP NUMBER             637
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.699372605E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36049E+02 0.13382E+02
   Friction velocity        uet   :  0.78202E-03 0.32222E+01
   Friction velocity        uk    :  0.25909E-01 0.43135E+01
   Dimensionless distance   yplus :  0.17494E+00 0.38532E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        454
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1939   0.46325E-02   0.39302E+00 
c  VelocityY    0.29411E+04    1939   0.46325E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1939   0.46325E-02   0.00000E+00 
c  Pressure     0.44714E+00    7110   0.39017E-01   0.21222E+00 
c  k            0.21628E+04    1249   0.13669E-03   0.95715E+00 
c  omega        0.10096E+08     339   0.37718E-04   0.87519E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0251e+05                             2
a  Local Time Step      1.1078e-05                         44410


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.84597          1.1009      0.00068569     -7.4248e-07
v  Velocity[Y]                 -20.104          30.679          6.6362          20.057
v  Velocity[Z]                 -29.265          28.847         0.12142     -0.00041677
v  ǁVelocityǁ                0.0097515           33.48          10.658          20.217
v  Pressure                    -407.98          343.77         -56.235          31.575
v  k                        1.4549e-08          50.015          4.2189          1.6831
v  omega                         1e-24      1.1702e+07          7962.3          11.849
v  turbulent_viscosity      4.1274e-14          1.2482        0.015937         0.11338
v  CourantNb                  0.054913          3027.8          44.408          1.3765
v  FourierNb                  0.010863           15301          95.277         0.71278
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889         0.01082        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15349          139.69          2.0892


 TIME FOR THE TIME STEP              637:        0.45697E+02

===============================================================


 INSTANT    0.638000000E+02   TIME STEP NUMBER             638
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.661118083E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30627E+02 0.13933E+02
   Friction velocity        uet   :  0.16196E-02 0.24604E+01
   Friction velocity        uk    :  0.19185E-01 0.31772E+01
   Dimensionless distance   yplus :  0.11563E+00 0.28358E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1927   0.47102E-02   0.40181E+00 
c  VelocityY    0.29411E+04    1927   0.47102E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1927   0.47102E-02   0.00000E+00 
c  Pressure     0.44946E+00    7092   0.36308E-01   0.21253E+00 
c  k            0.21536E+04    1351   0.76618E-04   0.74055E+00 
c  omega        0.10098E+08     322   0.81755E-04   0.22532E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.1722e+05                             3
a  Local Time Step      1.0979e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.84088          1.0021      0.00021083     -3.6837e-06
v  Velocity[Y]                 -17.701          31.046          6.6835          20.056
v  Velocity[Z]                 -28.791          28.985         0.13944     -0.00087113
v  ǁVelocityǁ                 0.017154          33.813          10.626          20.216
v  Pressure                    -405.86          344.66         -56.823          31.581
v  k                        9.1146e-08          51.174          4.1916          1.6809
v  omega                         1e-24      2.4095e+07          8046.7          11.857
v  turbulent_viscosity      6.9653e-15          1.2489        0.015885         0.11326
v  CourantNb                  0.040107          2585.6          44.487          1.3768
v  FourierNb                   0.01086           15418          95.459         0.71179
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1487         0.01082        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15474          139.95          2.0886


 TIME FOR THE TIME STEP              638:        0.45867E+02

===============================================================


 INSTANT    0.639000000E+02   TIME STEP NUMBER             639
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.304350849E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31270E+02 0.14158E+02
   Friction velocity        uet   :  0.15150E-02 0.28414E+01
   Friction velocity        uk    :  0.21068E-01 0.31952E+01
   Dimensionless distance   yplus :  0.10029E+00 0.28201E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :       1059
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1890   0.46911E-02   0.41776E+00 
c  VelocityY    0.29412E+04    1890   0.46911E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1890   0.46911E-02   0.00000E+00 
c  Pressure     0.42806E+00    7095   0.33571E-01   0.20358E+00 
c  k            0.21464E+04    1430   0.74819E-04   0.77079E+00 
c  omega        0.10626E+08     428   0.12966E-03   0.84472E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0407e+05                             2
a  Local Time Step      1.1556e-05                         44341


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79027         0.92433      -0.0015658     -4.4553e-06
v  Velocity[Y]                 -16.187          32.553          6.7289          20.056
v  Velocity[Z]                  -28.56          30.494         0.13007      -0.0012881
v  ǁVelocityǁ                0.0066623          33.545          10.579          20.216
v  Pressure                    -402.14          345.24          -56.21          31.759
v  k                        7.4791e-07          53.849          4.1254          1.6789
v  omega                         1e-24      4.6501e+07          8359.8          11.883
v  turbulent_viscosity      3.1336e-14          1.2518         0.01583         0.11313
v  CourantNb                  0.024602            2043          44.446          1.3771
v  FourierNb                  0.010858           15508          96.673         0.71083
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877         0.01082        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15574          141.12          2.0879


 TIME FOR THE TIME STEP              639:        0.45683E+02

===============================================================


 INSTANT    0.640000000E+02   TIME STEP NUMBER             640
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.187130224E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31516E+02 0.16763E+02
   Friction velocity        uet   :  0.29953E-02 0.28553E+01
   Friction velocity        uk    :  0.34054E-01 0.30948E+01
   Dimensionless distance   yplus :  0.97338E-01 0.30918E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1835   0.44179E-02   0.43513E+00 
c  VelocityY    0.29411E+04    1835   0.44179E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1835   0.44179E-02   0.00000E+00 
c  Pressure     0.42559E+00    7052   0.32173E-01   0.20125E+00 
c  k            0.21385E+04    1446   0.68765E-04   0.77920E+00 
c  omega        0.19917E+08     335   0.48169E-04   0.47790E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6387e+05                             1
a  Local Time Step      1.1657e-05                         44275


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80248         0.85732      -0.0039205     -6.1173e-06
v  Velocity[Y]                 -15.144          32.387          6.7377          20.057
v  Velocity[Z]                 -28.561          29.054         0.09703      -0.0019611
v  ǁVelocityǁ                 0.015777          33.254          10.539          20.217
v  Pressure                     -387.5          344.36         -55.596          31.393
v  k                        2.0694e-07          44.586          4.0325          1.6771
v  omega                         1e-24      2.4588e+07          8339.7          11.866
v  turbulent_viscosity      1.3575e-13          1.2557         0.01576         0.11298
v  CourantNb                  0.027362          2031.6          44.443          1.3773
v  FourierNb                  0.010856           15570          96.795         0.70957
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488         0.01082         0.04571


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15645          141.24          2.0869


 TIME FOR THE TIME STEP              640:        0.45398E+02

===============================================================


 INSTANT    0.641000000E+02   TIME STEP NUMBER             641
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.320814407E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31450E+02 0.21475E+02
   Friction velocity        uet   :  0.19102E-02 0.26902E+01
   Friction velocity        uk    :  0.38898E-01 0.31364E+01
   Dimensionless distance   yplus :  0.14750E+00 0.39420E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1791   0.44927E-02   0.44461E+00 
c  VelocityY    0.29411E+04    1791   0.44927E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1791   0.44927E-02   0.00000E+00 
c  Pressure     0.43188E+00    7047   0.30185E-01   0.20367E+00 
c  k            0.21313E+04    1401   0.57306E-04   0.71945E+00 
c  omega        0.14697E+08     286   0.58792E-04   0.46861E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -3370.4                             1
a  Local Time Step       1.105e-05                         44260


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.78611         0.79341      -0.0062484     -6.6403e-06
v  Velocity[Y]                 -16.195          32.715           6.725          20.057
v  Velocity[Z]                 -28.568          29.052        0.062971      -0.0025999
v  ǁVelocityǁ                 0.021095          32.885          10.513          20.217
v  Pressure                    -368.09          343.67          -54.35          31.111
v  k                        3.3076e-07          42.514           3.971          1.6755
v  omega                         1e-24      3.2154e+07          8438.2          11.878
v  turbulent_viscosity      2.3063e-14          1.2614        0.015702         0.11284
v  CourantNb                  0.017017          2010.1          44.451          1.3777
v  FourierNb                  0.010854           15481          95.355         0.70785
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010819        0.045683


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15563          139.81          2.0855


 TIME FOR THE TIME STEP              641:        0.44153E+02

===============================================================


 INSTANT    0.642000000E+02   TIME STEP NUMBER             642
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.178230092E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31666E+02 0.20675E+02
   Friction velocity        uet   :  0.77797E-03 0.26311E+01
   Friction velocity        uk    :  0.30101E-01 0.32064E+01
   Dimensionless distance   yplus :  0.11469E+00 0.30291E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1810   0.44038E-02   0.45277E+00 
c  VelocityY    0.29410E+04    1810   0.44038E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1810   0.44038E-02   0.00000E+00 
c  Pressure     0.43483E+00    7037   0.27821E-01   0.20580E+00 
c  k            0.21266E+04    1225   0.56405E-04   0.78525E+00 
c  omega        0.57160E+11       5   0.97537E-08   0.30575E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1134e-05                         44269


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.75609         0.70313      -0.0070787     -6.8339e-06
v  Velocity[Y]                 -15.251          30.341          6.7346          20.056
v  Velocity[Z]                 -29.978          28.947        0.033601      -0.0034418
v  ǁVelocityǁ                 0.022268          34.943          10.501          20.217
v  Pressure                    -349.89          346.74         -52.153          31.255
v  k                        7.4545e-09          42.439          3.9312          1.6743
v  omega                         1e-24      1.7966e+07          8238.5           11.88
v  turbulent_viscosity        3.53e-14          1.2668         0.01568         0.11269
v  CourantNb                  0.037335          2026.9          44.709           1.378
v  FourierNb                  0.010854           15410          94.338         0.70646
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14796        0.010819        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98841           15457          139.05          2.0845


 TIME FOR THE TIME STEP              642:        0.43361E+02

===============================================================


 INSTANT    0.643000000E+02   TIME STEP NUMBER             643
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.386918033E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30584E+02 0.20259E+02
   Friction velocity        uet   :  0.17446E-02 0.28839E+01
   Friction velocity        uk    :  0.25762E-01 0.30755E+01
   Dimensionless distance   yplus :  0.11512E+00 0.28648E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :       1004
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    1897   0.44694E-02   0.45047E+00 
c  VelocityY    0.29409E+04    1897   0.44694E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    1897   0.44694E-02   0.00000E+00 
c  Pressure     0.39839E+00    6992   0.29028E-01   0.18833E+00 
c  k            0.21262E+04    1099   0.59574E-04   0.95462E+00 
c  omega        0.68704E+15       2   0.29184E-11   0.27510E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1951e-05                         44356


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.76126         0.59845      -0.0067073     -5.6883e-06
v  Velocity[Y]                  -15.15          30.258          6.7617          20.056
v  Velocity[Z]                  -31.72          29.056       0.0094509      -0.0042519
v  ǁVelocityǁ                 0.015396          36.048          10.517          20.217
v  Pressure                    -355.67          349.48         -50.032          31.602
v  k                        5.3353e-08          49.667          3.9348          1.6734
v  omega                         1e-24      1.2539e+07          8185.1          11.853
v  turbulent_viscosity      2.6945e-14          1.2707         0.01572         0.11256
v  CourantNb                  0.050919            2049          44.847           1.378
v  FourierNb                  0.010855           15564          92.328         0.70551
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14794        0.010818        0.045667


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15619          137.18          2.0835


 TIME FOR THE TIME STEP              643:        0.44057E+02

===============================================================


 INSTANT    0.644000000E+02   TIME STEP NUMBER             644
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.213135195E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31311E+02 0.15290E+02
   Friction velocity        uet   :  0.17257E-02 0.30818E+01
   Friction velocity        uk    :  0.21249E-01 0.29329E+01
   Dimensionless distance   yplus :  0.84851E-01 0.28321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1860   0.45057E-02   0.44964E+00 
c  VelocityY    0.29408E+04    1860   0.45057E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1860   0.45057E-02   0.00000E+00 
c  Pressure     0.42610E+00    7110   0.33136E-01   0.20068E+00 
c  k            0.21329E+04    1502   0.65768E-04   0.11083E+01 
c  omega        0.10485E+08     297   0.80944E-04   0.39469E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1498e-05                         44417


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8939           0.587      -0.0057989     -2.9028e-06
v  Velocity[Y]                 -15.341          31.381          6.8019          20.057
v  Velocity[Z]                 -33.017           28.85       0.0060987      -0.0046863
v  ǁVelocityǁ                0.0068613          36.408          10.565          20.218
v  Pressure                    -409.89          350.66         -48.429          31.813
v  k                        1.1911e-08          59.407          3.9775          1.6731
v  omega                         1e-24      3.9631e+07          8180.3          11.861
v  turbulent_viscosity      2.9198e-14           1.276        0.015784         0.11244
v  CourantNb                  0.019292          2251.2          44.684          1.3778
v  FourierNb                  0.010856           15552          91.027         0.70477
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14857        0.010817        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15617          135.71          2.0825


 TIME FOR THE TIME STEP              644:        0.45398E+02

===============================================================


 INSTANT    0.645000000E+02   TIME STEP NUMBER             645
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.524849760E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31837E+02 0.14099E+02
   Friction velocity        uet   :  0.25035E-02 0.31467E+01
   Friction velocity        uk    :  0.15877E-01 0.29552E+01
   Dimensionless distance   yplus :  0.13624E+00 0.27776E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        483
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1783   0.44567E-02   0.45090E+00 
c  VelocityY    0.29407E+04    1783   0.44567E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1783   0.44567E-02   0.00000E+00 
c  Pressure     0.44524E+00    7126   0.37317E-01   0.20996E+00 
c  k            0.21476E+04    1499   0.67089E-04   0.11595E+01 
c  omega        0.12119E+08     261   0.27907E-03   0.31086E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0784e+05                             1
a  Local Time Step      1.1486e-05                         44428


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0618         0.56899      -0.0045403     -1.1851e-06
v  Velocity[Y]                 -15.763          30.099          6.8451          20.057
v  Velocity[Z]                 -32.176          28.785        0.037731      -0.0046343
v  ǁVelocityǁ                0.0059594          33.975          10.624          20.218
v  Pressure                     -433.4          350.13         -47.769           31.85
v  k                        8.8845e-07          63.891          3.9907          1.6727
v  omega                         1e-24      7.9133e+07          9093.7          11.897
v  turbulent_viscosity      1.2587e-15          1.2825        0.015821         0.11231
v  CourantNb                  0.041792          2755.6          44.568          1.3775
v  FourierNb                  0.010858           15396          90.432         0.70373
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14937        0.010816        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99993           15469             135          2.0812


 TIME FOR THE TIME STEP              645:        0.45427E+02

===============================================================


 INSTANT    0.646000000E+02   TIME STEP NUMBER             646
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.257596351E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31454E+02 0.13909E+02
   Friction velocity        uet   :  0.18302E-02 0.30179E+01
   Friction velocity        uk    :  0.15769E-01 0.31559E+01
   Dimensionless distance   yplus :  0.13246E+00 0.27147E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        939
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1733   0.45459E-02   0.43454E+00 
c  VelocityY    0.29405E+04    1733   0.45459E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1733   0.45459E-02   0.00000E+00 
c  Pressure     0.44998E+00    7112   0.38014E-01   0.21370E+00 
c  k            0.21641E+04    1448   0.70524E-04   0.12027E+01 
c  omega        0.43376E+08     117   0.38172E-04   0.90315E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4478e+05                             3
a  Local Time Step      1.1508e-05                         44435


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1088         0.67149      -0.0026176     -1.2512e-06
v  Velocity[Y]                  -24.15          29.778          6.8471          20.057
v  Velocity[Z]                 -32.007          28.648        0.090417      -0.0050118
v  ǁVelocityǁ                 0.012746           33.49          10.634          20.218
v  Pressure                    -434.08          348.39          -48.04          31.784
v  k                        9.9828e-07          56.629          4.0015          1.6724
v  omega                         1e-24      4.0181e+07            8534          11.864
v  turbulent_viscosity      1.2858e-13          1.2886        0.015865         0.11218
v  CourantNb                  0.049917          2698.7          44.561          1.3774
v  FourierNb                  0.010861           15374          90.923         0.70304
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14892        0.010817        0.045762


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15420          135.48          2.0805


 TIME FOR THE TIME STEP              646:        0.45349E+02

===============================================================


 INSTANT    0.647000000E+02   TIME STEP NUMBER             647
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.215296188E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30702E+02 0.13703E+02
   Friction velocity        uet   :  0.10887E-02 0.28450E+01
   Friction velocity        uk    :  0.43783E-02 0.27694E+01
   Dimensionless distance   yplus :  0.36343E-01 0.27369E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :        939
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1724   0.46297E-02   0.38945E+00 
c  VelocityY    0.29403E+04    1724   0.46297E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1724   0.46297E-02   0.00000E+00 
c  Pressure     0.43870E+00    6998   0.34242E-01   0.20818E+00 
c  k            0.21772E+04    1353   0.73911E-04   0.12556E+01 
c  omega        0.15330E+08     200   0.62312E-04   0.47790E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4735e+05                             2
a  Local Time Step      1.1357e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0534         0.78725     -0.00077093     -1.8626e-06
v  Velocity[Y]                 -30.651          29.615          6.7755          20.056
v  Velocity[Z]                 -31.375          28.677          0.1418      -0.0053126
v  ǁVelocityǁ                0.0098264          32.628          10.619          20.218
v  Pressure                    -417.46          346.79         -48.729          31.756
v  k                        1.0731e-07          54.667          4.0193           1.672
v  omega                         1e-24       2.133e+07          8439.5          11.862
v  turbulent_viscosity      6.3594e-14          1.2942        0.015897         0.11206
v  CourantNb                  0.015567          2070.6          44.478          1.3775
v  FourierNb                  0.010864           15430          91.976         0.70263
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14911        0.010818         0.04577


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15471          136.45          2.0802


 TIME FOR THE TIME STEP              647:        0.44727E+02

===============================================================


 INSTANT    0.648000000E+02   TIME STEP NUMBER             648
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.178148333E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31882E+02 0.21645E+02
   Friction velocity        uet   :  0.11567E-02 0.28716E+01
   Friction velocity        uk    :  0.16170E-01 0.30668E+01
   Dimensionless distance   yplus :  0.93835E-01 0.28133E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :        958
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1769   0.47056E-02   0.35074E+00 
c  VelocityY    0.29403E+04    1769   0.47056E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1769   0.47056E-02   0.00000E+00 
c  Pressure     0.45183E+00    7080   0.30481E-01   0.21405E+00 
c  k            0.21833E+04    1160   0.95702E-04   0.12139E+01 
c  omega        0.11117E+08     269   0.47034E-04   0.33323E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4856e+05                             2
a  Local Time Step       1.129e-05                         44378


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0886         0.88987      0.00018406     -3.2522e-06
v  Velocity[Y]                  -22.73          29.585          6.6763          20.056
v  Velocity[Z]                   -29.5          28.688         0.16239      -0.0052743
v  ǁVelocityǁ                0.0086408          32.853          10.625          20.218
v  Pressure                    -394.77           347.4         -49.814          31.566
v  k                        7.2038e-08           89.38          4.0769          1.6717
v  omega                         1e-24      1.3109e+07            8330          11.879
v  turbulent_viscosity      1.8407e-14          1.2989        0.015909         0.11196
v  CourantNb                   0.02206          2034.4          44.254          1.3775
v  FourierNb                  0.010867           15418          92.876         0.70234
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1493        0.010817        0.045777


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15461          137.13          2.0798


 TIME FOR THE TIME STEP              648:        0.45880E+02

===============================================================


 INSTANT    0.649000000E+02   TIME STEP NUMBER             649
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.192574512E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31191E+02 0.16782E+02
   Friction velocity        uet   :  0.17420E-02 0.25122E+01
   Friction velocity        uk    :  0.17520E-01 0.31917E+01
   Dimensionless distance   yplus :  0.13246E+00 0.30714E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :        955
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1802   0.44699E-02   0.33348E+00 
c  VelocityY    0.29402E+04    1802   0.44699E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1802   0.44699E-02   0.00000E+00 
c  Pressure     0.44188E+00    7098   0.32659E-01   0.20947E+00 
c  k            0.21818E+04    1217   0.11851E-03   0.11051E+01 
c  omega        0.10398E+08     482   0.41796E-04   0.25295E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.676e+05                             2
a  Local Time Step      1.1162e-05                         44292


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2053         0.97865      0.00073726     -4.1057e-06
v  Velocity[Y]                  -37.57          29.926           6.635          20.057
v  Velocity[Z]                 -29.289          28.632         0.18164      -0.0052837
v  ǁVelocityǁ                 0.018141          37.898          10.623          20.218
v  Pressure                    -398.52          348.17         -51.245           31.74
v  k                        1.6668e-08          91.153          4.1239          1.6715
v  omega                         1e-24      1.1784e+07          8255.4          11.894
v  turbulent_viscosity      6.6197e-14          1.3019        0.015911         0.11186
v  CourantNb                  0.028848            2014          44.193          1.3776
v  FourierNb                   0.01087           15440          94.124         0.70231
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14871        0.010817        0.045761


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15490          138.32          2.0799


 TIME FOR THE TIME STEP              649:        0.45622E+02

===============================================================


 INSTANT    0.650000000E+02   TIME STEP NUMBER             650
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.151399827E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43796E+02 0.13923E+02
   Friction velocity        uet   :  0.13987E-02 0.34528E+01
   Friction velocity        uk    :  0.32472E-01 0.35039E+01
   Dimensionless distance   yplus :  0.18997E+00 0.36088E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :        968
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1808   0.45245E-02   0.32426E+00 
c  VelocityY    0.29402E+04    1808   0.45245E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1808   0.45245E-02   0.00000E+00 
c  Pressure     0.42677E+00    7131   0.36615E-01   0.20198E+00 
c  k            0.21773E+04    1379   0.11739E-03   0.10374E+01 
c  omega        0.10172E+08     427   0.81965E-04   0.17538E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9708e+05                             3
a  Local Time Step      1.1424e-05                         44271


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2053          1.0476       0.0014554     -4.7271e-06
v  Velocity[Y]                 -25.363          30.373          6.6321          20.055
v  Velocity[Z]                 -28.573          28.628         0.18422       -0.005062
v  ǁVelocityǁ                 0.020498          33.341          10.599          20.217
v  Pressure                    -401.34          348.27         -52.944          31.806
v  k                        6.5585e-10          43.487          4.1033          1.6713
v  omega                         1e-24      1.3829e+07          8148.7          11.871
v  turbulent_viscosity      3.2488e-14          1.3027        0.015907         0.11176
v  CourantNb                  0.044436          3105.3          44.496          1.3777
v  FourierNb                  0.010872           15533          94.486         0.70214
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14817        0.010817        0.045768


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15592          138.98          2.0799


 TIME FOR THE TIME STEP              650:        0.45892E+02

===============================================================


 INSTANT    0.651000000E+02   TIME STEP NUMBER             651
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.183815546E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31022E+02 0.14050E+02
   Friction velocity        uet   :  0.14121E-02 0.28637E+01
   Friction velocity        uk    :  0.15605E-01 0.30820E+01
   Dimensionless distance   yplus :  0.13739E+00 0.28103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        381
   Nb of faces within the viscous sub-layer     :        994
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1847   0.45623E-02   0.32191E+00 
c  VelocityY    0.29402E+04    1847   0.45623E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1847   0.45623E-02   0.00000E+00 
c  Pressure     0.44034E+00    7117   0.36238E-01   0.20721E+00 
c  k            0.21730E+04    1462   0.70300E-04   0.88176E+00 
c  omega        0.14728E+08     274   0.48909E-04   0.15964E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4784e+05                             3
a  Local Time Step       1.075e-05                         44221


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1053          1.1074       0.0023365     -4.4635e-06
v  Velocity[Y]                 -17.633          32.351           6.656          20.056
v  Velocity[Z]                 -28.524          28.818         0.16477      -0.0050042
v  ǁVelocityǁ                0.0048361          33.433          10.565          20.218
v  Pressure                    -402.77          347.88         -53.858          31.878
v  k                        1.8647e-09          54.686          4.1038          1.6714
v  omega                         1e-24       5.707e+07          8133.8            11.9
v  turbulent_viscosity      7.6074e-16          1.3025        0.015887         0.11168
v  CourantNb                  0.018877          2857.6          44.485          1.3777
v  FourierNb                  0.010874           15649          93.339         0.70127
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14796        0.010817        0.045748


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15716          137.82           2.079


 TIME FOR THE TIME STEP              651:        0.45284E+02

===============================================================


 INSTANT    0.652000000E+02   TIME STEP NUMBER             652
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.634997770E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31321E+02 0.14029E+02
   Friction velocity        uet   :  0.62800E-03 0.29581E+01
   Friction velocity        uk    :  0.22087E-01 0.31302E+01
   Dimensionless distance   yplus :  0.10402E+00 0.27662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :       1007
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1945   0.43254E-02   0.33027E+00 
c  VelocityY    0.29403E+04    1945   0.43254E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1945   0.43254E-02   0.00000E+00 
c  Pressure     0.45483E+00    6986   0.34234E-01   0.21594E+00 
c  k            0.21702E+04    1477   0.69999E-04   0.89734E+00 
c  omega        0.40436E+08     216   0.58855E-04   0.21491E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1399e-05                         44228


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95427          1.1502       0.0026992       -3.62e-06
v  Velocity[Y]                 -16.986           33.71          6.7002          20.056
v  Velocity[Z]                 -28.621          29.051         0.12486      -0.0046856
v  ǁVelocityǁ                  0.01198          33.979          10.534          20.218
v  Pressure                    -401.51          347.08         -53.868          31.855
v  k                        1.1855e-09           49.23          4.0954          1.6715
v  omega                         1e-24      9.7385e+07          8558.4          11.913
v  turbulent_viscosity      2.0015e-15          1.3013        0.015888          0.1116
v  CourantNb                  0.038309          2038.3           44.29          1.3776
v  FourierNb                  0.010875           15654          93.806         0.70088
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14747        0.010817        0.045757


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15728           138.1          2.0785


 TIME FOR THE TIME STEP              652:        0.45312E+02

===============================================================


 INSTANT    0.653000000E+02   TIME STEP NUMBER             653
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.239493272E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30239E+02 0.13957E+02
   Friction velocity        uet   :  0.11396E-02 0.29396E+01
   Friction velocity        uk    :  0.38037E-01 0.31479E+01
   Dimensionless distance   yplus :  0.16533E+00 0.30745E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1890   0.46764E-02   0.34840E+00 
c  VelocityY    0.29402E+04    1890   0.46764E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1890   0.46764E-02   0.00000E+00 
c  Pressure     0.42853E+00    7057   0.31762E-01   0.20136E+00 
c  k            0.21679E+04    1412   0.74847E-04   0.10178E+01 
c  omega        0.40562E+08     311   0.27620E-04   0.81844E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6985e+05                             1
a  Local Time Step      1.0746e-05                         44270


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0129          1.1781       0.0026245     -2.1534e-06
v  Velocity[Y]                 -15.455          33.652          6.7351          20.056
v  Velocity[Z]                  -28.71          28.867        0.072281      -0.0043965
v  ǁVelocityǁ                 0.017197           34.47          10.516          20.217
v  Pressure                    -391.57           345.4         -54.077           31.49
v  k                        2.1707e-08          46.986          4.0359          1.6717
v  omega                         1e-24      4.9271e+07          8519.9          11.937
v  turbulent_viscosity      1.4693e-15          1.3015        0.015895         0.11153
v  CourantNb                  0.040197          2031.3           44.11          1.3775
v  FourierNb                  0.010876           15556          95.218         0.70085
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14876        0.010816        0.045769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15636          139.33          2.0784


 TIME FOR THE TIME STEP              653:        0.45056E+02

===============================================================


 INSTANT    0.654000000E+02   TIME STEP NUMBER             654
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.814449972E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29957E+02 0.15410E+02
   Friction velocity        uet   :  0.97677E-03 0.28309E+01
   Friction velocity        uk    :  0.18532E-01 0.30579E+01
   Dimensionless distance   yplus :  0.98215E-01 0.37264E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1933   0.45178E-02   0.36337E+00 
c  VelocityY    0.29403E+04    1933   0.45178E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1933   0.45178E-02   0.00000E+00 
c  Pressure     0.44825E+00    7045   0.30063E-01   0.21201E+00 
c  k            0.21650E+04    1172   0.69086E-04   0.97459E+00 
c  omega        0.14708E+08     341   0.42475E-04   0.43088E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1135e+05                             1
a  Local Time Step      1.1601e-05                         44323


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1506          1.1939       0.0028016      6.9396e-07
v  Velocity[Y]                  -15.62          33.079          6.7245          20.057
v  Velocity[Z]                 -29.162          29.068       0.0072333      -0.0041646
v  ǁVelocityǁ                0.0058427          33.803          10.504          20.218
v  Pressure                    -374.66          346.37         -53.901          31.252
v  k                        4.6979e-08          37.239          3.9845          1.6721
v  omega                         1e-24      2.5842e+07          8403.5          11.923
v  turbulent_viscosity      2.6942e-14          1.3001        0.015875         0.11147
v  CourantNb                  0.020765          2017.2          44.183          1.3777
v  FourierNb                  0.010877           15490          95.414         0.70038
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14884        0.010816        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15536           139.6           2.078


 TIME FOR THE TIME STEP              654:        0.46062E+02

===============================================================


 INSTANT    0.655000000E+02   TIME STEP NUMBER             655
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.855334532E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30989E+02 0.20346E+02
   Friction velocity        uet   :  0.11878E-02 0.27278E+01
   Friction velocity        uk    :  0.15323E-01 0.30227E+01
   Dimensionless distance   yplus :  0.58105E-01 0.30823E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2051   0.44290E-02   0.37650E+00 
c  VelocityY    0.29403E+04    2051   0.44290E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2051   0.44290E-02   0.00000E+00 
c  Pressure     0.44501E+00    6980   0.27538E-01   0.21084E+00 
c  k            0.21627E+04    1068   0.66458E-04   0.10076E+01 
c  omega        0.10641E+08     233   0.39489E-04   0.48135E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9319e+05                             2
a  Local Time Step      1.1478e-05                         44354


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1952          1.2071       0.0021036     -5.5378e-07
v  Velocity[Y]                 -15.102          31.077          6.7172          20.056
v  Velocity[Z]                 -29.785          28.948       -0.042682      -0.0038437
v  ǁVelocityǁ                  0.01164           34.18          10.498          20.217
v  Pressure                    -360.96          347.49         -53.278           30.92
v  k                        1.8099e-08          39.024            3.96          1.6728
v  omega                         1e-24      1.5297e+07          8436.4          11.912
v  turbulent_viscosity      1.1607e-13          1.2969        0.015853         0.11141
v  CourantNb                   0.03482          2010.6          44.185          1.3779
v  FourierNb                  0.010877           15573           93.88         0.69949
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1486        0.010817        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15628          138.07          2.0774


 TIME FOR THE TIME STEP              655:        0.45409E+02

===============================================================


 INSTANT    0.656000000E+02   TIME STEP NUMBER             656
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.403664139E-20
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31229E+02 0.19961E+02
   Friction velocity        uet   :  0.73300E-03 0.27504E+01
   Friction velocity        uk    :  0.13701E-01 0.32156E+01
   Dimensionless distance   yplus :  0.13556E+00 0.28939E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :       1033
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1945   0.45654E-02   0.38954E+00 
c  VelocityY    0.29402E+04    1945   0.45654E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1945   0.45654E-02   0.00000E+00 
c  Pressure     0.41308E+00    6944   0.27007E-01   0.19523E+00 
c  k            0.21619E+04    1408   0.67069E-04   0.11120E+01 
c  omega        0.10540E+08     242   0.48606E-03   0.63151E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6685e+05                             3
a  Local Time Step      1.1351e-05                         44368


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2535          1.3877       0.0013086      1.2326e-06
v  Velocity[Y]                 -15.319          30.269          6.7297          20.056
v  Velocity[Z]                  -31.23          28.837       -0.098968      -0.0031197
v  ǁVelocityǁ                  0.00855          36.627          10.499          20.217
v  Pressure                    -348.99          349.04         -51.525          31.133
v  k                        1.2023e-09          51.495          3.9799          1.6736
v  omega                         1e-24      1.5027e+08          9538.7          11.953
v  turbulent_viscosity      9.2178e-15          1.2931        0.015862         0.11136
v  CourantNb                  0.040807          2018.4          44.387          1.3779
v  FourierNb                  0.010877           15650          92.847          0.6989
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1493        0.010817        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15716          137.23          2.0768


 TIME FOR THE TIME STEP              656:        0.46058E+02

===============================================================


 INSTANT    0.657000000E+02   TIME STEP NUMBER             657
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.476112774E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31672E+02 0.16552E+02
   Friction velocity        uet   :  0.14896E-02 0.30334E+01
   Friction velocity        uk    :  0.82486E-02 0.30571E+01
   Dimensionless distance   yplus :  0.74073E-01 0.28357E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1060
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1746   0.44902E-02   0.39750E+00 
c  VelocityY    0.29401E+04    1746   0.44902E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1746   0.44902E-02   0.00000E+00 
c  Pressure     0.42199E+00    7020   0.31457E-01   0.19875E+00 
c  k            0.21640E+04    1501   0.71465E-04   0.12560E+01 
c  omega        0.10666E+09     141   0.23822E-04   0.27202E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.726e+05                             2
a  Local Time Step      1.0892e-05                         44378


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4567          1.6764      0.00021498      1.7929e-06
v  Velocity[Y]                 -15.236          32.501          6.7604          20.057
v  Velocity[Z]                 -32.733          28.796        -0.13223      -0.0024341
v  ǁVelocityǁ                 0.013622          36.855          10.544          20.218
v  Pressure                    -401.32          349.11         -50.461          31.299
v  k                        2.3178e-07           62.66          4.0166          1.6745
v  omega                         1e-24      7.5443e+07          8991.8          11.918
v  turbulent_viscosity      1.6523e-15          1.2878        0.015895         0.11132
v  CourantNb                  0.039624          2083.6          44.285          1.3776
v  FourierNb                  0.010878           15624          91.411         0.69843
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14922        0.010816         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15698           135.7           2.076


 TIME FOR THE TIME STEP              657:        0.43798E+02

===============================================================


 INSTANT    0.658000000E+02   TIME STEP NUMBER             658
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.489725681E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32238E+02 0.15219E+02
   Friction velocity        uet   :  0.11516E-02 0.31959E+01
   Friction velocity        uk    :  0.19247E-01 0.32182E+01
   Dimensionless distance   yplus :  0.18266E+00 0.27455E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    1695   0.42744E-02   0.41384E+00 
c  VelocityY    0.29402E+04    1695   0.42744E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    1695   0.42744E-02   0.00000E+00 
c  Pressure     0.44168E+00    7038   0.36729E-01   0.20897E+00 
c  k            0.21710E+04    1510   0.74229E-04   0.13591E+01 
c  omega        0.39319E+08     158   0.67660E-04   0.23657E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -51486                             1
a  Local Time Step      1.1803e-05                         44397


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7133          1.7991      -0.0010097     -6.3703e-07
v  Velocity[Y]                 -15.191          32.347          6.8007          20.057
v  Velocity[Z]                 -32.314          28.841        -0.11627      -0.0016442
v  ǁVelocityǁ                0.0054905          34.573          10.595          20.218
v  Pressure                    -434.32          348.36          -49.67          31.452
v  k                         6.296e-09          67.506          4.0609          1.6754
v  omega                         1e-24      6.5308e+07          9024.2          11.908
v  turbulent_viscosity      3.5866e-14          1.2836        0.015951         0.11128
v  CourantNb                  0.044671          2660.9          44.181          1.3772
v  FourierNb                  0.010879           15636           91.04          0.6986
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14851        0.010817        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92014           15682          135.22          2.0758


 TIME FOR THE TIME STEP              658:        0.43383E+02

===============================================================


 INSTANT    0.659000000E+02   TIME STEP NUMBER             659
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.512858597E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30636E+02 0.16184E+02
   Friction velocity        uet   :  0.13672E-02 0.32085E+01
   Friction velocity        uk    :  0.25087E-01 0.31209E+01
   Dimensionless distance   yplus :  0.21288E+00 0.27762E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :        986
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1775   0.44415E-02   0.41875E+00 
c  VelocityY    0.29403E+04    1775   0.44415E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1775   0.44415E-02   0.00000E+00 
c  Pressure     0.44055E+00    7053   0.38098E-01   0.20831E+00 
c  k            0.21810E+04    1407   0.77995E-04   0.14036E+01 
c  omega        0.31640E+08     247   0.41257E-04   0.76624E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.182e+05                             1
a  Local Time Step      1.1316e-05                         44358


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8693          1.7964      -0.0023002     -1.5196e-06
v  Velocity[Y]                 -22.432           29.96           6.819          20.057
v  Velocity[Z]                 -32.682          28.683       -0.062141     -0.00089021
v  ǁVelocityǁ                0.0079845            34.1          10.619          20.218
v  Pressure                    -442.72          346.84         -49.757          31.443
v  k                        1.1724e-07          62.149          4.0841          1.6762
v  omega                         1e-24      3.3443e+07          8461.6          11.877
v  turbulent_viscosity      1.9342e-16          1.2787         0.01602         0.11125
v  CourantNb                  0.026419            2816          44.152          1.3769
v  FourierNb                   0.01088           15689          91.706         0.69912
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14784        0.010817        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15731          135.86           2.076


 TIME FOR THE TIME STEP              659:        0.43619E+02

===============================================================


 INSTANT    0.660000000E+02   TIME STEP NUMBER             660
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.260438213E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30283E+02 0.15136E+02
   Friction velocity        uet   :  0.41485E-03 0.28923E+01
   Friction velocity        uk    :  0.20055E-01 0.30277E+01
   Dimensionless distance   yplus :  0.19813E+00 0.28123E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        419
   Nb of faces within the viscous sub-layer     :        973
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1810   0.46232E-02   0.39441E+00 
c  VelocityY    0.29403E+04    1810   0.46232E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1810   0.46232E-02   0.00000E+00 
c  Pressure     0.41761E+00    7012   0.35447E-01   0.19746E+00 
c  k            0.21895E+04    1148   0.80835E-04   0.14409E+01 
c  omega        0.14285E+08     195   0.53835E-04   0.42319E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -46650                             1
a  Local Time Step      1.1557e-05                         44418


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.919          1.4647      -0.0019721     -4.8869e-07
v  Velocity[Y]                 -25.043          29.803          6.7791          20.057
v  Velocity[Z]                 -32.369          28.965       0.0023818     -0.00011159
v  ǁVelocityǁ                0.0022133          33.018          10.613          20.218
v  Pressure                    -431.01          348.26         -50.195          31.484
v  k                        3.2858e-08          48.492          4.0979          1.6768
v  omega                         1e-24      1.8296e+07          8336.4          11.885
v  turbulent_viscosity      2.5567e-14           1.272        0.016075         0.11123
v  CourantNb                  0.051955          2390.2          44.128          1.3768
v  FourierNb                   0.01088           15589          92.371         0.69944
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14885        0.010819        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15633           136.5          2.0763


 TIME FOR THE TIME STEP              660:        0.44086E+02

===============================================================


 INSTANT    0.661000000E+02   TIME STEP NUMBER             661
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.388722362E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31313E+02 0.16140E+02
   Friction velocity        uet   :  0.16033E-02 0.27821E+01
   Friction velocity        uk    :  0.20699E-01 0.28434E+01
   Dimensionless distance   yplus :  0.13448E+00 0.28391E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1832   0.46697E-02   0.37647E+00 
c  VelocityY    0.29404E+04    1832   0.46697E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1832   0.46697E-02   0.00000E+00 
c  Pressure     0.43752E+00    6832   0.31713E-01   0.20716E+00 
c  k            0.21925E+04    1124   0.92597E-04   0.14115E+01 
c  omega        0.11360E+08     245   0.46626E-04   0.34989E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6036e+05                             1
a  Local Time Step      1.1447e-05                         44458


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7473          1.3096     -0.00064846     -1.6605e-06
v  Velocity[Y]                 -35.619          29.675          6.6825          20.057
v  Velocity[Z]                 -28.453          28.688        0.050517      0.00045186
v  ǁVelocityǁ                0.0079421          35.836          10.629          20.217
v  Pressure                    -404.62          349.29         -51.162          31.466
v  k                        2.9173e-07          83.568          4.1396          1.6772
v  omega                         1e-24      1.1988e+07          8271.2          11.904
v  turbulent_viscosity      7.1672e-15           1.268        0.016087         0.11121
v  CourantNb                  0.050516          2063.9          44.116          1.3768
v  FourierNb                   0.01088           15498          93.423         0.69969
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010818        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15548          137.54          2.0765


 TIME FOR THE TIME STEP              661:        0.44791E+02

===============================================================


 INSTANT    0.662000000E+02   TIME STEP NUMBER             662
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.413594442E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30730E+02 0.24726E+02
   Friction velocity        uet   :  0.28503E-03 0.31054E+01
   Friction velocity        uk    :  0.99730E-02 0.29837E+01
   Dimensionless distance   yplus :  0.13813E+00 0.30429E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        461
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1904   0.46425E-02   0.36852E+00 
c  VelocityY    0.29405E+04    1904   0.46425E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1904   0.46425E-02   0.00000E+00 
c  Pressure     0.42996E+00    7002   0.33203E-01   0.20384E+00 
c  k            0.21878E+04    1365   0.13074E-03   0.12839E+01 
c  omega        0.10607E+08     443   0.36205E-04   0.38854E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -78978                             1
a  Local Time Step      1.1168e-05                         44457


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4789          1.2476      0.00034153     -1.7063e-06
v  Velocity[Y]                 -39.429          29.918           6.627          20.056
v  Velocity[Z]                 -28.481          28.945        0.085032        0.001156
v  ǁVelocityǁ                 0.015177          41.071          10.642          20.217
v  Pressure                    -407.78          349.13         -53.009          31.479
v  k                        2.8557e-08          108.14          4.1836          1.6775
v  omega                         1e-24      1.3931e+07          8116.8          11.893
v  turbulent_viscosity      5.2569e-14          1.2629        0.016067         0.11119
v  CourantNb                  0.043764          2069.5          44.217          1.3768
v  FourierNb                  0.010879           15456          94.689         0.70028
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14799        0.010818        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15514          138.91          2.0771


 TIME FOR THE TIME STEP              662:        0.48089E+02

===============================================================


 INSTANT    0.663000000E+02   TIME STEP NUMBER             663
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.647661492E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.55862E+02 0.14051E+02
   Friction velocity        uet   :  0.21814E-02 0.36162E+01
   Friction velocity        uk    :  0.25831E-01 0.48373E+01
   Dimensionless distance   yplus :  0.10605E+00 0.40214E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        371
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1827   0.48133E-02   0.36468E+00 
c  VelocityY    0.29404E+04    1827   0.48133E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1827   0.48133E-02   0.00000E+00 
c  Pressure     0.45875E+00    7038   0.37521E-01   0.21654E+00 
c  k            0.21793E+04    1452   0.13640E-03   0.11521E+01 
c  omega        0.11217E+08     488   0.72387E-04   0.26957E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8262e+05                             2
a  Local Time Step      1.1126e-05                         44425


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2165          1.0002     -9.8277e-05     -1.2069e-06
v  Velocity[Y]                 -30.185          30.381          6.6343          20.056
v  Velocity[Z]                 -28.498          28.863         0.11342       0.0017652
v  ǁVelocityǁ                 0.011157          33.409          10.638          20.217
v  Pressure                    -408.13          348.37         -55.144          31.599
v  k                        2.8022e-09          58.241          4.1579          1.6779
v  omega                         1e-24      1.7742e+07          8109.8          11.887
v  turbulent_viscosity      2.4451e-14           1.256        0.016022         0.11119
v  CourantNb                  0.040596          2131.7            44.4           1.377
v  FourierNb                  0.010878           15489            94.4         0.70008
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14749        0.010817          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94539           15555           138.8          2.0771


 TIME FOR THE TIME STEP              663:        0.47353E+02

===============================================================


 INSTANT    0.664000000E+02   TIME STEP NUMBER             664
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.175731808E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31491E+02 0.14007E+02
   Friction velocity        uet   :  0.22084E-02 0.29223E+01
   Friction velocity        uk    :  0.23329E-01 0.32863E+01
   Dimensionless distance   yplus :  0.84039E-01 0.27773E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        394
   Nb of faces within the viscous sub-layer     :       1001
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1813   0.45955E-02   0.36503E+00 
c  VelocityY    0.29404E+04    1813   0.45955E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1813   0.45955E-02   0.00000E+00 
c  Pressure     0.46768E+00    7052   0.38223E-01   0.22147E+00 
c  k            0.21709E+04    1461   0.78249E-04   0.10110E+01 
c  omega        0.17267E+08     306   0.13625E-03   0.21775E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2454e+05                             3
a  Local Time Step      1.1492e-05                         44377


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0649          1.0308        -0.00123       1.695e-06
v  Velocity[Y]                 -17.758          30.598          6.6636          20.057
v  Velocity[Z]                 -28.565          29.049         0.12007       0.0024871
v  ǁVelocityǁ                   0.0128          33.319          10.604          20.218
v  Pressure                    -408.44          347.07          -56.56          31.917
v  k                        5.2042e-10          50.035          4.1368          1.6782
v  omega                         1e-24      5.8067e+07          9079.8          11.929
v  turbulent_viscosity      4.6736e-15          1.2494        0.015972         0.11118
v  CourantNb                  0.017436          2978.8          44.645          1.3771
v  FourierNb                  0.010877           15506          93.491          0.6991
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14809        0.010818        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99143           15578          138.14          2.0762


 TIME FOR THE TIME STEP              664:        0.46829E+02

===============================================================


 INSTANT    0.665000000E+02   TIME STEP NUMBER             665
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.103235118E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31912E+02 0.13794E+02
   Friction velocity        uet   :  0.11011E-02 0.27655E+01
   Friction velocity        uk    :  0.14060E-01 0.28124E+01
   Dimensionless distance   yplus :  0.11542E+00 0.28111E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        394
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    2002   0.44063E-02   0.37947E+00 
c  VelocityY    0.29404E+04    2002   0.44063E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    2002   0.44063E-02   0.00000E+00 
c  Pressure     0.45560E+00    7018   0.34742E-01   0.21683E+00 
c  k            0.21642E+04    1408   0.71530E-04   0.94640E+00 
c  omega        0.25686E+08     306   0.95165E-04   0.20858E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1105e+05                             1
a  Local Time Step      1.1069e-05                         44349


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.96498          1.0351      -0.0017798      9.2561e-07
v  Velocity[Y]                 -17.254          32.048          6.7042          20.057
v  Velocity[Z]                 -28.902          28.941          0.1036       0.0027305
v  ǁVelocityǁ                 0.016924          33.685          10.563          20.217
v  Pressure                    -407.96          346.72         -56.658          31.717
v  k                         1.974e-08          55.839          4.1345          1.6786
v  omega                         1e-24       1.019e+08          8905.6          11.927
v  turbulent_viscosity      2.2539e-16          1.2467        0.015944         0.11119
v  CourantNb                  0.029616          2066.8          44.511          1.3771
v  FourierNb                  0.010877           15380          94.033         0.69868
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14856        0.010818        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15457          138.54          2.0758


 TIME FOR THE TIME STEP              665:        0.46189E+02

===============================================================


 INSTANT    0.666000000E+02   TIME STEP NUMBER             666
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.675143228E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30359E+02 0.14959E+02
   Friction velocity        uet   :  0.91207E-03 0.28542E+01
   Friction velocity        uk    :  0.28199E-01 0.29479E+01
   Dimensionless distance   yplus :  0.12689E+00 0.30895E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1850   0.44856E-02   0.40114E+00 
c  VelocityY    0.29404E+04    1850   0.44856E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1850   0.44856E-02   0.00000E+00 
c  Pressure     0.42389E+00    6762   0.31285E-01   0.20219E+00 
c  k            0.21590E+04    1216   0.70553E-04   0.10351E+01 
c  omega        0.44264E+08     344   0.26994E-04   0.62376E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4132e+05                             2
a  Local Time Step      1.1175e-05                         44372


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94215          1.0064      -0.0012298      1.1063e-06
v  Velocity[Y]                 -15.335          32.683          6.7361          20.056
v  Velocity[Z]                 -29.512          28.876        0.069295       0.0031454
v  ǁVelocityǁ                0.0084869          33.724          10.519          20.216
v  Pressure                    -401.79          347.93         -56.328          31.673
v  k                        4.0254e-08          51.668          4.0818          1.6788
v  omega                         1e-24      5.1564e+07          8511.7          11.907
v  turbulent_viscosity      2.6679e-14          1.2462        0.015935         0.11119
v  CourantNb                  0.041048          2007.8          44.388          1.3771
v  FourierNb                  0.010877           15337          95.832         0.69897
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010818        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15382          140.22          2.0761


 TIME FOR THE TIME STEP              666:        0.43350E+02

===============================================================


 INSTANT    0.667000000E+02   TIME STEP NUMBER             667
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.871355118E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30903E+02 0.15345E+02
   Friction velocity        uet   :  0.29798E-02 0.27943E+01
   Friction velocity        uk    :  0.20858E-01 0.31326E+01
   Dimensionless distance   yplus :  0.11705E+00 0.34983E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        461
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1827   0.44243E-02   0.41821E+00 
c  VelocityY    0.29404E+04    1827   0.44243E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1827   0.44243E-02   0.00000E+00 
c  Pressure     0.42828E+00    6992   0.31155E-01   0.20336E+00 
c  k            0.21531E+04    1263   0.65416E-04   0.97876E+00 
c  omega        0.16689E+08     299   0.15044E-03   0.34954E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0426e-05                         44403


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2422         0.95716     -7.6463e-05      1.7537e-06
v  Velocity[Y]                 -15.132          32.958          6.7193          20.056
v  Velocity[Z]                 -29.162          28.787        0.025094       0.0037087
v  ǁVelocityǁ                 0.023274          33.423          10.498          20.216
v  Pressure                    -382.47          348.24         -56.246          31.136
v  k                        1.7421e-07          41.719          4.0306          1.6791
v  omega                         1e-24      1.2487e+08          8787.5          11.923
v  turbulent_viscosity      2.1205e-14          1.2463        0.015924          0.1112
v  CourantNb                   0.02788          2019.3          44.295          1.3771
v  FourierNb                  0.010876           15437          95.806         0.69902
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14858        0.010817        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15490           140.1          2.0761


 TIME FOR THE TIME STEP              667:        0.44373E+02

===============================================================


 INSTANT    0.668000000E+02   TIME STEP NUMBER             668
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.596200419E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30948E+02 0.22344E+02
   Friction velocity        uet   :  0.73607E-03 0.27285E+01
   Friction velocity        uk    :  0.14597E-01 0.32098E+01
   Dimensionless distance   yplus :  0.11630E+00 0.37529E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        485
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1783   0.44616E-02   0.43334E+00 
c  VelocityY    0.29404E+04    1783   0.44616E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1783   0.44616E-02   0.00000E+00 
c  Pressure     0.38953E+00    6978   0.30109E-01   0.18447E+00 
c  k            0.21492E+04    1475   0.60191E-04   0.96566E+00 
c  omega        0.94130E+08     131   0.13452E-04   0.11254E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1235e-05                         44410


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5075         0.89587       0.0011122      2.4133e-06
v  Velocity[Y]                 -15.704          31.693          6.7079          20.056
v  Velocity[Z]                 -28.954          28.852       -0.010756       0.0040279
v  ǁVelocityǁ                0.0097544          33.072          10.491          20.216
v  Pressure                    -368.45          348.76         -55.378          30.885
v  k                        8.1803e-08           42.45          3.9947          1.6794
v  omega                         1e-24      6.2481e+07          8601.6          11.898
v  turbulent_viscosity      2.4023e-14          1.2467         0.01591         0.11121
v  CourantNb                  0.044276          2039.6          44.145          1.3773
v  FourierNb                  0.010876           15471          94.815         0.69848
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.148        0.010817        0.045681


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15535          138.96          2.0758


 TIME FOR THE TIME STEP              668:        0.44040E+02

===============================================================


 INSTANT    0.669000000E+02   TIME STEP NUMBER             669
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.568645974E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30707E+02 0.21195E+02
   Friction velocity        uet   :  0.11685E-02 0.26730E+01
   Friction velocity        uk    :  0.10658E-01 0.31972E+01
   Dimensionless distance   yplus :  0.95881E-01 0.30628E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        506
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1699   0.45877E-02   0.44468E+00 
c  VelocityY    0.29404E+04    1699   0.45877E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1699   0.45877E-02   0.00000E+00 
c  Pressure     0.43333E+00    6988   0.28530E-01   0.20501E+00 
c  k            0.21477E+04    1536   0.60535E-04   0.10499E+01 
c  omega        0.25991E+08     180   0.23996E-04   0.32715E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7596e+05                             1
a  Local Time Step      1.1312e-05                         44442


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7785         0.83327       0.0017205      4.4716e-06
v  Velocity[Y]                 -15.198          30.434          6.7188          20.055
v  Velocity[Z]                 -31.771          28.722       -0.047275       0.0040062
v  ǁVelocityǁ                 0.018727          36.452          10.499          20.215
v  Pressure                    -351.36          349.84         -53.448          31.097
v  k                        9.5915e-09          44.763          3.9841          1.6797
v  omega                         1e-24      3.1376e+07          8210.6          11.842
v  turbulent_viscosity      7.9253e-14          1.2465        0.015902         0.11122
v  CourantNb                  0.036183          2049.2          44.326          1.3774
v  FourierNb                  0.010876           15277          93.648         0.69792
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010817        0.045662


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15351          137.97          2.0753


 TIME FOR THE TIME STEP              669:        0.43249E+02

===============================================================


 INSTANT    0.670000000E+02   TIME STEP NUMBER             670
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.114224577E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31623E+02 0.17831E+02
   Friction velocity        uet   :  0.80840E-03 0.30655E+01
   Friction velocity        uk    :  0.13159E-01 0.28910E+01
   Dimensionless distance   yplus :  0.11222E+00 0.27417E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1598   0.45080E-02   0.44472E+00 
c  VelocityY    0.29404E+04    1598   0.45080E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1598   0.45080E-02   0.00000E+00 
c  Pressure     0.42995E+00    7060   0.31431E-01   0.20348E+00 
c  k            0.21498E+04    1500   0.64463E-04   0.11795E+01 
c  omega        0.12013E+08     244   0.31003E-04   0.12361E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74894                             1
a  Local Time Step      1.1531e-05                         44450


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9088         0.77118       0.0018591      4.1615e-06
v  Velocity[Y]                 -15.164          30.334          6.7475          20.055
v  Velocity[Z]                 -31.575          28.992       -0.071569       0.0037267
v  ǁVelocityǁ                0.0068008          36.553          10.543          20.215
v  Pressure                    -391.31          349.97         -51.582           31.47
v  k                        1.9269e-08          56.716          4.0022          1.6802
v  omega                         1e-24      1.5974e+07          8054.4          11.831
v  turbulent_viscosity      1.7282e-14          1.2461        0.015921         0.11124
v  CourantNb                  0.032698            2047          44.332          1.3771
v  FourierNb                  0.010876           15224          91.995         0.69736
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14921        0.010817        0.045657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15273          136.33          2.0745


 TIME FOR THE TIME STEP              670:        0.43155E+02

===============================================================


 INSTANT    0.671000000E+02   TIME STEP NUMBER             671
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.519253349E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32239E+02 0.14182E+02
   Friction velocity        uet   :  0.14698E-02 0.30983E+01
   Friction velocity        uk    :  0.16994E-01 0.31018E+01
   Dimensionless distance   yplus :  0.14351E+00 0.27649E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1666   0.45715E-02   0.44551E+00 
c  VelocityY    0.29405E+04    1666   0.45715E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1666   0.45715E-02   0.00000E+00 
c  Pressure     0.42020E+00    7130   0.35847E-01   0.19888E+00 
c  k            0.21579E+04    1386   0.68098E-04   0.12830E+01 
c  omega        0.10291E+08     214   0.55219E-04   0.55929E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6333e+05                             1
a  Local Time Step      1.1033e-05                         44452


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9731          0.9094       0.0018371      2.7411e-06
v  Velocity[Y]                 -15.252          31.946          6.7899          20.056
v  Velocity[Z]                 -33.208           28.77       -0.057425       0.0032084
v  ǁVelocityǁ                 0.011438          35.473          10.613          20.215
v  Pressure                    -429.86           349.4           -50.1          31.807
v  k                        9.7254e-08          64.517          4.0367          1.6806
v  omega                         1e-24      4.1199e+07          8013.4           11.82
v  turbulent_viscosity      3.5744e-14           1.247        0.015962         0.11126
v  CourantNb                  0.018769          2466.1          44.246          1.3767
v  FourierNb                  0.010875           15263          91.461         0.69703
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010816         0.04564


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99934           15308          135.71          2.0737


 TIME FOR THE TIME STEP              671:        0.43422E+02

===============================================================


 INSTANT    0.672000000E+02   TIME STEP NUMBER             672
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.120277851E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30474E+02 0.13817E+02
   Friction velocity        uet   :  0.12036E-02 0.31608E+01
   Friction velocity        uk    :  0.22685E-01 0.31871E+01
   Dimensionless distance   yplus :  0.14118E+00 0.28292E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1788   0.46924E-02   0.44650E+00 
c  VelocityY    0.29405E+04    1788   0.46924E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1788   0.46924E-02   0.00000E+00 
c  Pressure     0.43449E+00    7104   0.37714E-01   0.20443E+00 
c  k            0.21711E+04    1161   0.69987E-04   0.13235E+01 
c  omega        0.17867E+08     189   0.15201E-03   0.19649E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -94460                             2
a  Local Time Step      1.1677e-05                         44461


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0209         0.97179       0.0012118      6.8895e-08
v  Velocity[Y]                 -20.491          30.098           6.822          20.057
v  Velocity[Z]                 -33.397          28.883      -0.0095836       0.0027979
v  ǁVelocityǁ                0.0091664           34.67          10.655          20.216
v  Pressure                    -443.51          350.39          -49.52          31.894
v  k                        5.3594e-07          62.442          4.0643          1.6809
v  omega                         1e-24       7.209e+07          8557.1           11.87
v  turbulent_viscosity      1.0273e-13          1.2486        0.016019         0.11128
v  CourantNb                  0.013254          2766.7          44.231          1.3764
v  FourierNb                  0.010875           15238          92.226         0.69729
v  total_pressure           1.0088e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010817        0.045661


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15284          136.46          2.0737


 TIME FOR THE TIME STEP              672:        0.43536E+02

===============================================================


 INSTANT    0.673000000E+02   TIME STEP NUMBER             673
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.145787853E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30712E+02 0.13909E+02
   Friction velocity        uet   :  0.25560E-02 0.29573E+01
   Friction velocity        uk    :  0.93336E-02 0.27658E+01
   Dimensionless distance   yplus :  0.83943E-01 0.28190E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1884   0.45168E-02   0.41373E+00 
c  VelocityY    0.29405E+04    1884   0.45168E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1884   0.45168E-02   0.00000E+00 
c  Pressure     0.44738E+00    7022   0.36178E-01   0.21207E+00 
c  k            0.21846E+04    1195   0.71228E-04   0.13528E+01 
c  omega        0.24784E+21       2   0.17886E-16   0.74125E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5154e+05                             2
a  Local Time Step      1.1537e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0327         0.98086     -0.00024452     -8.7706e-07
v  Velocity[Y]                  -22.91          29.939          6.7952          20.057
v  Velocity[Z]                 -33.492          28.601        0.061044       0.0024276
v  ǁVelocityǁ                0.0088424          34.291          10.636          20.215
v  Pressure                    -435.85          351.12         -49.481          31.922
v  k                        1.3969e-07          51.393          4.0681           1.681
v  omega                         1e-24      3.6782e+07          8319.3          11.855
v  turbulent_viscosity      1.1049e-13          1.2573        0.016048          0.1113
v  CourantNb                   0.01816          2524.8          44.301          1.3763
v  FourierNb                  0.010875           15167          93.141         0.69732
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010817        0.045676


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15219          137.44          2.0736


 TIME FOR THE TIME STEP              673:        0.43972E+02

===============================================================


 INSTANT    0.674000000E+02   TIME STEP NUMBER             674
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.632192553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31044E+02 0.14303E+02
   Friction velocity        uet   :  0.54480E-03 0.29253E+01
   Friction velocity        uk    :  0.27808E-01 0.28130E+01
   Dimensionless distance   yplus :  0.64978E-01 0.27978E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        394
   Nb of faces within the viscous sub-layer     :        975
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1858   0.43703E-02   0.37669E+00 
c  VelocityY    0.29405E+04    1858   0.43703E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1858   0.43703E-02   0.00000E+00 
c  Pressure     0.43710E+00    7020   0.31963E-01   0.20669E+00 
c  k            0.21940E+04    1433   0.82284E-04   0.14254E+01 
c  omega        0.13227E+08     301   0.60234E-04   0.47093E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5907e+05                             2
a  Local Time Step      1.1361e-05                         44421


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0299          1.0494       -0.001521     -2.7443e-06
v  Velocity[Y]                 -33.927          29.741          6.7049          20.056
v  Velocity[Z]                  -29.27          28.525         0.10397       0.0017861
v  ǁVelocityǁ                 0.012324          34.045          10.612          20.214
v  Pressure                    -413.27          350.79         -49.948          31.647
v  k                        2.9168e-09          70.608          4.0775          1.6807
v  omega                         1e-24      1.9834e+07          8255.6          11.882
v  turbulent_viscosity      2.2065e-14          1.2658        0.016033          0.1113
v  CourantNb                  0.025768          2006.6          44.221          1.3762
v  FourierNb                  0.010874           15056          93.661           0.697
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010818        0.045699


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15116          137.88          2.0732


 TIME FOR THE TIME STEP              674:        0.44838E+02

===============================================================


 INSTANT    0.675000000E+02   TIME STEP NUMBER             675
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.444198036E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31154E+02 0.23138E+02
   Friction velocity        uet   :  0.26637E-02 0.29733E+01
   Friction velocity        uk    :  0.29537E-01 0.28911E+01
   Dimensionless distance   yplus :  0.14519E+00 0.27354E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        385
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1884   0.45490E-02   0.35560E+00 
c  VelocityY    0.29406E+04    1884   0.45490E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1884   0.45490E-02   0.00000E+00 
c  Pressure     0.41882E+00    7002   0.31482E-01   0.19881E+00 
c  k            0.21955E+04    1439   0.97522E-04   0.12133E+01 
c  omega        0.10622E+08     378   0.50987E-04   0.29064E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0965e+05                             2
a  Local Time Step      1.1278e-05                         44371


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0013           1.101      -0.0026273     -3.4487e-06
v  Velocity[Y]                 -25.181          29.836          6.6267          20.055
v  Velocity[Z]                 -28.705          28.515         0.12821      0.00085341
v  ǁVelocityǁ                 0.010009          34.196          10.605          20.214
v  Pressure                    -406.38          349.57         -50.996          31.659
v  k                        6.2483e-07          92.176          4.0996          1.6805
v  omega                         1e-24      1.2584e+07            8110          11.894
v  turbulent_viscosity       5.255e-16           1.278        0.015995         0.11132
v  CourantNb                  0.025298          2001.4          44.178          1.3762
v  FourierNb                  0.010874           14927          94.284         0.69724
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1479        0.010819        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14995          138.46          2.0734


 TIME FOR THE TIME STEP              675:        0.45431E+02

===============================================================


 INSTANT    0.676000000E+02   TIME STEP NUMBER             676
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.511584665E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49176E+02 0.14174E+02
   Friction velocity        uet   :  0.29876E-02 0.29451E+01
   Friction velocity        uk    :  0.24884E-01 0.41571E+01
   Dimensionless distance   yplus :  0.87265E-01 0.31772E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        355
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1865   0.45779E-02   0.34179E+00 
c  VelocityY    0.29408E+04    1865   0.45779E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1865   0.45779E-02   0.00000E+00 
c  Pressure     0.45645E+00    7014   0.35546E-01   0.21609E+00 
c  k            0.21915E+04    1404   0.10400E-03   0.10350E+01 
c  omega        0.10074E+08     501   0.34117E-04   0.22779E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6313e+05                             1
a  Local Time Step      1.1074e-05                         44346


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.982          1.1345      -0.0041546     -3.0601e-06
v  Velocity[Y]                 -35.148          30.084           6.611          20.056
v  Velocity[Z]                 -28.751          28.548         0.13947      0.00016328
v  ǁVelocityǁ                0.0097458          36.236          10.588          20.214
v  Pressure                       -408          347.92         -52.322          32.002
v  k                         6.475e-09          65.068          4.0929          1.6803
v  omega                         1e-24      1.1744e+07            7985          11.896
v  turbulent_viscosity      1.1808e-13          1.2925        0.015956         0.11135
v  CourantNb                   0.05849          2002.8          44.265          1.3762
v  FourierNb                  0.010873           14897          94.257         0.69727
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14856        0.010818        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14970          138.52          2.0735


 TIME FOR THE TIME STEP              676:        0.45270E+02

===============================================================


 INSTANT    0.677000000E+02   TIME STEP NUMBER             677
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.106507445E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37052E+02 0.14460E+02
   Friction velocity        uet   :  0.20127E-02 0.33798E+01
   Friction velocity        uk    :  0.10259E-01 0.31972E+01
   Dimensionless distance   yplus :  0.36327E-01 0.29373E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1833   0.46512E-02   0.32548E+00 
c  VelocityY    0.29410E+04    1833   0.46512E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1833   0.46512E-02   0.00000E+00 
c  Pressure     0.41476E+00    7043   0.37768E-01   0.19595E+00 
c  k            0.21870E+04    1341   0.77522E-04   0.92311E+00 
c  omega        0.10021E+08     382   0.97441E-04   0.33547E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5843e+05                             4
a  Local Time Step      1.1502e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9299          1.0529      -0.0063506     -4.0819e-06
v  Velocity[Y]                  -19.07          30.723          6.6283          20.056
v  Velocity[Z]                 -28.964          28.402         0.13043     -0.00057619
v  ǁVelocityǁ                0.0056067          33.455          10.554          20.215
v  Pressure                    -408.67          346.68         -53.477          32.187
v  k                        2.5234e-08          48.531          4.0745          1.6801
v  omega                         1e-24      2.4434e+07          8073.8          11.871
v  turbulent_viscosity      2.7783e-15          1.3059        0.015924         0.11138
v  CourantNb                 0.0089349          3137.2          44.676          1.3763
v  FourierNb                  0.010872           14849          92.992         0.69661
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1482        0.010819        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14926          137.67          2.0729


 TIME FOR THE TIME STEP              677:        0.44638E+02

===============================================================


 INSTANT    0.678000000E+02   TIME STEP NUMBER             678
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.563192124E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31363E+02 0.13409E+02
   Friction velocity        uet   :  0.15346E-02 0.28180E+01
   Friction velocity        uk    :  0.23120E-01 0.27500E+01
   Dimensionless distance   yplus :  0.20821E+00 0.28852E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1887   0.46067E-02   0.32333E+00 
c  VelocityY    0.29411E+04    1887   0.46067E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1887   0.46067E-02   0.00000E+00 
c  Pressure     0.46676E+00    7019   0.35120E-01   0.21999E+00 
c  k            0.21837E+04    1178   0.64770E-04   0.81246E+00 
c  omega        0.16282E+08     231   0.17016E-03   0.26852E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2586e+05                             2
a  Local Time Step      1.1479e-05                         44322


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6487         0.93365      -0.0086527     -5.1109e-06
v  Velocity[Y]                  -17.52          32.864           6.656          20.056
v  Velocity[Z]                  -29.44          28.788        0.093773      -0.0016171
v  ǁVelocityǁ                 0.019249          33.898          10.513          20.215
v  Pressure                    -407.85          347.21         -53.871          32.239
v  k                         2.529e-10          52.811          4.0918            1.68
v  omega                         1e-24        6.16e+07          8998.9          11.904
v  turbulent_viscosity      1.6231e-14          1.3147        0.015917         0.11142
v  CourantNb                  0.052353            2438          44.607          1.3762
v  FourierNb                  0.010871           14916           92.84         0.69647
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14794         0.01082        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14959          137.45          2.0726


 TIME FOR THE TIME STEP              678:        0.44514E+02

===============================================================


 INSTANT    0.679000000E+02   TIME STEP NUMBER             679
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.219703340E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30578E+02 0.13678E+02
   Friction velocity        uet   :  0.13199E-02 0.29488E+01
   Friction velocity        uk    :  0.19412E-01 0.30072E+01
   Dimensionless distance   yplus :  0.82377E-01 0.29035E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        574
   Nb of faces within the viscous sub-layer     :       1047
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1972   0.44742E-02   0.32389E+00 
c  VelocityY    0.29413E+04    1972   0.44742E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1972   0.44742E-02   0.00000E+00 
c  Pressure     0.47851E+00    7045   0.33618E-01   0.22771E+00 
c  k            0.21822E+04    1205   0.68072E-04   0.88558E+00 
c  omega        0.16203E+18       2   0.25898E-13   0.79166E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9416e+05                             2
a  Local Time Step      1.1502e-05                         44303


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4962         0.79743       -0.010085     -2.9893e-06
v  Velocity[Y]                 -16.121          33.718          6.6873          20.057
v  Velocity[Z]                 -28.975          28.909        0.041131      -0.0030682
v  ǁVelocityǁ                 0.023353          34.154          10.474          20.215
v  Pressure                     -403.7          347.12         -54.145          31.866
v  k                        9.0617e-10          51.841          4.0797          1.6799
v  omega                         1e-24      3.1775e+07          8376.9          11.865
v  turbulent_viscosity      2.4511e-16          1.3229        0.015944         0.11146
v  CourantNb                  0.037282          2056.6          44.275           1.376
v  FourierNb                   0.01087           15062          94.096         0.69719
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010819        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15113          138.37          2.0732


 TIME FOR THE TIME STEP              679:        0.44777E+02

===============================================================


 INSTANT    0.680000000E+02   TIME STEP NUMBER             680
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.124562481E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31459E+02 0.15726E+02
   Friction velocity        uet   :  0.10495E-02 0.29045E+01
   Friction velocity        uk    :  0.31913E-01 0.31307E+01
   Dimensionless distance   yplus :  0.15576E+00 0.32336E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1893   0.44950E-02   0.33142E+00 
c  VelocityY    0.29414E+04    1893   0.44950E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1893   0.44950E-02   0.00000E+00 
c  Pressure     0.45890E+00    6968   0.31128E-01   0.21713E+00 
c  k            0.21814E+04    1476   0.68791E-04   0.92177E+00 
c  omega        0.12794E+08     349   0.20149E-03   0.19565E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1586e+05                             2
a  Local Time Step      1.0683e-05                         44304


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3759         0.79123       -0.010764     -3.1393e-06
v  Velocity[Y]                 -15.328          33.484           6.693          20.057
v  Velocity[Z]                 -29.045          28.893       -0.022368      -0.0040155
v  ǁVelocityǁ                 0.021419          33.793          10.448          20.214
v  Pressure                    -387.48          346.02         -54.516          31.447
v  k                        5.7409e-08          44.126          4.0526          1.6798
v  omega                         1e-24      6.0282e+07          8861.5          11.928
v  turbulent_viscosity      1.6932e-15          1.3316        0.015966         0.11147
v  CourantNb                  0.034349          2064.2           44.04          1.3759
v  FourierNb                  0.010868           15061          94.201         0.69777
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010818        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15122          138.24          2.0737


 TIME FOR THE TIME STEP              680:        0.45641E+02

===============================================================


 INSTANT    0.681000000E+02   TIME STEP NUMBER             681
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.118411236E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31491E+02 0.21854E+02
   Friction velocity        uet   :  0.13858E-02 0.27696E+01
   Friction velocity        uk    :  0.25478E-01 0.31971E+01
   Dimensionless distance   yplus :  0.13605E+00 0.36801E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        480
   Nb of faces within the viscous sub-layer     :        949
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1806   0.46655E-02   0.32978E+00 
c  VelocityY    0.29414E+04    1806   0.46655E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1806   0.46655E-02   0.00000E+00 
c  Pressure     0.43735E+00    6934   0.29087E-01   0.20684E+00 
c  k            0.21815E+04    1452   0.58987E-04   0.81564E+00 
c  omega        0.26105E+08     229   0.92372E-04   0.28609E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3927e+05                             2
a  Local Time Step      1.1493e-05                         44308


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3221         0.90412       -0.010427     -7.7076e-07
v  Velocity[Y]                 -15.201          32.343          6.6795          20.056
v  Velocity[Z]                 -28.657           29.06       -0.071269      -0.0049945
v  ǁVelocityǁ                0.0065014          32.914          10.435          20.214
v  Pressure                    -374.49          344.77         -54.852           30.89
v  k                        1.5322e-07          42.863          4.0161            1.68
v  omega                         1e-24      1.0101e+08          8778.2          11.905
v  turbulent_viscosity      5.0144e-14          1.3397        0.015995         0.11152
v  CourantNb                  0.036347          2059.6          43.852           1.376
v  FourierNb                  0.010866           15027          93.864         0.69806
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010817        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15098          137.72           2.074


 TIME FOR THE TIME STEP              681:        0.43854E+02

===============================================================


 INSTANT    0.682000000E+02   TIME STEP NUMBER             682
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.503439194E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31961E+02 0.20851E+02
   Friction velocity        uet   :  0.72072E-03 0.26269E+01
   Friction velocity        uk    :  0.15466E-01 0.27746E+01
   Dimensionless distance   yplus :  0.59852E-01 0.30454E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :        947
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1909   0.44408E-02   0.33454E+00 
c  VelocityY    0.29415E+04    1909   0.44408E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1909   0.44408E-02   0.00000E+00 
c  Pressure     0.44745E+00    6825   0.26491E-01   0.21104E+00 
c  k            0.21832E+04    1410   0.59038E-04   0.86289E+00 
c  omega        0.62539E+08     125   0.17950E-04   0.90013E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -51889                             2
a  Local Time Step      1.1444e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2553          1.0803      -0.0094425     -1.7186e-06
v  Velocity[Y]                 -14.575          30.367          6.6934          20.056
v  Velocity[Z]                 -30.226          28.962        -0.10976      -0.0059438
v  ǁVelocityǁ                0.0036878          35.687           10.44          20.214
v  Pressure                    -353.85           344.5         -53.856          31.042
v  k                        1.9738e-07          44.412           4.014          1.6804
v  omega                         1e-24      5.0576e+07          8304.6          11.863
v  turbulent_viscosity      3.8229e-14          1.3451         0.01602         0.11156
v  CourantNb                  0.053545          2044.3          43.829          1.3761
v  FourierNb                  0.010864           15132          93.192         0.69806
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14875        0.010817        0.045635


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9704           15176          137.02          2.0742


 TIME FOR THE TIME STEP              682:        0.44019E+02

===============================================================


 INSTANT    0.683000000E+02   TIME STEP NUMBER             683
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.368181135E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31884E+02 0.19827E+02
   Friction velocity        uet   :  0.96869E-03 0.28971E+01
   Friction velocity        uk    :  0.19306E-01 0.29185E+01
   Dimensionless distance   yplus :  0.16140E+00 0.27878E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1986   0.46059E-02   0.33477E+00 
c  VelocityY    0.29416E+04    1986   0.46059E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1986   0.46059E-02   0.00000E+00 
c  Pressure     0.44421E+00    7047   0.28088E-01   0.20838E+00 
c  k            0.21875E+04    1320   0.59459E-04   0.10063E+01 
c  omega        0.18562E+08     248   0.14602E-03   0.17616E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4406e+05                             2
a  Local Time Step       1.153e-05                         44286


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4032          1.3456      -0.0086094      1.2936e-06
v  Velocity[Y]                 -15.284          30.376          6.7321          20.056
v  Velocity[Z]                 -31.673          28.958        -0.13393      -0.0065471
v  ǁVelocityǁ                0.0027892          36.359          10.477          20.214
v  Pressure                     -377.1          345.08         -53.037          31.128
v  k                        4.7281e-09           56.32           4.043           1.681
v  omega                         1e-24      6.3559e+07          8630.2          11.851
v  turbulent_viscosity      2.2721e-14          1.3492        0.016065         0.11162
v  CourantNb                  0.026097          2022.2            43.9          1.3761
v  FourierNb                  0.010863           15318          92.054          0.6982
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14885        0.010818        0.045624


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15361          135.95          2.0743


 TIME FOR THE TIME STEP              683:        0.44900E+02

===============================================================


 INSTANT    0.684000000E+02   TIME STEP NUMBER             684
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.192660291E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29575E+02 0.14656E+02
   Friction velocity        uet   :  0.25376E-02 0.30756E+01
   Friction velocity        uk    :  0.19767E-01 0.30302E+01
   Dimensionless distance   yplus :  0.11731E+00 0.28541E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    2029   0.45385E-02   0.34155E+00 
c  VelocityY    0.29415E+04    2029   0.45385E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    2029   0.45385E-02   0.00000E+00 
c  Pressure     0.42207E+00    7098   0.32068E-01   0.19714E+00 
c  k            0.21962E+04     963   0.68700E-04   0.11536E+01 
c  omega        0.27260E+08     164   0.43754E-04   0.47781E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -61366                             2
a  Local Time Step      1.0821e-05                         44232


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4981          1.6752      -0.0077466      5.3888e-07
v  Velocity[Y]                 -15.201          31.429          6.7927          20.056
v  Velocity[Z]                 -33.185          29.085        -0.12299       -0.007342
v  ǁVelocityǁ                 0.013099          35.848          10.552          20.214
v  Pressure                    -425.06          347.06         -52.442          31.233
v  k                        6.8991e-07          67.353            4.07          1.6818
v  omega                         1e-24      3.2717e+07            8256          11.845
v  turbulent_viscosity      6.8655e-15          1.3529        0.016121         0.11167
v  CourantNb                  0.019067          2397.9          43.871          1.3759
v  FourierNb                  0.010861           15374          91.753          0.6984
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488        0.010819        0.045639


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15421          135.62          2.0743


 TIME FOR THE TIME STEP              684:        0.44919E+02

===============================================================


 INSTANT    0.685000000E+02   TIME STEP NUMBER             685
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.685093731E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31161E+02 0.14170E+02
   Friction velocity        uet   :  0.66731E-03 0.31346E+01
   Friction velocity        uk    :  0.19036E-01 0.32395E+01
   Dimensionless distance   yplus :  0.68621E-01 0.28558E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        436
   Nb of faces within the viscous sub-layer     :       1017
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    2100   0.46583E-02   0.34341E+00 
c  VelocityY    0.29415E+04    2100   0.46583E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    2100   0.46583E-02   0.00000E+00 
c  Pressure     0.44405E+00    6864   0.35886E-01   0.20960E+00 
c  k            0.22104E+04    1248   0.71378E-04   0.12147E+01 
c  omega        0.12256E+08     373   0.21436E-03   0.18626E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4206e+05                             4
a  Local Time Step      1.1681e-05                         44250


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6043          1.8978      -0.0060029     -1.1108e-06
v  Velocity[Y]                 -19.093          29.991           6.852          20.056
v  Velocity[Z]                 -33.091          29.106       -0.070371      -0.0079726
v  ǁVelocityǁ                 0.013045          34.749          10.618          20.214
v  Pressure                    -443.75          348.63         -51.828          31.527
v  k                        1.3396e-07          68.586          4.0852          1.6827
v  omega                         1e-24      6.7883e+07          8784.3          11.876
v  turbulent_viscosity      1.6726e-13           1.354        0.016169         0.11173
v  CourantNb                  0.019818            2729          43.968          1.3759
v  FourierNb                   0.01086           15403          92.359         0.69881
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14872         0.01082        0.045665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91635           15456          136.33          2.0747


 TIME FOR THE TIME STEP              685:        0.46697E+02

===============================================================


 INSTANT    0.686000000E+02   TIME STEP NUMBER             686
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.319611207E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31399E+02 0.15225E+02
   Friction velocity        uet   :  0.11296E-02 0.29770E+01
   Friction velocity        uk    :  0.31267E-01 0.28100E+01
   Dimensionless distance   yplus :  0.17346E+00 0.28171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        409
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    2035   0.46902E-02   0.32675E+00 
c  VelocityY    0.29415E+04    2035   0.46902E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    2035   0.46902E-02   0.00000E+00 
c  Pressure     0.43627E+00    7109   0.35782E-01   0.20555E+00 
c  k            0.22265E+04    1434   0.73912E-04   0.12559E+01 
c  omega        0.39064E+08     130   0.31381E-04   0.71340E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -68747                             1
a  Local Time Step      1.1642e-05                         44297


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6973          1.9441      -0.0039512     -1.2591e-06
v  Velocity[Y]                  -24.49          29.789          6.8698          20.056
v  Velocity[Z]                  -32.84          28.966      0.00085416      -0.0083125
v  ǁVelocityǁ                 0.014604          33.894          10.636          20.214
v  Pressure                    -440.33          349.03         -51.892          31.503
v  k                           5.8e-08          64.188          4.0772          1.6835
v  omega                         1e-24      3.4729e+07          8473.7          11.875
v  turbulent_viscosity      3.3453e-14          1.3537        0.016191         0.11179
v  CourantNb                  0.016435          2621.1          44.136           1.376
v  FourierNb                  0.010859           15397          92.753         0.69898
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14905        0.010819        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15459          136.89           2.075


 TIME FOR THE TIME STEP              686:        0.45021E+02

===============================================================


 INSTANT    0.687000000E+02   TIME STEP NUMBER             687
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.609238638E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31804E+02 0.14212E+02
   Friction velocity        uet   :  0.22375E-02 0.28836E+01
   Friction velocity        uk    :  0.76146E-02 0.30064E+01
   Dimensionless distance   yplus :  0.68573E-01 0.27388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1962   0.45491E-02   0.29497E+00 
c  VelocityY    0.29414E+04    1962   0.45491E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1962   0.45491E-02   0.00000E+00 
c  Pressure     0.45575E+00    7099   0.33263E-01   0.21458E+00 
c  k            0.22402E+04    1494   0.76890E-04   0.12669E+01 
c  omega        0.14514E+08     227   0.66125E-04   0.50049E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2132e+05                             2
a  Local Time Step      1.1532e-05                         44329


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5315          1.8436      -0.0035774      3.2125e-07
v  Velocity[Y]                 -31.538          29.623          6.8156          20.056
v  Velocity[Z]                 -30.911          28.781        0.067734      -0.0084636
v  ǁVelocityǁ                 0.017795          32.922          10.624          20.214
v  Pressure                    -420.66          349.15         -51.897          31.562
v  k                        1.8238e-09           70.07          4.0714          1.6842
v  omega                         1e-24      2.3509e+07          8394.3          11.885
v  turbulent_viscosity       1.045e-14           1.353        0.016163         0.11186
v  CourantNb                  0.019008          2065.7          44.353          1.3761
v  FourierNb                  0.010858           15225          93.109         0.69899
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14819        0.010819        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15295          137.46          2.0751


 TIME FOR THE TIME STEP              687:        0.44910E+02

===============================================================


 INSTANT    0.688000000E+02   TIME STEP NUMBER             688
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.223698957E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31254E+02 0.22175E+02
   Friction velocity        uet   :  0.42063E-03 0.28505E+01
   Friction velocity        uk    :  0.31674E-01 0.29651E+01
   Dimensionless distance   yplus :  0.15197E+00 0.26904E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1897   0.47808E-02   0.27746E+00 
c  VelocityY    0.29415E+04    1897   0.47808E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1897   0.47808E-02   0.00000E+00 
c  Pressure     0.44975E+00    7109   0.31650E-01   0.21196E+00 
c  k            0.22465E+04    1461   0.98893E-04   0.11453E+01 
c  omega        0.11245E+08     316   0.53654E-04   0.31343E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0891e-05                         44256


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2472           1.629      -0.0042954      1.1896e-07
v  Velocity[Y]                  -23.13          29.621          6.7348          20.056
v  Velocity[Z]                 -28.602          28.766         0.10407      -0.0084225
v  ǁVelocityǁ                0.0035932          33.012          10.636          20.214
v  Pressure                    -402.21          347.77         -52.572          31.658
v  k                        1.2873e-08          92.048          4.0966           1.685
v  omega                         1e-24      1.4475e+07          8169.6          11.871
v  turbulent_viscosity      2.4261e-15          1.3531        0.016108         0.11192
v  CourantNb                  0.045699          2056.6          44.456          1.3762
v  FourierNb                  0.010858           15186          93.722         0.69925
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1482        0.010819        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15227          138.18          2.0755


 TIME FOR THE TIME STEP              688:        0.44567E+02

===============================================================


 INSTANT    0.689000000E+02   TIME STEP NUMBER             689
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.413142735E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30369E+02 0.17982E+02
   Friction velocity        uet   :  0.91485E-03 0.24563E+01
   Friction velocity        uk    :  0.96088E-02 0.37358E+01
   Dimensionless distance   yplus :  0.86439E-01 0.33672E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        386
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1859   0.45282E-02   0.27655E+00 
c  VelocityY    0.29415E+04    1859   0.45282E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1859   0.45282E-02   0.00000E+00 
c  Pressure     0.44079E+00    7086   0.33989E-01   0.20908E+00 
c  k            0.22442E+04    1355   0.11767E-03   0.96755E+00 
c  omega        0.10306E+08     481   0.34625E-04   0.20237E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -76212                             2
a  Local Time Step      1.0593e-05                         44237


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0872          1.3906      -0.0050395     -7.4297e-07
v  Velocity[Y]                 -36.785          30.067          6.7099          20.056
v  Velocity[Z]                 -28.724           28.67         0.13916      -0.0082567
v  ǁVelocityǁ                 0.015333          37.352          10.639          20.214
v  Pressure                    -403.86          347.14         -53.886          31.867
v  k                         1.655e-08           89.58          4.1093          1.6859
v  omega                         1e-24      1.1808e+07          8030.7          11.863
v  turbulent_viscosity      5.5924e-14          1.3511        0.016045           0.112
v  CourantNb                  0.052955          2039.9          44.667          1.3765
v  FourierNb                  0.010858           15238          93.445         0.69958
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14779        0.010819        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15280          138.11          2.0761


 TIME FOR THE TIME STEP              689:        0.43913E+02

===============================================================


 INSTANT    0.690000000E+02   TIME STEP NUMBER             690
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.209401463E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39744E+02 0.15845E+02
   Friction velocity        uet   :  0.69103E-03 0.34565E+01
   Friction velocity        uk    :  0.23921E-01 0.41611E+01
   Dimensionless distance   yplus :  0.14894E+00 0.38248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        375
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1879   0.44879E-02   0.27895E+00 
c  VelocityY    0.29415E+04    1879   0.44879E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1879   0.44879E-02   0.00000E+00 
c  Pressure     0.44275E+00    7124   0.36044E-01   0.20968E+00 
c  k            0.22384E+04    1048   0.10212E-03   0.84585E+00 
c  omega        0.10152E+08     388   0.16188E-03   0.12183E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.649e+05                             2
a  Local Time Step      1.1176e-05                         44266


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98035          1.2514      -0.0055449     -1.8548e-06
v  Velocity[Y]                 -23.697          30.539          6.7189          20.056
v  Velocity[Z]                 -29.204           28.86          0.1528      -0.0079172
v  ǁVelocityǁ                  0.01874          33.435          10.615          20.215
v  Pressure                    -404.18          348.49             -55          32.121
v  k                        2.7171e-10          39.304          4.0684          1.6869
v  omega                         1e-24      5.4874e+07          8482.2          11.892
v  turbulent_viscosity      1.9491e-14          1.3471        0.016003         0.11207
v  CourantNb                  0.064811          3096.5           45.13          1.3769
v  FourierNb                  0.010859           15261          92.666         0.69972
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010819        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15307           137.8          2.0766


 TIME FOR THE TIME STEP              690:        0.43668E+02

===============================================================


 INSTANT    0.691000000E+02   TIME STEP NUMBER             691
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.265694714E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30764E+02 0.14506E+02
   Friction velocity        uet   :  0.13214E-02 0.27007E+01
   Friction velocity        uk    :  0.93616E-02 0.28027E+01
   Dimensionless distance   yplus :  0.10742E+00 0.28442E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1877   0.44608E-02   0.28773E+00 
c  VelocityY    0.29416E+04    1877   0.44608E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1877   0.44608E-02   0.00000E+00 
c  Pressure     0.41065E+00    7046   0.34628E-01   0.19514E+00 
c  k            0.22327E+04    1171   0.59647E-04   0.66957E+00 
c  omega        0.20703E+08     217   0.62899E-04   0.13847E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -47241                             2
a  Local Time Step      1.1364e-05                         44280


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2226          1.1528       -0.006141     -3.0636e-06
v  Velocity[Y]                 -17.518          31.035          6.7317          20.055
v  Velocity[Z]                 -29.135          28.747         0.14181      -0.0075205
v  ǁVelocityǁ                0.0088724          33.627          10.579          20.214
v  Pressure                    -403.92          349.51         -55.206          32.165
v  k                        1.4747e-08          46.561          4.0692           1.688
v  omega                         1e-24       4.267e+07          8685.2          11.905
v  turbulent_viscosity      2.6421e-16          1.3437        0.015975         0.11216
v  CourantNb                  0.049098            2743           45.22          1.3769
v  FourierNb                   0.01086           15356          92.402         0.69991
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010817        0.045657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15410          137.62          2.0768


 TIME FOR THE TIME STEP              691:        0.43543E+02

===============================================================


 INSTANT    0.692000000E+02   TIME STEP NUMBER             692
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.391236379E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31742E+02 0.14154E+02
   Friction velocity        uet   :  0.16228E-02 0.28750E+01
   Friction velocity        uk    :  0.18734E-01 0.30270E+01
   Dimensionless distance   yplus :  0.16003E+00 0.28445E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        533
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1885   0.44623E-02   0.31043E+00 
c  VelocityY    0.29418E+04    1885   0.44623E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1885   0.44623E-02   0.00000E+00 
c  Pressure     0.42748E+00    7015   0.32655E-01   0.20188E+00 
c  k            0.22281E+04    1435   0.58833E-04   0.65588E+00 
c  omega        0.18351E+08     285   0.48178E-04   0.48638E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.1358e+05                             2
a  Local Time Step      1.0756e-05                         44332


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4171          1.0325       -0.006652     -3.8195e-06
v  Velocity[Y]                 -16.651          33.051          6.7418          20.055
v  Velocity[Z]                 -28.827          28.731         0.10286      -0.0067312
v  ǁVelocityǁ                0.0096511          33.479          10.549          20.214
v  Pressure                    -402.46          349.48         -54.671          32.138
v  k                        2.1075e-07          51.384          4.0846          1.6892
v  omega                         1e-24      2.1537e+07          8316.4          11.861
v  turbulent_viscosity      1.4854e-14          1.3385         0.01598         0.11224
v  CourantNb                  0.053865          2012.3          44.867          1.3768
v  FourierNb                  0.010861           15374          93.407         0.70075
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14808        0.010817        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15435          138.27          2.0775


 TIME FOR THE TIME STEP              692:        0.44155E+02

===============================================================


 INSTANT    0.693000000E+02   TIME STEP NUMBER             693
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.566888132E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31781E+02 0.15030E+02
   Friction velocity        uet   :  0.79733E-03 0.29108E+01
   Friction velocity        uk    :  0.21574E-01 0.32032E+01
   Dimensionless distance   yplus :  0.15045E+00 0.30396E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        519
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1684   0.44381E-02   0.34005E+00 
c  VelocityY    0.29419E+04    1684   0.44381E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1684   0.44381E-02   0.00000E+00 
c  Pressure     0.43817E+00    6954   0.30694E-01   0.20689E+00 
c  k            0.22234E+04    1487   0.61530E-04   0.72628E+00 
c  omega        0.11075E+08     422   0.68816E-03   0.12817E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3174e+05                             2
a  Local Time Step      1.1509e-05                         44366


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6942          1.0431      -0.0065091     -1.2014e-06
v  Velocity[Y]                 -15.324          32.995          6.7417          20.056
v  Velocity[Z]                 -28.632           28.77        0.049116      -0.0059601
v  ǁVelocityǁ                 0.016997          33.589          10.533          20.215
v  Pressure                    -392.11          347.62          -54.54          31.584
v  k                        1.9809e-07          44.862          4.0653          1.6904
v  omega                         1e-24      2.6866e+08          9961.7          11.997
v  turbulent_viscosity      9.2543e-14          1.3333        0.015984         0.11234
v  CourantNb                  0.019103          2012.9          44.492          1.3766
v  FourierNb                  0.010861           15322          94.846           0.702
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14828        0.010818        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15392          139.34          2.0786


 TIME FOR THE TIME STEP              693:        0.42470E+02

===============================================================


 INSTANT    0.694000000E+02   TIME STEP NUMBER             694
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.125648024E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31062E+02 0.19347E+02
   Friction velocity        uet   :  0.19243E-02 0.28087E+01
   Friction velocity        uk    :  0.24997E-01 0.29213E+01
   Dimensionless distance   yplus :  0.11904E+00 0.36566E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        494
   Nb of faces within the viscous sub-layer     :        975
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1606   0.45803E-02   0.35802E+00 
c  VelocityY    0.29419E+04    1606   0.45803E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1606   0.45803E-02   0.00000E+00 
c  Pressure     0.44021E+00    6960   0.30525E-01   0.20805E+00 
c  k            0.22179E+04    1443   0.57990E-04   0.67703E+00 
c  omega        0.28651E+09     110   0.86778E-05   0.33053E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0587e+05                             1
a  Local Time Step      1.1346e-05                         44370


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9479          1.0721      -0.0060919     -8.2292e-08
v  Velocity[Y]                 -17.093          33.496          6.7046          20.057
v  Velocity[Z]                 -28.537          28.785      -0.0068269      -0.0049449
v  ǁVelocityǁ                0.0078915           33.85          10.519          20.216
v  Pressure                    -374.43          345.69         -54.038          31.136
v  k                        7.2696e-07          35.196          4.0479          1.6916
v  omega                         1e-24      1.3453e+08            9054          11.907
v  turbulent_viscosity      6.2839e-14            1.33        0.015959         0.11243
v  CourantNb                  0.067999          2003.4           44.35          1.3768
v  FourierNb                  0.010861           15230          94.734         0.70278
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14803        0.010819         0.04563


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15308          139.08          2.0796


 TIME FOR THE TIME STEP              694:        0.42076E+02

===============================================================


 INSTANT    0.695000000E+02   TIME STEP NUMBER             695
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.391223243E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32254E+02 0.20262E+02
   Friction velocity        uet   :  0.74125E-03 0.26994E+01
   Friction velocity        uk    :  0.13304E-01 0.32270E+01
   Dimensionless distance   yplus :  0.13995E+00 0.29910E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1705   0.44996E-02   0.37564E+00 
c  VelocityY    0.29418E+04    1705   0.44996E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1705   0.44996E-02   0.00000E+00 
c  Pressure     0.43789E+00    6998   0.28653E-01   0.20769E+00 
c  k            0.22128E+04    1381   0.54410E-04   0.71449E+00 
c  omega        0.73051E+08     144   0.19194E-04   0.90764E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4257e+05                             2
a  Local Time Step      1.2033e-05                         44357


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1311            1.11       -0.005433      6.6208e-07
v  Velocity[Y]                  -16.78          30.591          6.6767          20.057
v  Velocity[Z]                 -30.613          28.794       -0.043915      -0.0041901
v  ǁVelocityǁ                0.0095278          34.838          10.506          20.216
v  Pressure                    -359.22          345.48         -52.981          30.977
v  k                         8.628e-08          40.361          4.0403           1.693
v  omega                         1e-24      6.7684e+07          8568.4          11.869
v  turbulent_viscosity      7.3362e-14          1.3244        0.015935         0.11253
v  CourantNb                 0.0091769          2018.5          44.222          1.3769
v  FourierNb                   0.01086           15116          93.092         0.70304
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14886        0.010819        0.045643


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.81365           15157          137.31            2.08


 TIME FOR THE TIME STEP              695:        0.42884E+02

===============================================================


 INSTANT    0.696000000E+02   TIME STEP NUMBER             696
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.399221989E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31965E+02 0.20143E+02
   Friction velocity        uet   :  0.15083E-02 0.28221E+01
   Friction velocity        uk    :  0.16402E-01 0.30088E+01
   Dimensionless distance   yplus :  0.10203E+00 0.28484E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        540
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1795   0.44202E-02   0.39138E+00 
c  VelocityY    0.29416E+04    1795   0.44202E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1795   0.44202E-02   0.00000E+00 
c  Pressure     0.44006E+00    7013   0.29107E-01   0.20862E+00 
c  k            0.22093E+04    1281   0.55446E-04   0.81814E+00 
c  omega        0.21505E+08     164   0.34032E-04   0.50692E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9553e+05                             1
a  Local Time Step      1.1488e-05                         44348


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3376          1.1312       -0.004826     -1.4016e-06
v  Velocity[Y]                 -15.682          30.512          6.6753          20.057
v  Velocity[Z]                 -31.371          29.271       -0.083734      -0.0032177
v  ǁVelocityǁ                 0.005926           36.73          10.503          20.216
v  Pressure                    -349.81          347.89         -51.486          31.049
v  k                         8.694e-08          51.968          4.0575          1.6944
v  omega                         1e-24      3.4711e+07          8236.5           11.84
v  turbulent_viscosity      1.5024e-15          1.3208        0.015957         0.11263
v  CourantNb                  0.062832          2038.6          44.249          1.3769
v  FourierNb                   0.01086           15292           92.25         0.70394
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010821        0.045706


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15338           136.5          2.0809


 TIME FOR THE TIME STEP              696:        0.43722E+02

===============================================================


 INSTANT    0.697000000E+02   TIME STEP NUMBER             697
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.195072747E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30632E+02 0.17160E+02
   Friction velocity        uet   :  0.79773E-03 0.30794E+01
   Friction velocity        uk    :  0.20526E-01 0.31525E+01
   Dimensionless distance   yplus :  0.10698E+00 0.28401E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1805   0.44006E-02   0.40385E+00 
c  VelocityY    0.29415E+04    1805   0.44006E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1805   0.44006E-02   0.00000E+00 
c  Pressure     0.40817E+00    7145   0.33033E-01   0.19358E+00 
c  k            0.22088E+04    1227   0.64934E-04   0.96052E+00 
c  omega        0.13977E+08     204   0.32049E-04   0.17990E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -64803                             1
a  Local Time Step      1.1899e-05                         44390


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4072          1.1511      -0.0042712      2.6103e-07
v  Velocity[Y]                 -15.166          32.971          6.6925          20.056
v  Velocity[Z]                  -33.16          28.788        -0.09568      -0.0021799
v  ǁVelocityǁ                0.0083497          35.997          10.539          20.215
v  Pressure                    -410.17          349.33         -50.453          31.132
v  k                        3.9516e-07          62.796          4.0746          1.6959
v  omega                         1e-24      1.9098e+07          8051.3          11.837
v  turbulent_viscosity      2.9521e-15          1.3162        0.016014         0.11274
v  CourantNb                  0.043138          2281.6          44.083          1.3766
v  FourierNb                   0.01086           15429          92.348         0.70514
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14938         0.01082        0.045732


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0029           15484          136.43          2.0818


 TIME FOR THE TIME STEP              697:        0.44354E+02

===============================================================


 INSTANT    0.698000000E+02   TIME STEP NUMBER             698
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.291449346E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30280E+02 0.14327E+02
   Friction velocity        uet   :  0.23496E-03 0.32108E+01
   Friction velocity        uk    :  0.21239E-01 0.30765E+01
   Dimensionless distance   yplus :  0.10805E+00 0.28010E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        498
   Nb of faces within the viscous sub-layer     :        954
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1903   0.46011E-02   0.41577E+00 
c  VelocityY    0.29415E+04    1903   0.46011E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1903   0.46011E-02   0.00000E+00 
c  Pressure     0.40626E+00    7158   0.36727E-01   0.19195E+00 
c  k            0.22135E+04    1403   0.70760E-04   0.10541E+01 
c  omega        0.29272E+27       2   0.12264E-22   0.11062E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5451e+05                             1
a  Local Time Step      1.0929e-05                         44394


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4767          1.1506      -0.0038551     -5.6215e-07
v  Velocity[Y]                  -16.33          31.637          6.7235          20.056
v  Velocity[Z]                 -33.119          28.751       -0.064716      -0.0011002
v  ǁVelocityǁ                  0.01187          35.079          10.579          20.215
v  Pressure                    -440.34          349.27         -49.953          31.262
v  k                        5.8844e-07          66.417           4.081          1.6972
v  omega                         1e-24      1.2835e+07          7906.9           11.82
v  turbulent_viscosity      5.8005e-14          1.3099        0.016085         0.11284
v  CourantNb                  0.014816          2736.5          43.892          1.3764
v  FourierNb                  0.010859           15447          92.671         0.70651
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14905        0.010819        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15511          136.56          2.0829


 TIME FOR THE TIME STEP              698:        0.46030E+02

===============================================================


 INSTANT    0.699000000E+02   TIME STEP NUMBER             699
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.917561675E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31376E+02 0.14633E+02
   Friction velocity        uet   :  0.14884E-02 0.31321E+01
   Friction velocity        uk    :  0.24630E-01 0.31374E+01
   Dimensionless distance   yplus :  0.15841E+00 0.27304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1939   0.46537E-02   0.40978E+00 
c  VelocityY    0.29415E+04    1939   0.46537E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1939   0.46537E-02   0.00000E+00 
c  Pressure     0.42542E+00    7038   0.35874E-01   0.20096E+00 
c  k            0.22205E+04    1516   0.73531E-04   0.11587E+01 
c  omega        0.10768E+08     282   0.23813E-03   0.17981E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -94553                             1
a  Local Time Step      1.1393e-05                         44355


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2929           1.082      -0.0036459     -5.9649e-07
v  Velocity[Y]                 -23.788          29.992          6.7368          20.056
v  Velocity[Z]                 -31.784          28.665      -0.0097224      0.00011691
v  ǁVelocityǁ                 0.018757          33.321          10.587          20.216
v  Pressure                    -446.18          347.99         -50.102          31.324
v  k                         7.314e-07          58.755          4.0613          1.6983
v  omega                         1e-24      7.2013e+07          8438.3          11.886
v  turbulent_viscosity       1.206e-13          1.3024        0.016121         0.11295
v  CourantNb                  0.035242          2753.3          43.937          1.3763
v  FourierNb                  0.010859           15222          92.892         0.70732
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14786        0.010818         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94607           15296          136.83          2.0836


 TIME FOR THE TIME STEP              699:        0.46598E+02

===============================================================


 INSTANT    0.700000000E+02   TIME STEP NUMBER             700
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.139518701E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31802E+02 0.14248E+02
   Friction velocity        uet   :  0.23509E-02 0.28402E+01
   Friction velocity        uk    :  0.29453E-01 0.29397E+01
   Dimensionless distance   yplus :  0.78638E-01 0.26697E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1839   0.46101E-02   0.38060E+00 
c  VelocityY    0.29413E+04    1839   0.46101E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1839   0.46101E-02   0.00000E+00 
c  Pressure     0.44437E+00    6959   0.32460E-01   0.21060E+00 
c  k            0.22277E+04    1411   0.71475E-04   0.10964E+01 
c  omega        0.34845E+08     140   0.45663E-04   0.11158E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8857e+05                             2
a  Local Time Step      1.1146e-05                         44315


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1926          1.0005      -0.0031098     -1.2334e-06
v  Velocity[Y]                 -27.692          29.863          6.6949          20.056
v  Velocity[Z]                 -32.143          28.709        0.039089       0.0012577
v  ǁVelocityǁ                 0.015994          33.272          10.562          20.215
v  Pressure                    -432.16           346.5         -50.299          31.193
v  k                        2.5468e-07          44.877          4.0173           1.699
v  omega                         1e-24      3.7224e+07          8641.1          11.936
v  turbulent_viscosity      8.7887e-14          1.2938        0.016087         0.11305
v  CourantNb                  0.052073          2306.6          44.051          1.3763
v  FourierNb                  0.010857           15288          92.411         0.70759
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14798        0.010818         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15330          136.46          2.0839


 TIME FOR THE TIME STEP              700:        0.45409E+02

===============================================================


 INSTANT    0.701000000E+02   TIME STEP NUMBER             701
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240515336E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30072E+02 0.17250E+02
   Friction velocity        uet   :  0.29173E-02 0.28087E+01
   Friction velocity        uk    :  0.18743E-01 0.29756E+01
   Dimensionless distance   yplus :  0.14146E+00 0.27539E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        371
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1816   0.45392E-02   0.35477E+00 
c  VelocityY    0.29413E+04    1816   0.45392E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1816   0.45392E-02   0.00000E+00 
c  Pressure     0.42139E+00    7005   0.30880E-01   0.20050E+00 
c  k            0.22282E+04    1286   0.79576E-04   0.10269E+01 
c  omega        0.14579E+08     242   0.54857E-04   0.45905E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -40356                             2
a  Local Time Step      1.0975e-05                         44325


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0509         0.91475      -0.0024541      1.0225e-06
v  Velocity[Y]                 -31.551          29.749          6.6133          20.056
v  Velocity[Z]                 -30.415           28.79        0.060549       0.0022288
v  ǁVelocityǁ                0.0047178          33.151          10.575          20.215
v  Pressure                     -405.7          345.92         -50.834           31.16
v  k                        1.6072e-07          76.303          4.0299          1.6995
v  omega                         1e-24      2.0301e+07          8207.1            11.9
v  turbulent_viscosity      3.6881e-14          1.2878         0.01604         0.11314
v  CourantNb                  0.027269          2012.3          44.072          1.3762
v  FourierNb                  0.010857           15350          92.747         0.70799
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889        0.010818        0.045635


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15390          136.82          2.0842


 TIME FOR THE TIME STEP              701:        0.45272E+02

===============================================================


 INSTANT    0.702000000E+02   TIME STEP NUMBER             702
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.424142318E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29591E+02 0.21642E+02
   Friction velocity        uet   :  0.44439E-03 0.27230E+01
   Friction velocity        uk    :  0.11167E-01 0.32050E+01
   Dimensionless distance   yplus :  0.10045E+00 0.29817E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        369
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1866   0.44591E-02   0.34326E+00 
c  VelocityY    0.29411E+04    1866   0.44591E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1866   0.44591E-02   0.00000E+00 
c  Pressure     0.42693E+00    7043   0.34600E-01   0.20207E+00 
c  k            0.22218E+04    1125   0.10783E-03   0.89951E+00 
c  omega        0.10521E+08     462   0.67576E-04   0.27863E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5271e+05                             3
a  Local Time Step      1.0913e-05                         44304


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8859          1.1826      -0.0022818       3.279e-06
v  Velocity[Y]                 -37.467          30.128          6.5899          20.056
v  Velocity[Z]                 -29.239          28.987        0.079437       0.0027749
v  ǁVelocityǁ                0.0080679          38.035          10.589          20.215
v  Pressure                    -407.29          346.79         -52.072          31.348
v  k                         4.598e-09          103.16          4.0961          1.6998
v  omega                         1e-24      1.3828e+07          8124.8          11.899
v  turbulent_viscosity      4.0132e-14          1.2821        0.015987         0.11322
v  CourantNb                    0.0187          2025.7            44.2          1.3762
v  FourierNb                  0.010856           15329          92.786         0.70848
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1481        0.010819         0.04565


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83398           15375          136.99          2.0847


 TIME FOR THE TIME STEP              702:        0.45924E+02

===============================================================


 INSTANT    0.703000000E+02   TIME STEP NUMBER             703
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.427625245E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46207E+02 0.13700E+02
   Friction velocity        uet   :  0.26257E-02 0.34299E+01
   Friction velocity        uk    :  0.10716E-01 0.47792E+01
   Dimensionless distance   yplus :  0.10540E+00 0.39801E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        358
   Nb of faces within the viscous sub-layer     :       1067
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1855   0.45088E-02   0.34113E+00 
c  VelocityY    0.29411E+04    1855   0.45088E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1855   0.45088E-02   0.00000E+00 
c  Pressure     0.42636E+00    7040   0.39028E-01   0.20202E+00 
c  k            0.22122E+04    1256   0.11890E-03   0.75967E+00 
c  omega        0.14841E+08     447   0.60557E-04   0.41980E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0115e+05                             3
a  Local Time Step      1.1318e-05                         44296


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7252           1.443      -0.0024844      1.1786e-06
v  Velocity[Y]                 -27.143          30.487          6.6165          20.056
v  Velocity[Z]                 -28.672          28.708        0.091677       0.0031689
v  ǁVelocityǁ                0.0085037          33.563          10.584          20.215
v  Pressure                    -406.97          347.18          -53.76          31.487
v  k                        6.1472e-09          50.354          4.1061          1.6999
v  omega                         1e-24      3.2707e+07          8283.7          11.939
v  turbulent_viscosity      3.8662e-15          1.2759        0.015967          0.1133
v  CourantNb                  0.003476          2601.3          44.444          1.3763
v  FourierNb                  0.010855           15335          92.965         0.70913
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14908         0.01082        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7428           15388          137.41          2.0854


 TIME FOR THE TIME STEP              703:        0.44949E+02

===============================================================


 INSTANT    0.704000000E+02   TIME STEP NUMBER             704
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.372882225E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31617E+02 0.14000E+02
   Friction velocity        uet   :  0.29156E-03 0.28908E+01
   Friction velocity        uk    :  0.24469E-01 0.28489E+01
   Dimensionless distance   yplus :  0.16595E+00 0.28557E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :       1055
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1885   0.43591E-02   0.34253E+00 
c  VelocityY    0.29410E+04    1885   0.43591E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1885   0.43591E-02   0.00000E+00 
c  Pressure     0.44437E+00    7024   0.37467E-01   0.21217E+00 
c  k            0.22030E+04    1393   0.65043E-04   0.62158E+00 
c  omega        0.12443E+08     290   0.26112E-03   0.29993E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0012e+05                             2
a  Local Time Step      1.1411e-05                         44266


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.638          1.6277      -0.0023241      1.1883e-06
v  Velocity[Y]                 -18.008          30.764          6.6556          20.056
v  Velocity[Z]                 -30.549          28.735        0.081038       0.0039106
v  ǁVelocityǁ                  0.01359          33.544          10.557          20.216
v  Pressure                    -406.81           346.9         -54.636            31.6
v  k                        1.8879e-10          52.375          4.1396          1.6997
v  omega                         1e-24      6.6029e+07          9220.9          11.976
v  turbulent_viscosity      1.2322e-14          1.2702        0.015972         0.11336
v  CourantNb                  0.025207          2891.8          44.641          1.3762
v  FourierNb                  0.010854           15429          93.089         0.70962
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14886        0.010821        0.045673


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7388           15492          137.73          2.0858


 TIME FOR THE TIME STEP              704:        0.46218E+02

===============================================================


 INSTANT    0.705000000E+02   TIME STEP NUMBER             705
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.306257781E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.33871E+02 0.13949E+02
   Friction velocity        uet   :  0.15869E-02 0.28735E+01
   Friction velocity        uk    :  0.29939E-01 0.30393E+01
   Dimensionless distance   yplus :  0.15681E+00 0.27913E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        501
   Nb of faces within the viscous sub-layer     :       1092
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2005   0.42686E-02   0.34946E+00 
c  VelocityY    0.29410E+04    2005   0.42686E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2005   0.42686E-02   0.00000E+00 
c  Pressure     0.44667E+00    7055   0.33126E-01   0.21410E+00 
c  k            0.21959E+04    1445   0.67992E-04   0.59670E+00 
c  omega        0.34145E+08     318   0.10136E-03   0.35761E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5131e+05                             3
a  Local Time Step      1.0824e-05                         44241


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5423          1.7141      -0.0016059     -3.7591e-07
v  Velocity[Y]                 -16.949           33.14          6.6919          20.057
v  Velocity[Z]                 -28.622          28.762        0.054136       0.0039107
v  ǁVelocityǁ                 0.011202          33.563          10.523          20.216
v  Pressure                     -406.3          346.19          -54.51          31.596
v  k                        1.8528e-08          54.442          4.1692          1.6994
v  omega                         1e-24      7.6694e+07          9602.6          11.989
v  turbulent_viscosity      2.3861e-16          1.2648        0.016016         0.11341
v  CourantNb                  0.013701          2067.4          44.512          1.3761
v  FourierNb                  0.010853           15453           95.29          0.7109
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14807        0.010821        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15524           139.8           2.087


 TIME FOR THE TIME STEP              705:        0.47207E+02

===============================================================


 INSTANT    0.706000000E+02   TIME STEP NUMBER             706
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.418378028E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32106E+02 0.14562E+02
   Friction velocity        uet   :  0.22197E-02 0.29430E+01
   Friction velocity        uk    :  0.20631E-01 0.30297E+01
   Dimensionless distance   yplus :  0.61024E-01 0.32137E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        556
   Nb of faces within the viscous sub-layer     :       1077
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1723   0.44189E-02   0.36395E+00 
c  VelocityY    0.29408E+04    1723   0.44189E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1723   0.44189E-02   0.00000E+00 
c  Pressure     0.41984E+00    6745   0.29567E-01   0.19928E+00 
c  k            0.21887E+04    1410   0.64191E-04   0.67694E+00 
c  omega        0.39071E+08     343   0.41169E-04   0.11033E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.8824e+05                             1
a  Local Time Step      1.0973e-05                         44194


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4501          1.6971      -0.0005146     -2.3658e-06
v  Velocity[Y]                 -15.198          33.443          6.7009          20.056
v  Velocity[Z]                 -28.655          29.003        0.013849       0.0037968
v  ǁVelocityǁ                  0.01554          33.848          10.485          20.215
v  Pressure                    -398.34          344.08         -54.603          31.125
v  k                        3.6977e-09          50.735          4.1439          1.6987
v  omega                         1e-24      3.8991e+07          8785.6          11.921
v  turbulent_viscosity      8.1973e-14          1.2598        0.016059         0.11344
v  CourantNb                  0.023319          2060.2          44.343           1.376
v  FourierNb                  0.010851           15418          97.544         0.71239
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010822        0.045757


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15495          141.89          2.0884


 TIME FOR THE TIME STEP              706:        0.43576E+02

===============================================================


 INSTANT    0.707000000E+02   TIME STEP NUMBER             707
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.186532173E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30781E+02 0.13572E+02
   Friction velocity        uet   :  0.77431E-03 0.28526E+01
   Friction velocity        uk    :  0.12156E-01 0.31477E+01
   Dimensionless distance   yplus :  0.10090E+00 0.37324E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        528
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1825   0.44161E-02   0.37731E+00 
c  VelocityY    0.29407E+04    1825   0.44161E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1825   0.44161E-02   0.00000E+00 
c  Pressure     0.44174E+00    6825   0.29565E-01   0.20802E+00 
c  k            0.21809E+04    1303   0.56818E-04   0.59451E+00 
c  omega        0.15041E+08     280   0.51281E-04   0.34343E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3353e+05                             2
a  Local Time Step      1.1002e-05                         44212


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3261          1.6304       0.0012631     -1.6257e-06
v  Velocity[Y]                 -15.238          34.177          6.6724          20.057
v  Velocity[Z]                 -28.783          29.109       -0.033399       0.0037785
v  ǁVelocityǁ                0.0034315          34.425          10.478          20.216
v  Pressure                    -384.28          343.26         -55.055           30.56
v  k                        1.0756e-07          40.736          4.1213          1.6979
v  omega                         1e-24      2.0784e+07          8284.7          11.869
v  turbulent_viscosity      1.1662e-14          1.2556        0.016063         0.11345
v  CourantNb                   0.01736            2045          44.031           1.376
v  FourierNb                  0.010851           15356          97.369         0.71281
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14808        0.010822        0.045727


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.86921           15397           141.4          2.0888


 TIME FOR THE TIME STEP              707:        0.44047E+02

===============================================================


 INSTANT    0.708000000E+02   TIME STEP NUMBER             708
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.154147771E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30589E+02 0.21313E+02
   Friction velocity        uet   :  0.83819E-03 0.27643E+01
   Friction velocity        uk    :  0.70219E-02 0.34038E+01
   Dimensionless distance   yplus :  0.80727E-01 0.32770E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        534
   Nb of faces within the viscous sub-layer     :        971
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1854   0.44948E-02   0.39065E+00 
c  VelocityY    0.29406E+04    1854   0.44948E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1854   0.44948E-02   0.00000E+00 
c  Pressure     0.43573E+00    6938   0.28239E-01   0.20715E+00 
c  k            0.21745E+04    1030   0.53776E-04   0.61150E+00 
c  omega        0.10598E+08     242   0.47528E-04   0.15109E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3974e+05                             1
a  Local Time Step      1.1579e-05                         44233


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3489          1.5619       0.0024457     -4.4285e-07
v  Velocity[Y]                 -15.244          30.947          6.6594          20.056
v  Velocity[Z]                 -29.332          29.178       -0.064942       0.0031748
v  ǁVelocityǁ                 0.008402          33.941          10.475          20.215
v  Pressure                    -369.91          344.77         -54.696          30.426
v  k                        2.8053e-08          41.036          4.1017           1.697
v  omega                         1e-24      1.8002e+07          8022.4          11.839
v  turbulent_viscosity      1.2784e-14          1.2519        0.016065         0.11345
v  CourantNb                  0.022129          2022.9          43.893          1.3762
v  FourierNb                  0.010851           15419          96.136         0.71269
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010822         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15465          140.03          2.0889


 TIME FOR THE TIME STEP              708:        0.44140E+02

===============================================================


 INSTANT    0.709000000E+02   TIME STEP NUMBER             709
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.780138686E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31495E+02 0.20264E+02
   Friction velocity        uet   :  0.54456E-03 0.27344E+01
   Friction velocity        uk    :  0.14071E-01 0.28730E+01
   Dimensionless distance   yplus :  0.12685E+00 0.28425E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        485
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1815   0.44232E-02   0.39437E+00 
c  VelocityY    0.29405E+04    1815   0.44232E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1815   0.44232E-02   0.00000E+00 
c  Pressure     0.46111E+00    6970   0.27898E-01   0.21868E+00 
c  k            0.21697E+04    1265   0.51996E-04   0.71692E+00 
c  omega        0.10424E+08     255   0.72234E-03   0.15270E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3483e+05                             1
a  Local Time Step       1.133e-05                         44260


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3709            1.47       0.0030024     -7.0583e-07
v  Velocity[Y]                 -15.153          30.406          6.6784          20.056
v  Velocity[Z]                 -30.744          28.984        -0.08586       0.0028439
v  ǁVelocityǁ                 0.011411          36.507          10.486          20.214
v  Pressure                    -344.97          346.64         -53.551          30.604
v  k                         1.352e-07          48.982          4.0962           1.696
v  omega                         1e-24      3.0047e+08          9723.3          11.944
v  turbulent_viscosity       2.581e-15          1.2527        0.016083         0.11343
v  CourantNb                  0.041878          2008.8          44.031          1.3763
v  FourierNb                  0.010851           15524          95.285         0.71254
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814        0.010822        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0094           15581          139.32          2.0889


 TIME FOR THE TIME STEP              709:        0.44343E+02

===============================================================


 INSTANT    0.710000000E+02   TIME STEP NUMBER             710
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.402800066E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30961E+02 0.16788E+02
   Friction velocity        uet   :  0.78738E-03 0.30558E+01
   Friction velocity        uk    :  0.12212E-01 0.29566E+01
   Dimensionless distance   yplus :  0.10178E+00 0.28103E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1731   0.44014E-02   0.38716E+00 
c  VelocityY    0.29406E+04    1731   0.44014E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1731   0.44014E-02   0.00000E+00 
c  Pressure     0.44281E+00    7018   0.31266E-01   0.20929E+00 
c  k            0.21684E+04    1426   0.59313E-04   0.87990E+00 
c  omega        0.35634E+09      96   0.84302E-05   0.38654E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3265e+05                             2
a  Local Time Step      1.1347e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2819          1.3607       0.0028058     -4.8854e-07
v  Velocity[Y]                 -14.635          30.378          6.7233          20.056
v  Velocity[Z]                  -32.55          28.772       -0.084449       0.0027473
v  ǁVelocityǁ                 0.022239          37.155           10.53          20.215
v  Pressure                    -402.11          347.34         -52.377           30.91
v  k                        3.6759e-10          61.653          4.0986          1.6948
v  omega                         1e-24      1.5041e+08          8840.4          11.889
v  turbulent_viscosity      1.2438e-13          1.2562        0.016115         0.11339
v  CourantNb                   0.06016          2022.8          44.049          1.3762
v  FourierNb                  0.010851           15601          94.241          0.7123
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010821        0.045662


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15669          138.29          2.0885


 TIME FOR THE TIME STEP              710:        0.43956E+02

===============================================================


 INSTANT    0.711000000E+02   TIME STEP NUMBER             711
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.138870241E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30473E+02 0.14164E+02
   Friction velocity        uet   :  0.29307E-03 0.31955E+01
   Friction velocity        uk    :  0.25575E-01 0.32117E+01
   Dimensionless distance   yplus :  0.17506E+00 0.27336E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1709   0.45466E-02   0.38846E+00 
c  VelocityY    0.29405E+04    1709   0.45466E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1709   0.45466E-02   0.00000E+00 
c  Pressure     0.43131E+00    7045   0.35452E-01   0.20298E+00 
c  k            0.21728E+04    1527   0.66492E-04   0.97659E+00 
c  omega        0.90208E+08     128   0.31407E-04   0.26006E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0041e+05                             3
a  Local Time Step      1.1635e-05                         44359


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2236          1.2595       0.0021336     -5.1879e-07
v  Velocity[Y]                 -15.211          30.843          6.7822          20.055
v  Velocity[Z]                 -32.762          28.797       -0.043697       0.0022388
v  ǁVelocityǁ                 0.015931          35.016          10.592          20.214
v  Pressure                    -432.63          346.99          -51.37          31.158
v  k                         1.865e-08          68.133          4.0996          1.6935
v  omega                         1e-24      7.5579e+07          8997.8          11.902
v  turbulent_viscosity      1.2538e-15            1.26        0.016147         0.11334
v  CourantNb                  0.051593            2598          44.057           1.376
v  FourierNb                  0.010851           15482          94.072         0.71209
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010819        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15558          138.13          2.0881


 TIME FOR THE TIME STEP              711:        0.43831E+02

===============================================================


 INSTANT    0.712000000E+02   TIME STEP NUMBER             712
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.212951015E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31835E+02 0.13945E+02
   Friction velocity        uet   :  0.24945E-02 0.30541E+01
   Friction velocity        uk    :  0.28218E-01 0.31567E+01
   Dimensionless distance   yplus :  0.10666E+00 0.27085E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        388
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1739   0.46004E-02   0.39574E+00 
c  VelocityY    0.29406E+04    1739   0.46004E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1739   0.46004E-02   0.00000E+00 
c  Pressure     0.44428E+00    7112   0.37332E-01   0.20884E+00 
c  k            0.21820E+04    1502   0.69270E-04   0.10153E+01 
c  omega        0.37762E+08     140   0.38508E-04   0.88010E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4297e+05                             3
a  Local Time Step      1.1779e-05                         44397


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1756          1.1683       0.0010293       5.448e-07
v  Velocity[Y]                 -19.653          30.073          6.8299          20.055
v  Velocity[Z]                 -31.813           28.73        0.017368       0.0014416
v  ǁVelocityǁ                0.0068816          33.471          10.623          20.214
v  Pressure                    -439.62           345.5         -51.169          31.325
v  k                        2.2911e-09           63.54          4.0691           1.692
v  omega                         1e-24      3.8581e+07          8577.3          11.898
v  turbulent_viscosity      5.1056e-15           1.266        0.016156         0.11327
v  CourantNb                  0.052023          2689.1           44.16           1.376
v  FourierNb                  0.010852           15620          94.387         0.71175
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14859        0.010819        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15663          138.55          2.0878


 TIME FOR THE TIME STEP              712:        0.44558E+02

===============================================================


 INSTANT    0.713000000E+02   TIME STEP NUMBER             713
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.904709274E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31549E+02 0.13710E+02
   Friction velocity        uet   :  0.54283E-03 0.28525E+01
   Friction velocity        uk    :  0.14109E-01 0.28409E+01
   Dimensionless distance   yplus :  0.12706E+00 0.27590E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        350
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1844   0.46227E-02   0.36696E+00 
c  VelocityY    0.29406E+04    1844   0.46227E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1844   0.46227E-02   0.00000E+00 
c  Pressure     0.45868E+00    7083   0.35544E-01   0.21768E+00 
c  k            0.21910E+04    1383   0.69615E-04   0.10590E+01 
c  omega        0.19220E+08     225   0.53116E-04   0.53010E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3757e+05                             2
a  Local Time Step      1.1768e-05                         44398


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0923          1.0545        0.000251      6.7177e-07
v  Velocity[Y]                 -24.166          29.879          6.8107          20.057
v  Velocity[Z]                 -31.389          28.722        0.089545       0.0010257
v  ǁVelocityǁ                0.0064022          32.349          10.601          20.215
v  Pressure                     -427.8          346.82         -51.111          31.515
v  k                         1.388e-09           50.25          4.0227          1.6903
v  omega                         1e-24      2.3665e+07          8558.3          11.895
v  turbulent_viscosity      3.4822e-15          1.2725        0.016112         0.11318
v  CourantNb                  0.022986          2288.1          44.434          1.3763
v  FourierNb                  0.010853           15671          94.295         0.71098
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869        0.010819          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15713          138.73          2.0873


 TIME FOR THE TIME STEP              713:        0.44245E+02

===============================================================


 INSTANT    0.714000000E+02   TIME STEP NUMBER             714
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.871572087E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30258E+02 0.16334E+02
   Friction velocity        uet   :  0.10825E-02 0.27255E+01
   Friction velocity        uk    :  0.17893E-01 0.29547E+01
   Dimensionless distance   yplus :  0.11408E+00 0.28036E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        302
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1914   0.44423E-02   0.33557E+00 
c  VelocityY    0.29405E+04    1914   0.44423E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1914   0.44423E-02   0.00000E+00 
c  Pressure     0.42794E+00    7110   0.32020E-01   0.20399E+00 
c  k            0.21952E+04    1077   0.81870E-04   0.10175E+01 
c  omega        0.12832E+08     213   0.40577E-04   0.31376E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9196e+05                             2
a  Local Time Step      1.1522e-05                         44366


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0677         0.97421     -5.9989e-05      1.3313e-06
v  Velocity[Y]                 -32.562          29.769          6.7289          20.056
v  Velocity[Z]                 -30.372          28.821         0.12369      0.00044568
v  ǁVelocityǁ                0.0094554          33.094          10.592          20.215
v  Pressure                    -402.08          348.21         -51.457          31.304
v  k                          3.14e-08          71.989           4.021          1.6883
v  omega                         1e-24      1.4588e+07          8330.7          11.883
v  turbulent_viscosity      5.3346e-15          1.2772        0.016045         0.11309
v  CourantNb                  0.022827          2029.8           44.47          1.3764
v  FourierNb                  0.010853           15617          93.783         0.70988
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14812         0.01082        0.045736


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90897           15664          138.25          2.0863


 TIME FOR THE TIME STEP              714:        0.44704E+02

===============================================================


 INSTANT    0.715000000E+02   TIME STEP NUMBER             715
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.254640967E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31299E+02 0.21920E+02
   Friction velocity        uet   :  0.55665E-03 0.27821E+01
   Friction velocity        uk    :  0.12034E-01 0.30789E+01
   Dimensionless distance   yplus :  0.89225E-01 0.28195E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        307
   Nb of faces within the viscous sub-layer     :       1043
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1851   0.44867E-02   0.32017E+00 
c  VelocityY    0.29404E+04    1851   0.44867E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1851   0.44867E-02   0.00000E+00 
c  Pressure     0.42371E+00    7074   0.32920E-01   0.20127E+00 
c  k            0.21920E+04    1255   0.97730E-04   0.88530E+00 
c  omega        0.10910E+08     402   0.31501E-04   0.19136E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -2255.1                             1
a  Local Time Step      1.0686e-05                         44309


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0292         0.99257      -0.0002143      2.9326e-06
v  Velocity[Y]                 -39.436          29.863          6.6793          20.056
v  Velocity[Z]                 -28.711          28.629         0.14974     -0.00023073
v  ǁVelocityǁ                 0.016423          41.612           10.59          20.215
v  Pressure                    -405.22           349.1         -51.973            31.6
v  k                        2.5127e-10          90.091          4.0581          1.6863
v  omega                         1e-24      1.1846e+07          8257.7          11.896
v  turbulent_viscosity      1.7223e-14          1.2825        0.015976         0.11298
v  CourantNb                  0.031077          2036.3          44.683          1.3765
v  FourierNb                  0.010854           15616          93.267         0.70891
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14905        0.010821        0.045743


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15671          137.95          2.0854


 TIME FOR THE TIME STEP              715:        0.44572E+02

===============================================================


 INSTANT    0.716000000E+02   TIME STEP NUMBER             716
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.656508503E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57301E+02 0.14035E+02
   Friction velocity        uet   :  0.78114E-03 0.36527E+01
   Friction velocity        uk    :  0.21628E-01 0.46083E+01
   Dimensionless distance   yplus :  0.74677E-01 0.36820E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        312
   Nb of faces within the viscous sub-layer     :       1041
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1797   0.44756E-02   0.31727E+00 
c  VelocityY    0.29405E+04    1797   0.44756E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1797   0.44756E-02   0.00000E+00 
c  Pressure     0.40951E+00    7032   0.36722E-01   0.19461E+00 
c  k            0.21852E+04    1424   0.99275E-04   0.72511E+00 
c  omega        0.10323E+08     438   0.88680E-04   0.71161E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9778e+05                             1
a  Local Time Step      1.0574e-05                         44291


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98337         0.97942     -0.00059837      2.0726e-06
v  Velocity[Y]                 -31.753          30.237          6.6714          20.056
v  Velocity[Z]                 -28.447          28.908         0.15774     -0.00081796
v  ǁVelocityǁ                0.0094752           33.34          10.572          20.215
v  Pressure                     -406.6          348.94         -52.929          31.934
v  k                        8.1353e-10          50.277          4.0519          1.6845
v  omega                         1e-24      3.8795e+07          8625.3          11.952
v  turbulent_viscosity        1.12e-15          1.2876        0.015936         0.11286
v  CourantNb                  0.044554          2126.6          44.921          1.3767
v  FourierNb                  0.010854           15629          93.105         0.70823
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14817         0.01082        0.045756


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15694          138.03          2.0849


 TIME FOR THE TIME STEP              716:        0.45130E+02

===============================================================


 INSTANT    0.717000000E+02   TIME STEP NUMBER             717
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.572645567E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30320E+02 0.14136E+02
   Friction velocity        uet   :  0.74270E-03 0.30751E+01
   Friction velocity        uk    :  0.15892E-01 0.31179E+01
   Dimensionless distance   yplus :  0.76253E-01 0.27557E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1794   0.45477E-02   0.31902E+00 
c  VelocityY    0.29406E+04    1794   0.45477E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1794   0.45477E-02   0.00000E+00 
c  Pressure     0.44726E+00    7127   0.37260E-01   0.21258E+00 
c  k            0.21789E+04    1473   0.59872E-04   0.60963E+00 
c  omega        0.15243E+08     317   0.48807E-04   0.13111E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -5561.3                             1
a  Local Time Step      1.1332e-05                         44262


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93355         0.85876     -0.00090553      3.0334e-06
v  Velocity[Y]                 -17.336          30.674           6.674          20.056
v  Velocity[Z]                 -28.578          28.804         0.14434      -0.0018035
v  ǁVelocityǁ                0.0091423          33.399          10.542          20.215
v  Pressure                    -407.47          347.95         -53.633           32.05
v  k                        1.4983e-09          44.788          4.0621          1.6826
v  omega                         1e-24      5.2829e+07          8626.4          11.933
v  turbulent_viscosity      1.0776e-15          1.2921        0.015929         0.11274
v  CourantNb                  0.041094          3132.8           45.12          1.3767
v  FourierNb                  0.010855           15612          92.161         0.70742
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14883         0.01082        0.045755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15685          137.28          2.0841


 TIME FOR THE TIME STEP              717:        0.45428E+02

===============================================================


 INSTANT    0.718000000E+02   TIME STEP NUMBER             718
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.418581382E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31875E+02 0.13966E+02
   Friction velocity        uet   :  0.31485E-02 0.28636E+01
   Friction velocity        uk    :  0.27575E-01 0.28389E+01
   Dimensionless distance   yplus :  0.16322E+00 0.27321E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1791   0.45255E-02   0.33692E+00 
c  VelocityY    0.29407E+04    1791   0.45255E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1791   0.45255E-02   0.00000E+00 
c  Pressure     0.42856E+00    7091   0.34470E-01   0.20175E+00 
c  k            0.21739E+04    1455   0.55899E-04   0.53562E+00 
c  omega        0.27001E+08     181   0.19124E-04   0.56837E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.153e-05                         44279


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8786         0.77372     -0.00070108       4.086e-06
v  Velocity[Y]                 -17.208          32.866          6.6874          20.056
v  Velocity[Z]                 -28.566          28.896         0.10579      -0.0024275
v  ǁVelocityǁ                 0.012901          33.925          10.508          20.215
v  Pressure                    -406.81          346.44         -53.743          31.968
v  k                        2.5815e-08          46.474          4.1048          1.6809
v  omega                         1e-24      2.6446e+07          8432.3          11.901
v  turbulent_viscosity      1.6951e-15          1.2971        0.015962         0.11261
v  CourantNb                  0.053649          2113.2          44.779          1.3765
v  FourierNb                  0.010855           15477          92.398         0.70711
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010819        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15555          137.18          2.0836


 TIME FOR THE TIME STEP              718:        0.44533E+02

===============================================================


 INSTANT    0.719000000E+02   TIME STEP NUMBER             719
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.232848629E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31856E+02 0.13718E+02
   Friction velocity        uet   :  0.66969E-03 0.29167E+01
   Friction velocity        uk    :  0.20239E-01 0.28506E+01
   Dimensionless distance   yplus :  0.11643E+00 0.30145E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        472
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1845   0.44465E-02   0.35899E+00 
c  VelocityY    0.29407E+04    1845   0.44465E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1845   0.44465E-02   0.00000E+00 
c  Pressure     0.44412E+00    6964   0.34189E-01   0.20973E+00 
c  k            0.21698E+04    1387   0.62547E-04   0.61622E+00 
c  omega        0.12469E+08     301   0.60503E-04   0.55046E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1548e-05                         44320


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.81578         0.72883      0.00033155      1.2266e-06
v  Velocity[Y]                 -16.062          33.644          6.7081          20.056
v  Velocity[Z]                  -28.81          28.782        0.054032      -0.0028103
v  ǁVelocityǁ                 0.010294          33.741          10.494          20.215
v  Pressure                    -400.17          345.99         -53.662           31.86
v  k                        7.8666e-08          54.905          4.1118          1.6793
v  omega                         1e-24      2.8735e+07          8437.3          11.902
v  turbulent_viscosity       2.242e-14          1.3009        0.015999         0.11248
v  CourantNb                  0.048158          2023.6          44.226          1.3763
v  FourierNb                  0.010855           15254          94.305         0.70717
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010819        0.045755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15335          138.53          2.0834


 TIME FOR THE TIME STEP              719:        0.44760E+02

===============================================================


 INSTANT    0.720000000E+02   TIME STEP NUMBER             720
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.361058878E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31581E+02 0.13981E+02
   Friction velocity        uet   :  0.12261E-02 0.28733E+01
   Friction velocity        uk    :  0.16264E-01 0.30732E+01
   Dimensionless distance   yplus :  0.12667E+00 0.33629E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1915   0.44582E-02   0.38829E+00 
c  VelocityY    0.29407E+04    1915   0.44582E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1915   0.44582E-02   0.00000E+00 
c  Pressure     0.44100E+00    6947   0.32435E-01   0.20895E+00 
c  k            0.21655E+04    1098   0.60330E-04   0.60218E+00 
c  omega        0.12258E+08     350   0.34210E-04   0.28512E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1055e-05                         44337


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79883         0.70886       0.0015615     -3.1253e-07
v  Velocity[Y]                  -15.35          33.621          6.7057          20.056
v  Velocity[Z]                 -29.382          28.938      -0.0065273       -0.003111
v  ǁVelocityǁ                0.0091725          34.138          10.496          20.215
v  Pressure                    -383.81          346.13         -53.993          31.276
v  k                         2.468e-08          43.094          4.0933          1.6778
v  omega                         1e-24       1.469e+07          8418.2           11.89
v  turbulent_viscosity       4.122e-14          1.3052        0.016001         0.11234
v  CourantNb                  0.023022          2052.3           43.97          1.3763
v  FourierNb                  0.010854           15292          94.915         0.70669
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14812        0.010819        0.045744


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15338          138.89          2.0829


 TIME FOR THE TIME STEP              720:        0.45249E+02

===============================================================


 INSTANT    0.721000000E+02   TIME STEP NUMBER             721
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.201936625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30620E+02 0.22565E+02
   Friction velocity        uet   :  0.53083E-03 0.27509E+01
   Friction velocity        uk    :  0.66758E-02 0.32537E+01
   Dimensionless distance   yplus :  0.91962E-01 0.37572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        458
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1964   0.44483E-02   0.40074E+00 
c  VelocityY    0.29407E+04    1964   0.44483E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1964   0.44483E-02   0.00000E+00 
c  Pressure     0.44293E+00    6986   0.30545E-01   0.20889E+00 
c  k            0.21612E+04    1244   0.53229E-04   0.60576E+00 
c  omega        0.10359E+08     314   0.36206E-04   0.16385E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -49125                             1
a  Local Time Step       1.201e-05                         44313


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89416          0.7632       0.0023648       -1.57e-06
v  Velocity[Y]                 -16.027          31.496          6.6803          20.056
v  Velocity[Z]                 -28.979          28.765       -0.042206      -0.0036667
v  ǁVelocityǁ                   0.0242          32.856          10.497          20.215
v  Pressure                    -371.17          346.64         -53.689          30.891
v  k                         4.352e-07          38.798          4.0775          1.6765
v  omega                         1e-24      1.1798e+07          8338.4          11.867
v  turbulent_viscosity       6.162e-15          1.3067        0.015985         0.11221
v  CourantNb                  0.014865          2073.7          43.872          1.3765
v  FourierNb                  0.010854           15396          94.687          0.7055
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14885         0.01082        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15452          138.56           2.082


 TIME FOR THE TIME STEP              721:        0.45605E+02

===============================================================


 INSTANT    0.722000000E+02   TIME STEP NUMBER             722
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.518854002E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31492E+02 0.20813E+02
   Friction velocity        uet   :  0.24088E-02 0.25287E+01
   Friction velocity        uk    :  0.28351E-01 0.28446E+01
   Dimensionless distance   yplus :  0.95612E-01 0.31415E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1936   0.44559E-02   0.41841E+00 
c  VelocityY    0.29407E+04    1936   0.44559E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1936   0.44559E-02   0.00000E+00 
c  Pressure     0.45500E+00    6980   0.29258E-01   0.21487E+00 
c  k            0.21580E+04    1427   0.55994E-04   0.70697E+00 
c  omega        0.10165E+08     253   0.29886E-04   0.79658E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.493e+05                             2
a  Local Time Step      1.2214e-05                         44291


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.9632         0.82003         0.00307     -1.5802e-06
v  Velocity[Y]                 -15.345          31.346          6.6764          20.056
v  Velocity[Z]                 -30.192          29.013       -0.062257      -0.0040437
v  ǁVelocityǁ                 0.018206          36.385          10.504          20.215
v  Pressure                    -351.94           347.1         -52.675           30.87
v  k                        1.0262e-07          48.698          4.0777          1.6756
v  omega                         1e-24      1.1809e+07          8188.7          11.853
v  turbulent_viscosity      5.8816e-14           1.308        0.015986         0.11208
v  CourantNb                  0.025671          2083.9          43.862          1.3766
v  FourierNb                  0.010852           15509          94.575         0.70452
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14873         0.01082        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15576          138.44          2.0811


 TIME FOR THE TIME STEP              722:        0.46669E+02

===============================================================


 INSTANT    0.723000000E+02   TIME STEP NUMBER             723
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.102670101E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31028E+02 0.21134E+02
   Friction velocity        uet   :  0.22632E-02 0.29987E+01
   Friction velocity        uk    :  0.18285E-01 0.28838E+01
   Dimensionless distance   yplus :  0.12290E+00 0.27500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        506
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1899   0.44188E-02   0.42370E+00 
c  VelocityY    0.29407E+04    1899   0.44188E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1899   0.44188E-02   0.00000E+00 
c  Pressure     0.41487E+00    7091   0.31258E-01   0.19607E+00 
c  k            0.21572E+04    1484   0.64497E-04   0.85252E+00 
c  omega        0.10049E+08     241   0.28492E-03   0.48686E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1363e+05                             2
a  Local Time Step      1.2262e-05                         44342


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.99555         0.90328       0.0034011     -2.9268e-07
v  Velocity[Y]                 -15.134          32.827          6.6945          20.057
v  Velocity[Z]                 -31.914          28.812       -0.083398      -0.0044051
v  ǁVelocityǁ                 0.013516           36.82          10.528          20.216
v  Pressure                    -391.92          347.57         -51.238          31.141
v  k                        2.3872e-08          59.193          4.0881          1.6749
v  omega                         1e-24      3.5065e+08          9096.4          12.003
v  turbulent_viscosity      2.3524e-13          1.3073        0.016027         0.11195
v  CourantNb                  0.026111          2078.9          43.959          1.3766
v  FourierNb                  0.010851           15522          93.817         0.70387
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14806        0.010819        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15597          137.78          2.0805


 TIME FOR THE TIME STEP              723:        0.45574E+02

===============================================================


 INSTANT    0.724000000E+02   TIME STEP NUMBER             724
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.844979720E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30387E+02 0.19043E+02
   Friction velocity        uet   :  0.64766E-03 0.31656E+01
   Friction velocity        uk    :  0.27293E-01 0.30778E+01
   Dimensionless distance   yplus :  0.18337E+00 0.27259E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1763   0.43783E-02   0.43468E+00 
c  VelocityY    0.29407E+04    1763   0.43783E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1763   0.43783E-02   0.00000E+00 
c  Pressure     0.41618E+00    7058   0.35952E-01   0.19596E+00 
c  k            0.21618E+04    1462   0.72817E-04   0.97903E+00 
c  omega        0.14538E+10      60   0.87803E-06   0.12246E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6909e+05                             2
a  Local Time Step      1.1577e-05                         44322


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98822          1.0764       0.0033376      2.5891e-06
v  Velocity[Y]                 -14.578           33.02          6.7353          20.057
v  Velocity[Z]                 -32.611          29.024       -0.077078      -0.0043943
v  ǁVelocityǁ                 0.013503          35.246          10.569          20.216
v  Pressure                    -432.78          346.83         -50.659          31.274
v  k                        3.6423e-07          65.725          4.0793          1.6745
v  omega                         1e-24      1.7532e+08          8511.2          11.919
v  turbulent_viscosity      1.1459e-14          1.3064        0.016065         0.11183
v  CourantNb                  0.040708          2395.2          43.909          1.3766
v  FourierNb                  0.010851           15500          93.381         0.70325
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14882        0.010818        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15543          137.29          2.0798


 TIME FOR THE TIME STEP              724:        0.43647E+02

===============================================================


 INSTANT    0.725000000E+02   TIME STEP NUMBER             725
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.344960620E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31671E+02 0.16569E+02
   Friction velocity        uet   :  0.29375E-02 0.32316E+01
   Friction velocity        uk    :  0.26882E-01 0.32110E+01
   Dimensionless distance   yplus :  0.12473E+00 0.27789E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1789   0.46210E-02   0.44935E+00 
c  VelocityY    0.29407E+04    1789   0.46210E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1789   0.46210E-02   0.00000E+00 
c  Pressure     0.43865E+00    7051   0.38315E-01   0.20711E+00 
c  k            0.21720E+04    1364   0.75271E-04   0.10421E+01 
c  omega        0.65502E+18       2   0.64687E-13   0.45751E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.641e+05                             3
a  Local Time Step        1.23e-05                         44317


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97914          1.2686       0.0031453      3.7834e-06
v  Velocity[Y]                 -18.681          30.134          6.7754          20.057
v  Velocity[Z]                 -33.185          28.655       -0.028828      -0.0040317
v  ǁVelocityǁ                0.0086429          34.888          10.592          20.215
v  Pressure                     -449.2          347.62         -50.387          31.448
v  k                        8.9343e-08          64.686          4.0491          1.6741
v  omega                         1e-24      8.7654e+07          8708.2          11.918
v  turbulent_viscosity      6.5647e-14          1.3048        0.016065         0.11172
v  CourantNb                  0.042565          2760.3          43.936          1.3765
v  FourierNb                  0.010851           15692          93.201         0.70244
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14797        0.010819        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99701           15734          137.14          2.0789


 TIME FOR THE TIME STEP              725:        0.44603E+02

===============================================================


 INSTANT    0.726000000E+02   TIME STEP NUMBER             726
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.109366429E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31217E+02 0.15592E+02
   Friction velocity        uet   :  0.16949E-02 0.30001E+01
   Friction velocity        uk    :  0.21720E-01 0.32711E+01
   Dimensionless distance   yplus :  0.11379E+00 0.28245E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1874   0.44698E-02   0.43907E+00 
c  VelocityY    0.29407E+04    1874   0.44698E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1874   0.44698E-02   0.00000E+00 
c  Pressure     0.44129E+00    7090   0.36217E-01   0.20877E+00 
c  k            0.21828E+04    1148   0.75101E-04   0.11576E+01 
c  omega        0.94668E+08     129   0.14471E-04   0.12860E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2254e+05                             2
a  Local Time Step      1.2001e-05                         44337


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90068          1.3749       0.0024868      1.8871e-06
v  Velocity[Y]                 -23.697          29.964          6.7745          20.056
v  Velocity[Z]                 -33.346          28.715        0.019382      -0.0040146
v  ǁVelocityǁ                 0.011703          34.362          10.578          20.215
v  Pressure                    -443.45          349.11         -50.274          31.429
v  k                        2.8529e-08           52.66          3.9974          1.6737
v  omega                         1e-24      4.3827e+07          8267.5          11.895
v  turbulent_viscosity       2.231e-14          1.3046        0.016041         0.11162
v  CourantNb                  0.037626          2565.6           44.08          1.3765
v  FourierNb                  0.010851           15784          93.262         0.70161
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14856        0.010819         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0091           15830          137.34          2.0781


 TIME FOR THE TIME STEP              726:        0.44418E+02

===============================================================


 INSTANT    0.727000000E+02   TIME STEP NUMBER             727
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.376601635E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30969E+02 0.14021E+02
   Friction velocity        uet   :  0.15541E-02 0.29198E+01
   Friction velocity        uk    :  0.92334E-02 0.28384E+01
   Dimensionless distance   yplus :  0.38520E-01 0.28312E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        391
   Nb of faces within the viscous sub-layer     :        969
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1774   0.46261E-02   0.40721E+00 
c  VelocityY    0.29407E+04    1774   0.46261E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1774   0.46261E-02   0.00000E+00 
c  Pressure     0.42700E+00    7066   0.32091E-01   0.20223E+00 
c  k            0.21915E+04    1355   0.71794E-04   0.10632E+01 
c  omega        0.25718E+08     183   0.37839E-04   0.61845E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -48372                             1
a  Local Time Step      1.1531e-05                         44351


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.76948          1.3042      0.00099046      1.3875e-06
v  Velocity[Y]                  -34.42          29.813          6.7152          20.056
v  Velocity[Z]                 -29.929          28.698        0.053831      -0.0036027
v  ǁVelocityǁ                 0.022247          34.441          10.563          20.214
v  Pressure                    -421.61          350.77         -49.979          31.492
v  k                        2.0291e-07          60.279          3.9674          1.6734
v  omega                         1e-24      2.2926e+07          8280.9          11.886
v  turbulent_viscosity      2.4597e-14          1.3023        0.015958         0.11154
v  CourantNb                  0.011984          2022.5          44.317          1.3766
v  FourierNb                  0.010852           15687          92.507         0.70046
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010819        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15742          136.82           2.077


 TIME FOR THE TIME STEP              727:        0.43494E+02

===============================================================


 INSTANT    0.728000000E+02   TIME STEP NUMBER             728
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.205094106E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31141E+02 0.23839E+02
   Friction velocity        uet   :  0.18505E-02 0.31316E+01
   Friction velocity        uk    :  0.20825E-01 0.28930E+01
   Dimensionless distance   yplus :  0.11461E+00 0.28255E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1645   0.46565E-02   0.38530E+00 
c  VelocityY    0.29407E+04    1645   0.46565E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1645   0.46565E-02   0.00000E+00 
c  Pressure     0.42664E+00    7041   0.32021E-01   0.20158E+00 
c  k            0.21919E+04    1450   0.89150E-04   0.93629E+00 
c  omega        0.11970E+08     357   0.37931E-04   0.29480E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2706e+05                             1
a  Local Time Step      1.1323e-05                         44350


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.69968          1.1335     -0.00025319       2.083e-06
v  Velocity[Y]                 -28.023          29.869          6.6404          20.056
v  Velocity[Z]                 -28.539          28.793        0.063993      -0.0030645
v  ǁVelocityǁ                 0.012405          36.803           10.57          20.214
v  Pressure                    -410.02          350.49         -50.783          31.455
v  k                        9.3966e-09          98.684          4.0123          1.6731
v  omega                         1e-24      1.4181e+07          8047.9          11.872
v  turbulent_viscosity      2.5696e-13          1.2993        0.015904         0.11147
v  CourantNb                  0.036845          2025.8            44.4          1.3765
v  FourierNb                  0.010852           15529          92.221         0.69987
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010819        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15594          136.62          2.0763


 TIME FOR THE TIME STEP              728:        0.43074E+02

===============================================================


 INSTANT    0.729000000E+02   TIME STEP NUMBER             729
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.347849225E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.45499E+02 0.17279E+02
   Friction velocity        uet   :  0.83661E-03 0.31758E+01
   Friction velocity        uk    :  0.27275E-01 0.38438E+01
   Dimensionless distance   yplus :  0.11163E+00 0.34475E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :       1063
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1674   0.45053E-02   0.37935E+00 
c  VelocityY    0.29408E+04    1674   0.45053E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1674   0.45053E-02   0.00000E+00 
c  Pressure     0.42753E+00    7039   0.36936E-01   0.20374E+00 
c  k            0.21863E+04    1459   0.12509E-03   0.77959E+00 
c  omega        0.10251E+08     522   0.11029E-03   0.83630E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5231e+05                             1
a  Local Time Step       1.094e-05                         44338


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.73626         0.95303     -0.00064259      1.5708e-06
v  Velocity[Y]                 -35.474          30.135          6.6304          20.056
v  Velocity[Z]                 -28.632          28.495        0.074577      -0.0025276
v  ǁVelocityǁ                 0.018362          36.398          10.571          20.215
v  Pressure                    -410.74          349.34         -52.224          31.638
v  k                        4.2693e-09           87.45          4.0654          1.6731
v  omega                         1e-24      4.2179e+07          8486.9          11.927
v  turbulent_viscosity      4.3258e-14          1.2974        0.015875         0.11141
v  CourantNb                  0.052551          2010.3          44.567          1.3765
v  FourierNb                  0.010852           15469          92.364         0.69985
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14922        0.010819        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15542          136.93          2.0763


 TIME FOR THE TIME STEP              729:        0.43421E+02

===============================================================


 INSTANT    0.730000000E+02   TIME STEP NUMBER             730
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.620217277E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37994E+02 0.13893E+02
   Friction velocity        uet   :  0.18306E-02 0.33877E+01
   Friction velocity        uk    :  0.27961E-01 0.37867E+01
   Dimensionless distance   yplus :  0.11846E+00 0.36521E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :       1064
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1668   0.45700E-02   0.37892E+00 
c  VelocityY    0.29407E+04    1668   0.45700E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1668   0.45700E-02   0.00000E+00 
c  Pressure     0.43893E+00    7117   0.39441E-01   0.20845E+00 
c  k            0.21791E+04    1395   0.10021E-03   0.68281E+00 
c  omega        0.13959E+08     381   0.41285E-03   0.12163E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.819e+05                             2
a  Local Time Step      1.0585e-05                         44325


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79452         0.87447      0.00020168      4.5719e-07
v  Velocity[Y]                  -19.74          30.721          6.6526          20.056
v  Velocity[Z]                  -28.65          28.772        0.070798      -0.0021647
v  ǁVelocityǁ                 0.015274          33.503          10.561          20.216
v  Pressure                    -411.23          347.36         -53.962          31.695
v  k                        2.1707e-09          50.052          4.0841          1.6732
v  omega                         1e-24      1.9632e+08           10715          12.074
v  turbulent_viscosity      1.6325e-14          1.2933        0.015876         0.11137
v  CourantNb                   0.01177          3061.8          44.802          1.3765
v  FourierNb                  0.010852           15399          92.198         0.69997
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14828        0.010819        0.045681


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15477             137          2.0765


 TIME FOR THE TIME STEP              730:        0.43881E+02

===============================================================


 INSTANT    0.731000000E+02   TIME STEP NUMBER             731
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.479378627E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30261E+02 0.13653E+02
   Friction velocity        uet   :  0.14432E-02 0.26280E+01
   Friction velocity        uk    :  0.24282E-01 0.31154E+01
   Dimensionless distance   yplus :  0.13223E+00 0.28230E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        545
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1932   0.44617E-02   0.38553E+00 
c  VelocityY    0.29407E+04    1932   0.44617E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1932   0.44617E-02   0.00000E+00 
c  Pressure     0.42731E+00    7127   0.36120E-01   0.20293E+00 
c  k            0.21730E+04    1264   0.66277E-04   0.55323E+00 
c  omega        0.17918E+09     120   0.16261E-04   0.34196E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1156e+05                             2
a  Local Time Step      1.1554e-05                         44282


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.87754         0.85157       0.0010117     -1.7629e-06
v  Velocity[Y]                 -17.634          31.746          6.6864          20.056
v  Velocity[Z]                 -28.988           28.83        0.049375      -0.0014524
v  ǁVelocityǁ                 0.010134          33.875          10.544          20.215
v  Pressure                    -410.88           347.3         -54.886          31.699
v  k                        2.6662e-08          47.969          4.1329          1.6735
v  omega                         1e-24      9.8439e+07          9398.2          11.961
v  turbulent_viscosity      1.4847e-15           1.289        0.015895         0.11134
v  CourantNb                  0.048613          2481.2          44.644          1.3764
v  FourierNb                  0.010852           15228          93.105         0.70042
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14857        0.010819        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.83918           15307          137.75          2.0768


 TIME FOR THE TIME STEP              731:        0.45051E+02

===============================================================


 INSTANT    0.732000000E+02   TIME STEP NUMBER             732
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.719319073E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31153E+02 0.13384E+02
   Friction velocity        uet   :  0.18874E-02 0.28955E+01
   Friction velocity        uk    :  0.75048E-02 0.29559E+01
   Dimensionless distance   yplus :  0.65867E-01 0.28882E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        596
   Nb of faces within the viscous sub-layer     :       1066
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1925   0.46974E-02   0.40055E+00 
c  VelocityY    0.29407E+04    1925   0.46974E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1925   0.46974E-02   0.00000E+00 
c  Pressure     0.43551E+00    7070   0.31564E-01   0.20706E+00 
c  k            0.21684E+04    1074   0.71202E-04   0.61720E+00 
c  omega        0.47186E+08     329   0.28560E-04   0.92205E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.2584e+05                             3
a  Local Time Step      1.1422e-05                         44249


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93421         0.90273       0.0012875     -2.1412e-06
v  Velocity[Y]                 -16.323           33.23          6.7236          20.057
v  Velocity[Z]                 -29.122          29.395        0.019251       -0.001161
v  ǁVelocityǁ                0.0070193          33.672           10.52          20.216
v  Pressure                    -407.28          348.37         -55.059          31.655
v  k                         1.944e-08          51.993           4.147          1.6739
v  omega                         1e-24      4.9816e+07          8687.8          11.899
v  turbulent_viscosity      2.3779e-14          1.2858        0.015918         0.11133
v  CourantNb                  0.016882          2002.3          44.398          1.3764
v  FourierNb                  0.010853           15325          95.696         0.70143
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14796         0.01082        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15370          140.09          2.0778


 TIME FOR THE TIME STEP              732:        0.44918E+02

===============================================================


 INSTANT    0.733000000E+02   TIME STEP NUMBER             733
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.278745393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31401E+02 0.16184E+02
   Friction velocity        uet   :  0.14879E-02 0.29087E+01
   Friction velocity        uk    :  0.16768E-01 0.31723E+01
   Dimensionless distance   yplus :  0.41722E-01 0.32304E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        542
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1848   0.44914E-02   0.41757E+00 
c  VelocityY    0.29406E+04    1848   0.44914E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1848   0.44914E-02   0.00000E+00 
c  Pressure     0.44600E+00    6988   0.31233E-01   0.21291E+00 
c  k            0.21623E+04    1299   0.63897E-04   0.62040E+00 
c  omega        0.15823E+08     358   0.45228E-04   0.29604E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -68548                             1
a  Local Time Step      1.1064e-05                         44226


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95111         0.93006      0.00071921      1.8169e-07
v  Velocity[Y]                 -15.093          33.315          6.7244          20.057
v  Velocity[Z]                 -29.184          28.783       -0.010388     -0.00093425
v  ǁVelocityǁ                 0.011901          33.362          10.517          20.215
v  Pressure                    -393.57          347.93         -55.745          31.212
v  k                        4.9903e-08           43.57          4.1286          1.6743
v  omega                         1e-24      2.6145e+07          8311.3          11.865
v  turbulent_viscosity      1.4157e-15          1.2823        0.015924         0.11133
v  CourantNb                  0.060077          2016.1          44.173          1.3765
v  FourierNb                  0.010854           15371          96.675          0.7021
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14819        0.010821        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15426          140.85          2.0786


 TIME FOR THE TIME STEP              733:        0.44601E+02

===============================================================


 INSTANT    0.734000000E+02   TIME STEP NUMBER             734
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.216859460E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31464E+02 0.21076E+02
   Friction velocity        uet   :  0.20921E-02 0.27955E+01
   Friction velocity        uk    :  0.14577E-01 0.32861E+01
   Dimensionless distance   yplus :  0.80089E-01 0.41302E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        515
   Nb of faces within the viscous sub-layer     :        962
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1818   0.45976E-02   0.42412E+00 
c  VelocityY    0.29405E+04    1818   0.45976E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1818   0.45976E-02   0.00000E+00 
c  Pressure     0.42545E+00    6953   0.30755E-01   0.20185E+00 
c  k            0.21567E+04    1445   0.53930E-04   0.57182E+00 
c  omega        0.10770E+08     308   0.39919E-04   0.17095E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3974e+05                             2
a  Local Time Step       1.169e-05                         44189


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94994         0.92271     -0.00065247     -3.7704e-07
v  Velocity[Y]                 -15.262          33.048          6.7078          20.056
v  Velocity[Z]                 -28.597          28.779       -0.028221     -0.00055919
v  ǁVelocityǁ                 0.018486          33.412          10.512          20.215
v  Pressure                    -379.66           347.2         -56.023          30.714
v  k                        1.1869e-09          37.531          4.1113          1.6748
v  omega                         1e-24      1.5469e+07          8290.5           11.86
v  turbulent_viscosity      5.9204e-15          1.2786        0.015921         0.11134
v  CourantNb                  0.050049          2017.9          43.995          1.3767
v  FourierNb                  0.010855           15400           96.08         0.70227
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14906        0.010822        0.045738


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15466          140.07           2.079


 TIME FOR THE TIME STEP              734:        0.44860E+02

===============================================================


 INSTANT    0.735000000E+02   TIME STEP NUMBER             735
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.109239589E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31879E+02 0.20578E+02
   Friction velocity        uet   :  0.39332E-02 0.26728E+01
   Friction velocity        uk    :  0.20042E-01 0.31665E+01
   Dimensionless distance   yplus :  0.14882E+00 0.31145E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        500
   Nb of faces within the viscous sub-layer     :        927
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1857   0.45187E-02   0.42897E+00 
c  VelocityY    0.29404E+04    1857   0.45187E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1857   0.45187E-02   0.00000E+00 
c  Pressure     0.43986E+00    6978   0.29215E-01   0.20844E+00 
c  k            0.21523E+04    1454   0.54677E-04   0.63600E+00 
c  omega        0.10301E+08     253   0.28133E-04   0.15565E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1536e+05                             1
a  Local Time Step      1.1937e-05                         44144


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94492         0.86392       -0.001599      1.5894e-06
v  Velocity[Y]                 -15.234          30.409          6.7117          20.056
v  Velocity[Z]                 -30.448          28.937       -0.032884      -0.0003452
v  ǁVelocityǁ                  0.01204          35.444          10.517          20.214
v  Pressure                    -361.09          347.52         -54.844          30.927
v  k                        1.8829e-07          41.368          4.0763          1.6754
v  omega                         1e-24      1.3994e+07            8137          11.845
v  turbulent_viscosity      3.0231e-15          1.2752         0.01593         0.11136
v  CourantNb                  0.060265          2010.1          44.071          1.3771
v  FourierNb                  0.010856           15338          96.035         0.70242
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14864        0.010823        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15413          140.11          2.0795


 TIME FOR THE TIME STEP              735:        0.44625E+02

===============================================================


 INSTANT    0.736000000E+02   TIME STEP NUMBER             736
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.918896620E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31096E+02 0.20398E+02
   Friction velocity        uet   :  0.15283E-02 0.29055E+01
   Friction velocity        uk    :  0.24827E-01 0.30062E+01
   Dimensionless distance   yplus :  0.17003E+00 0.27739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1936   0.45292E-02   0.41724E+00 
c  VelocityY    0.29403E+04    1936   0.45292E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1936   0.45292E-02   0.00000E+00 
c  Pressure     0.44432E+00    7027   0.29843E-01   0.21042E+00 
c  k            0.21496E+04    1418   0.58074E-04   0.77673E+00 
c  omega        0.10304E+08     230   0.27318E-04   0.97027E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -3.464e+05                             2
a  Local Time Step       1.182e-05                         44133


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95219         0.90329      -0.0017727      6.3955e-07
v  Velocity[Y]                 -15.245          30.384          6.7404          20.056
v  Velocity[Z]                 -31.818          28.701       -0.031786      0.00022105
v  ǁVelocityǁ                0.0089701          36.761          10.547          20.215
v  Pressure                    -368.15          347.65         -53.319          31.282
v  k                         1.242e-08          52.413          4.0446           1.676
v  omega                         1e-24      1.1789e+07          8038.7          11.834
v  turbulent_viscosity      9.9701e-14          1.2723        0.015927         0.11138
v  CourantNb                  0.041174          1998.8          44.135           1.377
v  FourierNb                  0.010857           15215          94.307         0.70188
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14904        0.010822        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15297          138.44          2.0789


 TIME FOR THE TIME STEP              736:        0.45833E+02

===============================================================


 INSTANT    0.737000000E+02   TIME STEP NUMBER             737
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.595657689E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30410E+02 0.15342E+02
   Friction velocity        uet   :  0.18622E-02 0.31191E+01
   Friction velocity        uk    :  0.17590E-01 0.30911E+01
   Dimensionless distance   yplus :  0.10640E+00 0.28033E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    2010   0.45666E-02   0.40900E+00 
c  VelocityY    0.29404E+04    2010   0.45666E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    2010   0.45666E-02   0.00000E+00 
c  Pressure     0.43938E+00    7119   0.34255E-01   0.20778E+00 
c  k            0.21512E+04    1281   0.66134E-04   0.91321E+00 
c  omega        0.10210E+08     231   0.35641E-04   0.72084E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -13865                             1
a  Local Time Step      1.1482e-05                         44149


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.132         0.94971      -0.0013652     -1.3635e-06
v  Velocity[Y]                 -15.167           30.83          6.7926          20.056
v  Velocity[Z]                 -33.145          28.871      -0.0061085      0.00080939
v  ǁVelocityǁ                0.0033153          36.882          10.608          20.214
v  Pressure                     -421.4          349.13         -51.987          31.602
v  k                        6.0533e-09           64.07          4.0232          1.6767
v  omega                         1e-24       1.172e+07          7960.3          11.838
v  turbulent_viscosity        5.26e-15          1.2693        0.015912         0.11142
v  CourantNb                  0.043485          2145.8          44.155          1.3768
v  FourierNb                  0.010859           15295          93.738         0.70142
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010822        0.045743


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15340          137.89          2.0782


 TIME FOR THE TIME STEP              737:        0.46777E+02

===============================================================


 INSTANT    0.738000000E+02   TIME STEP NUMBER             738
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.610629257E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31714E+02 0.14018E+02
   Friction velocity        uet   :  0.14433E-02 0.31616E+01
   Friction velocity        uk    :  0.17862E-01 0.30500E+01
   Dimensionless distance   yplus :  0.78676E-01 0.28150E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :        977
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2056   0.46822E-02   0.41091E+00 
c  VelocityY    0.29405E+04    2056   0.46822E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2056   0.46822E-02   0.00000E+00 
c  Pressure     0.44055E+00    7142   0.37844E-01   0.20703E+00 
c  k            0.21587E+04    1091   0.67061E-04   0.96940E+00 
c  omega        0.99928E+07     241   0.14263E-03   0.59911E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8586e+05                             2
a  Local Time Step      1.2035e-05                         44201


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.241          0.8589     -0.00039606     -5.9159e-06
v  Velocity[Y]                 -16.036          30.136           6.855          20.056
v  Velocity[Z]                 -32.504          28.694        0.046772       0.0012419
v  ǁVelocityǁ                 0.016447           34.36          10.661          20.214
v  Pressure                    -442.97          350.46         -51.294          31.769
v  k                        1.1536e-08           66.75          4.0012          1.6773
v  omega                         1e-24       5.734e+07          8123.2          11.839
v  turbulent_viscosity      4.7985e-15          1.2663        0.015885         0.11146
v  CourantNb                  0.024951          2697.6          44.462          1.3767
v  FourierNb                   0.01086           15344          93.277           0.701
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869        0.010822        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99983           15395          137.74          2.0777


 TIME FOR THE TIME STEP              738:        0.46484E+02

===============================================================


 INSTANT    0.739000000E+02   TIME STEP NUMBER             739
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.174558800E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30557E+02 0.14300E+02
   Friction velocity        uet   :  0.12757E-02 0.29534E+01
   Friction velocity        uk    :  0.19618E-01 0.31504E+01
   Dimensionless distance   yplus :  0.10383E+00 0.28136E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        368
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2049   0.45061E-02   0.39040E+00 
c  VelocityY    0.29405E+04    2049   0.45061E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2049   0.45061E-02   0.00000E+00 
c  Pressure     0.43810E+00    6774   0.37512E-01   0.20675E+00 
c  k            0.21691E+04    1384   0.69731E-04   0.10067E+01 
c  omega        0.17117E+08     239   0.11588E-03   0.11284E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.618e+05                             3
a  Local Time Step      1.2124e-05                         44234


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1981         0.88385       0.0012207     -8.9224e-06
v  Velocity[Y]                 -24.526          29.928           6.871          20.056
v  Velocity[Z]                 -31.558          28.745         0.11611       0.0013975
v  ǁVelocityǁ                 0.015601          32.938          10.657          20.214
v  Pressure                    -441.02          351.27         -50.846           32.04
v  k                        1.9126e-08          58.257          3.9638          1.6777
v  omega                         1e-24      7.4494e+07          8367.5          11.885
v  turbulent_viscosity      1.8845e-14           1.263        0.015853          0.1115
v  CourantNb                  0.041064          2657.5          44.807          1.3768
v  FourierNb                  0.010862           15321           92.96         0.70065
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14884        0.010823        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91376           15380          137.77          2.0775


 TIME FOR THE TIME STEP              739:        0.45989E+02

===============================================================


 INSTANT    0.740000000E+02   TIME STEP NUMBER             740
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.160203742E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31413E+02 0.14555E+02
   Friction velocity        uet   :  0.10608E-02 0.27987E+01
   Friction velocity        uk    :  0.23427E-01 0.31628E+01
   Dimensionless distance   yplus :  0.12630E+00 0.27899E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        352
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2030   0.47068E-02   0.34389E+00 
c  VelocityY    0.29405E+04    2030   0.47068E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2030   0.47068E-02   0.00000E+00 
c  Pressure     0.45856E+00    7088   0.33716E-01   0.21736E+00 
c  k            0.21780E+04    1452   0.70833E-04   0.10221E+01 
c  omega        0.29058E+08     151   0.43393E-04   0.62413E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8235e+05                             2
a  Local Time Step      1.2054e-05                         44277


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0844         0.87282       0.0026377     -8.6916e-06
v  Velocity[Y]                 -29.421           29.77          6.8153          20.056
v  Velocity[Z]                 -31.148          28.901         0.16998       0.0014083
v  ǁVelocityǁ                0.0068287          32.862          10.613          20.214
v  Pressure                    -422.25          351.26         -50.554          32.078
v  k                        1.1127e-08           57.08          3.9393          1.6778
v  omega                         1e-24      3.7982e+07          8332.2          11.869
v  turbulent_viscosity      2.2389e-14          1.2611        0.015799         0.11154
v  CourantNb                  0.052342          2078.7          44.979           1.377
v  FourierNb                  0.010863           15205           92.05         0.70006
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010823        0.045749


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15273          137.03           2.077


 TIME FOR THE TIME STEP              740:        0.46173E+02

===============================================================


 INSTANT    0.741000000E+02   TIME STEP NUMBER             741
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.248875725E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31328E+02 0.20868E+02
   Friction velocity        uet   :  0.14201E-02 0.27526E+01
   Friction velocity        uk    :  0.11385E-01 0.28917E+01
   Dimensionless distance   yplus :  0.14119E+00 0.27424E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        296
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1995   0.46616E-02   0.31175E+00 
c  VelocityY    0.29406E+04    1995   0.46616E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1995   0.46616E-02   0.00000E+00 
c  Pressure     0.45712E+00    7075   0.31247E-01   0.21618E+00 
c  k            0.21809E+04    1448   0.90089E-04   0.92472E+00 
c  omega        0.14379E+08     253   0.16113E-03   0.17483E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6417e+05                             2
a  Local Time Step      1.1478e-05                         44296


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0911         0.81741         0.00368     -7.0563e-06
v  Velocity[Y]                 -22.407          29.655            6.73          20.056
v  Velocity[Z]                 -29.646          28.683         0.18645       0.0012364
v  ǁVelocityǁ                 0.011011          32.977          10.603          20.214
v  Pressure                    -400.17          349.87         -50.834          32.073
v  k                        5.6487e-09          87.125          3.9763          1.6777
v  omega                         1e-24      1.0206e+08          8599.6          11.907
v  turbulent_viscosity      3.4504e-14          1.2602        0.015757         0.11159
v  CourantNb                  0.028969          2070.5          44.926          1.3769
v  FourierNb                  0.010865           14996          91.833         0.69996
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14882        0.010823        0.045738


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15071          136.76          2.0769


 TIME FOR THE TIME STEP              741:        0.45303E+02

===============================================================


 INSTANT    0.742000000E+02   TIME STEP NUMBER             742
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.320947004E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31616E+02 0.17003E+02
   Friction velocity        uet   :  0.75673E-03 0.25155E+01
   Friction velocity        uk    :  0.24448E-01 0.33038E+01
   Dimensionless distance   yplus :  0.15137E+00 0.30631E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        347
   Nb of faces within the viscous sub-layer     :       1113
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1971   0.47090E-02   0.30167E+00 
c  VelocityY    0.29407E+04    1971   0.47090E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1971   0.47090E-02   0.00000E+00 
c  Pressure     0.46038E+00    7061   0.33743E-01   0.21852E+00 
c  k            0.21768E+04    1375   0.10363E-03   0.76885E+00 
c  omega        0.42388E+08     303   0.27422E-04   0.86843E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7333e+05                             2
a  Local Time Step      1.0364e-05                         44285


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0282         0.72783       0.0048497     -2.3656e-06
v  Velocity[Y]                 -38.412          30.083          6.6908          20.056
v  Velocity[Z]                 -28.663          28.622         0.19295       0.0011371
v  ǁVelocityǁ                0.0069868          38.763           10.59          20.215
v  Pressure                    -403.37          347.93         -51.619          32.296
v  k                        8.6339e-10          86.933          4.0236          1.6776
v  omega                         1e-24      5.1619e+07          8637.8          11.956
v  turbulent_viscosity      7.0534e-15          1.2599        0.015736         0.11162
v  CourantNb                  0.033785          2049.6          44.964          1.3769
v  FourierNb                  0.010867           14995           91.78         0.70033
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010824        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15036          136.74          2.0772


 TIME FOR THE TIME STEP              742:        0.46523E+02

===============================================================


 INSTANT    0.743000000E+02   TIME STEP NUMBER             743
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.244962623E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.43595E+02 0.14502E+02
   Friction velocity        uet   :  0.39492E-02 0.35760E+01
   Friction velocity        uk    :  0.20588E-01 0.37604E+01
   Dimensionless distance   yplus :  0.12774E+00 0.36557E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        391
   Nb of faces within the viscous sub-layer     :       1113
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    2008   0.45359E-02   0.29603E+00 
c  VelocityY    0.29408E+04    2008   0.45359E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    2008   0.45359E-02   0.00000E+00 
c  Pressure     0.45852E+00    7144   0.37881E-01   0.21814E+00 
c  k            0.21705E+04    1262   0.10049E-03   0.66941E+00 
c  omega        0.15598E+08     335   0.87586E-04   0.85524E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3545e+05                             2
a  Local Time Step      1.1114e-05                         44238


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92161         0.68518       0.0062376     -8.8032e-07
v  Velocity[Y]                 -24.926          30.519            6.68          20.057
v  Velocity[Z]                 -28.616          28.623         0.18034      0.00087927
v  ǁVelocityǁ                0.0095943          33.489          10.563          20.216
v  Pressure                    -405.57          347.56         -52.754          32.471
v  k                        4.4257e-10          40.759          4.0325          1.6774
v  omega                         1e-24      4.3024e+07          8763.3          11.951
v  turbulent_viscosity      3.7428e-15          1.2616        0.015745         0.11166
v  CourantNb                  0.021867          3126.6          45.238          1.3769
v  FourierNb                  0.010869           15001          91.361         0.70068
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14894        0.010825        0.045736


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15043           136.6          2.0776


 TIME FOR THE TIME STEP              743:        0.46577E+02

===============================================================


 INSTANT    0.744000000E+02   TIME STEP NUMBER             744
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.645233303E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30602E+02 0.14097E+02
   Friction velocity        uet   :  0.99154E-03 0.28361E+01
   Friction velocity        uk    :  0.14380E-01 0.27868E+01
   Dimensionless distance   yplus :  0.33601E-01 0.28418E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :       1070
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    2081   0.45600E-02   0.29969E+00 
c  VelocityY    0.29408E+04    2081   0.45600E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    2081   0.45600E-02   0.00000E+00 
c  Pressure     0.42448E+00    7152   0.38411E-01   0.20151E+00 
c  k            0.21649E+04    1260   0.57168E-04   0.51015E+00 
c  omega        0.14538E+08     266   0.81281E-04   0.93127E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -19201                             1
a  Local Time Step      1.1133e-05                         44231


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.75563         0.68556       0.0073877       2.389e-06
v  Velocity[Y]                 -17.367          32.174          6.6848          20.057
v  Velocity[Z]                 -29.282          28.799         0.14407      0.00031642
v  ǁVelocityǁ                0.0088338          33.556          10.526          20.216
v  Pressure                    -406.66          347.75         -53.539           32.33
v  k                        2.7488e-08          48.319          4.0854           1.677
v  omega                         1e-24      5.2379e+07          8542.9          11.925
v  turbulent_viscosity      2.2381e-16          1.2655        0.015777         0.11169
v  CourantNb                  0.041726          2837.5          45.058          1.3766
v  FourierNb                  0.010869           15058          91.601         0.70132
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14919        0.010825        0.045778


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15106          136.66           2.078


 TIME FOR THE TIME STEP              744:        0.47293E+02

===============================================================


 INSTANT    0.745000000E+02   TIME STEP NUMBER             745
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.545481443E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30841E+02 0.13810E+02
   Friction velocity        uet   :  0.64312E-03 0.29422E+01
   Friction velocity        uk    :  0.15819E-01 0.28300E+01
   Dimensionless distance   yplus :  0.11889E+00 0.28480E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        524
   Nb of faces within the viscous sub-layer     :       1113
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2100   0.45430E-02   0.32361E+00 
c  VelocityY    0.29410E+04    2100   0.45430E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2100   0.45430E-02   0.00000E+00 
c  Pressure     0.44095E+00    7113   0.35913E-01   0.20962E+00 
c  k            0.21605E+04    1337   0.59575E-04   0.49337E+00 
c  omega        0.19812E+08     182   0.40683E-04   0.84040E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.6482e+05                             3
a  Local Time Step      1.1312e-05                         44256


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.73115          0.6925       0.0075296       4.425e-06
v  Velocity[Y]                 -16.903          33.323          6.7098          20.056
v  Velocity[Z]                 -28.763          28.638        0.091308      0.00022414
v  ǁVelocityǁ                0.0052627          33.817          10.504          20.215
v  Pressure                    -405.17          347.88         -53.663          32.195
v  k                        1.0274e-07          50.477          4.1448          1.6766
v  omega                         1e-24      2.6327e+07          8555.7          11.967
v  turbulent_viscosity      1.5434e-14          1.2697        0.015827         0.11171
v  CourantNb                  0.027205            2022          44.567          1.3763
v  FourierNb                  0.010868           15188           92.94         0.70217
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010823        0.045773


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94365           15244          137.51          2.0785


 TIME FOR THE TIME STEP              745:        0.47239E+02

===============================================================


 INSTANT    0.746000000E+02   TIME STEP NUMBER             746
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.328744670E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30504E+02 0.14317E+02
   Friction velocity        uet   :  0.13705E-02 0.29181E+01
   Friction velocity        uk    :  0.18678E-01 0.29724E+01
   Dimensionless distance   yplus :  0.14424E+00 0.31148E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :       1083
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2080   0.44954E-02   0.35366E+00 
c  VelocityY    0.29410E+04    2080   0.44954E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2080   0.44954E-02   0.00000E+00 
c  Pressure     0.46540E+00    6989   0.33743E-01   0.22101E+00 
c  k            0.21563E+04    1427   0.62911E-04   0.58323E+00 
c  omega        0.13589E+08     346   0.38071E-04   0.34226E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -68539                             1
a  Local Time Step      1.0918e-05                         44294


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80422         0.69271       0.0066323       5.604e-06
v  Velocity[Y]                 -15.322          32.844          6.7331          20.056
v  Velocity[Z]                 -28.492          28.627        0.028845     -0.00051263
v  ǁVelocityǁ                 0.011315          33.881          10.498          20.214
v  Pressure                    -395.18          346.62         -54.216          31.765
v  k                        1.1834e-08          47.315          4.1482          1.6761
v  omega                         1e-24      1.3499e+07          8469.9          11.923
v  turbulent_viscosity      4.1804e-14          1.2733        0.015879         0.11172
v  CourantNb                  0.026501          2037.4          44.062          1.3762
v  FourierNb                  0.010868           15262          94.869         0.70323
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14799        0.010825        0.045785


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15327          138.93          2.0794


 TIME FOR THE TIME STEP              746:        0.47110E+02

===============================================================


 INSTANT    0.747000000E+02   TIME STEP NUMBER             747
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.834063086E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31532E+02 0.16687E+02
   Friction velocity        uet   :  0.59889E-03 0.28150E+01
   Friction velocity        uk    :  0.19034E-01 0.32058E+01
   Dimensionless distance   yplus :  0.10330E+00 0.36958E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        432
   Nb of faces within the viscous sub-layer     :       1093
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2058   0.46195E-02   0.38937E+00 
c  VelocityY    0.29411E+04    2058   0.46195E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2058   0.46195E-02   0.00000E+00 
c  Pressure     0.46522E+00    6982   0.32081E-01   0.21825E+00 
c  k            0.21518E+04    1446   0.60169E-04   0.54332E+00 
c  omega        0.10471E+08     388   0.34449E-04   0.19816E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3006e+05                             2
a  Local Time Step      1.1747e-05                         44278


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93265         0.68347       0.0052942      5.5757e-06
v  Velocity[Y]                 -15.175          33.031          6.7188          20.056
v  Velocity[Z]                  -29.28           28.77       -0.029935      -0.0012396
v  ǁVelocityǁ                 0.018069          33.492          10.501          20.215
v  Pressure                    -379.01          345.25         -54.432          31.214
v  k                        1.5572e-10          40.687          4.1339          1.6755
v  omega                         1e-24       1.171e+07          8474.8          11.917
v  turbulent_viscosity      8.8493e-15          1.2787        0.015919         0.11172
v  CourantNb                  0.014053          2036.9          43.858          1.3763
v  FourierNb                  0.010868           15307          96.375           0.704
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14841        0.010825        0.045765


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15380          140.23          2.0803


 TIME FOR THE TIME STEP              747:        0.47078E+02

===============================================================


 INSTANT    0.748000000E+02   TIME STEP NUMBER             748
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.505771512E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31685E+02 0.19720E+02
   Friction velocity        uet   :  0.41422E-03 0.26605E+01
   Friction velocity        uk    :  0.19444E-01 0.32742E+01
   Dimensionless distance   yplus :  0.14181E+00 0.30753E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        507
   Nb of faces within the viscous sub-layer     :       1097
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2037   0.44349E-02   0.41955E+00 
c  VelocityY    0.29412E+04    2037   0.44349E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2037   0.44349E-02   0.00000E+00 
c  Pressure     0.45964E+00    7004   0.30935E-01   0.21645E+00 
c  k            0.21477E+04    1443   0.55634E-04   0.58057E+00 
c  omega        0.27086E+20       2   0.48056E-15   0.24878E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3744e+05                             2
a  Local Time Step      1.1785e-05                         44328


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94782         0.88972       0.0032567      5.0853e-06
v  Velocity[Y]                 -15.115          30.752          6.7062          20.056
v  Velocity[Z]                 -29.636          28.636       -0.063073      -0.0016701
v  ǁVelocityǁ                 0.012039          34.275          10.501          20.215
v  Pressure                    -365.45          344.04         -54.281          30.913
v  k                        1.0705e-10           40.58          4.1153           1.675
v  omega                         1e-24       1.508e+07          8388.2          11.891
v  turbulent_viscosity      4.4856e-17          1.2836        0.015941         0.11172
v  CourantNb                  0.017386          2029.4          43.775          1.3765
v  FourierNb                  0.010868           15328           96.11          0.7038
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14806        0.010824        0.045753


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87453           15406          139.88          2.0803


 TIME FOR THE TIME STEP              748:        0.46864E+02

===============================================================


 INSTANT    0.749000000E+02   TIME STEP NUMBER             749
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.154426944E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30394E+02 0.19789E+02
   Friction velocity        uet   :  0.64421E-03 0.28003E+01
   Friction velocity        uk    :  0.20343E-01 0.34287E+01
   Dimensionless distance   yplus :  0.13469E+00 0.28086E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        520
   Nb of faces within the viscous sub-layer     :       1114
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2050   0.45589E-02   0.45806E+00 
c  VelocityY    0.29412E+04    2050   0.45589E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2050   0.45589E-02   0.00000E+00 
c  Pressure     0.43457E+00    7002   0.29730E-01   0.20433E+00 
c  k            0.21456E+04    1456   0.61187E-04   0.73484E+00 
c  omega        0.10274E+08     283   0.48225E-04   0.11051E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5417e+05                             1
a  Local Time Step       1.193e-05                         44406


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0078          1.0601       0.0012708      3.6819e-06
v  Velocity[Y]                 -15.155            30.4          6.7121          20.056
v  Velocity[Z]                 -31.811          28.621       -0.089768      -0.0023525
v  ǁVelocityǁ                  0.01655          37.173           10.51          20.215
v  Pressure                    -348.77          346.37          -52.94          30.923
v  k                        6.1391e-11           51.07          4.1229          1.6747
v  omega                         1e-24       1.179e+07            8228          11.886
v  turbulent_viscosity      8.7522e-17          1.2868        0.015957          0.1117
v  CourantNb                  0.043135          2015.7          43.797          1.3765
v  FourierNb                  0.010868           15548          95.796         0.70344
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010822        0.045749


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.97635           15591          139.59          2.0799


 TIME FOR THE TIME STEP              749:        0.48020E+02

===============================================================


 INSTANT    0.750000000E+02   TIME STEP NUMBER             750
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.153797757E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30333E+02 0.19552E+02
   Friction velocity        uet   :  0.10646E-02 0.30828E+01
   Friction velocity        uk    :  0.18018E-01 0.30518E+01
   Dimensionless distance   yplus :  0.13749E+00 0.28450E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :       1085
   Total number of wall faces                   :       7680
------------------------------------------------------------




 Write intermediate restart files
   checkpoint at iteration        750, Physical time    0.75000E+02


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 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                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
   End writing the wall distance                        
 End writing


 Time for restart files:    0.18047E+01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2089   0.45672E-02   0.47949E+00 
c  VelocityY    0.29413E+04    2089   0.45672E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2089   0.45672E-02   0.00000E+00 
c  Pressure     0.42367E+00    7041   0.33824E-01   0.19966E+00 
c  k            0.21475E+04    1297   0.68351E-04   0.83391E+00 
c  omega        0.99582E+07     243   0.34934E-04   0.10478E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -14567                             1
a  Local Time Step      1.1299e-05                         44454


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1293          1.1469     -0.00042593      1.6224e-06
v  Velocity[Y]                 -15.306          32.497          6.7394          20.056
v  Velocity[Z]                 -33.434          28.616        -0.10947      -0.0028783
v  ǁVelocityǁ                0.0046354          36.807          10.542          20.215
v  Pressure                    -408.79          349.12         -51.477          31.326
v  k                        2.0402e-09          62.373          4.1035          1.6744
v  omega                         1e-24      1.1752e+07          7926.4          11.857
v  turbulent_viscosity      6.9464e-17          1.2913         0.01598         0.11168
v  CourantNb                  0.061318          1999.9          43.756          1.3764
v  FourierNb                  0.010867           15735          95.089         0.70305
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14819        0.010822        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15786          138.84          2.0795


 TIME FOR THE TIME STEP              750:        0.48933E+02

===============================================================


 INSTANT    0.751000000E+02   TIME STEP NUMBER             751
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.536503224E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31324E+02 0.16853E+02
   Friction velocity        uet   :  0.13910E-02 0.31752E+01
   Friction velocity        uk    :  0.16867E-01 0.32060E+01
   Dimensionless distance   yplus :  0.17118E+00 0.28762E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        431
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2148   0.46747E-02   0.49965E+00 
c  VelocityY    0.29413E+04    2148   0.46747E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2148   0.46747E-02   0.00000E+00 
c  Pressure     0.42669E+00    7122   0.38340E-01   0.19993E+00 
c  k            0.21547E+04    1347   0.74140E-04   0.92862E+00 
c  omega        0.81437E+20       2   0.43206E-16   0.80694E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1747e-05                         44451


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3155          1.1615       -0.001355      3.8442e-07
v  Velocity[Y]                 -17.292          31.913          6.7798          20.057
v  Velocity[Z]                 -33.115          28.662       -0.085733      -0.0033005
v  ǁVelocityǁ                 0.004407          35.303          10.582          20.216
v  Pressure                    -442.96          350.35         -50.705          31.546
v  k                        1.0412e-07          66.801          4.0751           1.674
v  omega                         1e-24      1.1736e+07          7766.2          11.838
v  turbulent_viscosity      4.3872e-15          1.2967        0.015989         0.11166
v  CourantNb                  0.035344          2504.2          43.751          1.3763
v  FourierNb                  0.010866           15844          95.455         0.70272
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14775        0.010822        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15905          139.21           2.079


 TIME FOR THE TIME STEP              751:        0.48302E+02

===============================================================


 INSTANT    0.752000000E+02   TIME STEP NUMBER             752
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.484209197E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31294E+02 0.14419E+02
   Friction velocity        uet   :  0.33276E-03 0.31214E+01
   Friction velocity        uk    :  0.15366E-01 0.29387E+01
   Dimensionless distance   yplus :  0.14998E+00 0.28172E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :       1049
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2154   0.45098E-02   0.50573E+00 
c  VelocityY    0.29413E+04    2154   0.45098E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2154   0.45098E-02   0.00000E+00 
c  Pressure     0.44515E+00    7124   0.39074E-01   0.20946E+00 
c  k            0.21646E+04    1553   0.74914E-04   0.10417E+01 
c  omega        0.99038E+07     310   0.19957E-03   0.11298E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1357e-05                         44439


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3927          1.0864      -0.0014672      1.5594e-07
v  Velocity[Y]                 -22.442          30.144          6.8003          20.057
v  Velocity[Z]                 -33.143          28.806       -0.035736      -0.0037469
v  ǁVelocityǁ                0.0038422          34.452          10.584          20.216
v  Pressure                    -451.29          350.29         -50.227          31.591
v  k                        3.3511e-09          60.409          4.0273          1.6737
v  omega                         1e-24      6.7476e+07          8072.5          11.888
v  turbulent_viscosity      3.8466e-14          1.2986        0.015964         0.11162
v  CourantNb                  0.023027          2697.6          43.944          1.3762
v  FourierNb                  0.010866           15741           94.31         0.70182
v  total_pressure           1.0087e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14846        0.010822        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15810          138.25           2.078


 TIME FOR THE TIME STEP              752:        0.48118E+02

===============================================================


 INSTANT    0.753000000E+02   TIME STEP NUMBER             753
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.327372291E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30323E+02 0.14078E+02
   Friction velocity        uet   :  0.33482E-02 0.29138E+01
   Friction velocity        uk    :  0.13525E-01 0.29741E+01
   Dimensionless distance   yplus :  0.12537E+00 0.27501E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        354
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2186   0.45933E-02   0.48549E+00 
c  VelocityY    0.29414E+04    2186   0.45933E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2186   0.45933E-02   0.00000E+00 
c  Pressure     0.44111E+00    7108   0.36051E-01   0.20634E+00 
c  k            0.21759E+04    1508   0.72943E-04   0.99592E+00 
c  omega        0.24665E+08     167   0.40785E-04   0.47923E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3159e+05                             1
a  Local Time Step      1.1246e-05                         44426


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3505         0.92305     -0.00030424      4.9908e-08
v  Velocity[Y]                  -27.22          30.017           6.768          20.057
v  Velocity[Z]                 -32.229          28.721       0.0010923      -0.0039859
v  ǁVelocityǁ                0.0063919          32.755          10.564          20.216
v  Pressure                    -440.23          349.83         -49.762          31.616
v  k                        2.5703e-07           47.62          3.9719          1.6732
v  omega                         1e-24      3.4542e+07          8029.3          11.879
v  turbulent_viscosity      4.7578e-16          1.3011         0.01589         0.11159
v  CourantNb                  0.014675            2332           44.15          1.3762
v  FourierNb                  0.010866           15717          93.182         0.70067
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14724        0.010823        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15764          137.33          2.0769


 TIME FOR THE TIME STEP              753:        0.48919E+02

===============================================================


 INSTANT    0.754000000E+02   TIME STEP NUMBER             754
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.128263288E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31807E+02 0.17235E+02
   Friction velocity        uet   :  0.21040E-02 0.27682E+01
   Friction velocity        uk    :  0.19764E-01 0.31079E+01
   Dimensionless distance   yplus :  0.13969E+00 0.27640E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        355
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2195   0.44254E-02   0.46254E+00 
c  VelocityY    0.29414E+04    2195   0.44254E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2195   0.44254E-02   0.00000E+00 
c  Pressure     0.44648E+00    7086   0.33293E-01   0.20928E+00 
c  k            0.21810E+04    1453   0.75309E-04   0.96040E+00 
c  omega        0.11751E+08     261   0.50467E-04   0.26895E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3836e+05                             1
a  Local Time Step      1.1427e-05                         44413


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1658         0.78802       0.0013851     -3.6584e-07
v  Velocity[Y]                 -36.323          29.919          6.6829          20.057
v  Velocity[Z]                 -30.915          28.564        0.010186      -0.0042155
v  ǁVelocityǁ                 0.012438          36.574          10.563          20.216
v  Pressure                    -414.81          348.62         -50.015          31.536
v  k                        5.7937e-08          74.974           3.993          1.6728
v  omega                         1e-24      1.8793e+07          7841.6          11.859
v  turbulent_viscosity      2.3752e-13          1.3032         0.01583         0.11156
v  CourantNb                  0.050176          2003.4          44.293          1.3761
v  FourierNb                  0.010866           15714          92.967         0.69992
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14801        0.010824        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15758          137.26           2.076


 TIME FOR THE TIME STEP              754:        0.49741E+02

===============================================================


 INSTANT    0.755000000E+02   TIME STEP NUMBER             755
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.147053324E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31033E+02 0.24633E+02
   Friction velocity        uet   :  0.20933E-02 0.30703E+01
   Friction velocity        uk    :  0.25915E-01 0.28683E+01
   Dimensionless distance   yplus :  0.11652E+00 0.31057E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        374
   Nb of faces within the viscous sub-layer     :       1066
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2252   0.45009E-02   0.45912E+00 
c  VelocityY    0.29414E+04    2252   0.45009E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2252   0.45009E-02   0.00000E+00 
c  Pressure     0.46310E+00    7062   0.35107E-01   0.21846E+00 
c  k            0.21796E+04    1321   0.10788E-03   0.85233E+00 
c  omega        0.10130E+08     437   0.13659E-03   0.88615E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.601e+05                             2
a  Local Time Step      1.1165e-05                         44430


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.96344         0.72076        0.002673     -2.0133e-06
v  Velocity[Y]                 -39.939           30.23           6.628          20.056
v  Velocity[Z]                 -29.089          28.536         0.01563       -0.004566
v  ǁVelocityǁ                0.0080241          41.458          10.576          20.216
v  Pressure                     -418.3          349.13         -51.341          31.533
v  k                        5.3405e-08           107.9           4.079          1.6725
v  omega                         1e-24      4.9754e+07          8311.8          11.905
v  turbulent_viscosity      5.3204e-14          1.3045        0.015813         0.11153
v  CourantNb                  0.015404          2027.8          44.369           1.376
v  FourierNb                  0.010866           15654          93.495         0.70001
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14883        0.010823        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15700          137.86           2.076


 TIME FOR THE TIME STEP              755:        0.50030E+02

===============================================================


 INSTANT    0.756000000E+02   TIME STEP NUMBER             756
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.309921679E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57827E+02 0.13695E+02
   Friction velocity        uet   :  0.16400E-02 0.36457E+01
   Friction velocity        uk    :  0.27077E-01 0.48579E+01
   Dimensionless distance   yplus :  0.12226E+00 0.41296E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :       1055
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2313   0.45820E-02   0.46476E+00 
c  VelocityY    0.29414E+04    2313   0.45820E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2313   0.45820E-02   0.00000E+00 
c  Pressure     0.44494E+00    6945   0.38308E-01   0.21007E+00 
c  k            0.21749E+04    1251   0.13059E-03   0.71636E+00 
c  omega        0.15206E+08     455   0.20176E-03   0.29601E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4585e+05                             3
a  Local Time Step      1.1136e-05                         44421


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93578         0.57379       0.0027424     -7.7492e-07
v  Velocity[Y]                  -29.36          30.704          6.6365          20.057
v  Velocity[Z]                 -29.377          28.409        0.011825      -0.0045734
v  ǁVelocityǁ                0.0053745          33.725          10.579          20.216
v  Pressure                    -418.98          349.06         -53.354           31.74
v  k                        2.3605e-08          60.719          4.1169          1.6723
v  omega                         1e-24      6.1852e+07          9410.6          11.984
v  turbulent_viscosity      7.4148e-14          1.3043        0.015831         0.11149
v  CourantNb                   0.02326          2149.1           44.49          1.3761
v  FourierNb                  0.010866           15611           93.79         0.70044
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14935        0.010822        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15663          138.28          2.0765


 TIME FOR THE TIME STEP              756:        0.50070E+02

===============================================================


 INSTANT    0.757000000E+02   TIME STEP NUMBER             757
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.299236954E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30355E+02 0.13881E+02
   Friction velocity        uet   :  0.11869E-03 0.28976E+01
   Friction velocity        uk    :  0.11559E-01 0.32157E+01
   Dimensionless distance   yplus :  0.80872E-01 0.28412E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2237   0.45105E-02   0.47397E+00 
c  VelocityY    0.29414E+04    2237   0.45105E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2237   0.45105E-02   0.00000E+00 
c  Pressure     0.43146E+00    7128   0.37661E-01   0.20224E+00 
c  k            0.21702E+04    1340   0.72677E-04   0.60057E+00 
c  omega        0.29701E+08     216   0.61402E-04   0.18098E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3859e+05                             3
a  Local Time Step      1.1195e-05                         44457


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.9114          0.6191       0.0024755     -1.3348e-06
v  Velocity[Y]                 -17.887          30.956          6.6674          20.057
v  Velocity[Z]                 -28.794          28.515      -0.0056257      -0.0048194
v  ǁVelocityǁ                0.0049175          33.657          10.567          20.217
v  Pressure                     -419.6          348.68         -55.127          31.766
v  k                        2.9983e-09          53.014          4.1625          1.6723
v  omega                         1e-24       4.041e+07          8980.6          11.946
v  turbulent_viscosity      1.2197e-14          1.3038        0.015867         0.11146
v  CourantNb                  0.014937          2925.4           44.64          1.3761
v  FourierNb                  0.010867           15636          94.291         0.70103
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14872        0.010821        0.045747


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0043           15694          138.93          2.0771


 TIME FOR THE TIME STEP              757:        0.48770E+02

===============================================================


 INSTANT    0.758000000E+02   TIME STEP NUMBER             758
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.480975086E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30634E+02 0.13984E+02
   Friction velocity        uet   :  0.69179E-03 0.27940E+01
   Friction velocity        uk    :  0.17606E-01 0.28181E+01
   Dimensionless distance   yplus :  0.89185E-01 0.28046E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2240   0.46099E-02   0.48325E+00 
c  VelocityY    0.29414E+04    2240   0.46099E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2240   0.46099E-02   0.00000E+00 
c  Pressure     0.44782E+00    7103   0.33417E-01   0.21233E+00 
c  k            0.21660E+04    1460   0.75276E-04   0.56988E+00 
c  omega        0.26687E+08     349   0.60390E-04   0.12145E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -65666                             1
a  Local Time Step      1.1411e-05                         44484


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.84838         0.64541       0.0024397      1.1282e-06
v  Velocity[Y]                 -17.236          32.545          6.7082          20.056
v  Velocity[Z]                 -28.683           31.53       -0.036542      -0.0047765
v  ǁVelocityǁ                0.0087168          33.985          10.537          20.216
v  Pressure                    -418.78          348.21         -55.759          31.818
v  k                        2.1091e-09          48.035          4.2155          1.6723
v  omega                         1e-24       5.566e+07          8688.8           11.91
v  turbulent_viscosity      7.7035e-15          1.3034        0.015902         0.11144
v  CourantNb                  0.027095          2059.7          44.437          1.3761
v  FourierNb                  0.010867           15578          96.109         0.70178
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494         0.01082        0.045763


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15643          140.55          2.0779


 TIME FOR THE TIME STEP              758:        0.49277E+02

===============================================================


 INSTANT    0.759000000E+02   TIME STEP NUMBER             759
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.128003321E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31309E+02 0.15031E+02
   Friction velocity        uet   :  0.74271E-03 0.29200E+01
   Friction velocity        uk    :  0.21209E-01 0.30389E+01
   Dimensionless distance   yplus :  0.13562E+00 0.30976E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        476
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    2208   0.44685E-02   0.49378E+00 
c  VelocityY    0.29415E+04    2208   0.44685E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    2208   0.44685E-02   0.00000E+00 
c  Pressure     0.45521E+00    6982   0.30548E-01   0.21623E+00 
c  k            0.21606E+04    1474   0.66219E-04   0.63560E+00 
c  omega        0.19166E+08     418   0.53464E-04   0.52408E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.2088e+05                             2
a  Local Time Step      1.0914e-05                         44506


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85301         0.60843       0.0026282      2.4591e-06
v  Velocity[Y]                 -15.195          33.255          6.7328          20.057
v  Velocity[Z]                 -28.619          28.624       -0.064186      -0.0045301
v  ǁVelocityǁ                 0.011411          33.963          10.507          20.216
v  Pressure                    -411.93          346.88         -56.082          31.582
v  k                        2.3083e-07          55.041          4.2137          1.6724
v  omega                         1e-24      3.4256e+07          8425.1          11.875
v  turbulent_viscosity      5.0515e-16          1.3007        0.015934         0.11142
v  CourantNb                  0.019973          2043.3          44.191          1.3762
v  FourierNb                  0.010868           15517          98.746         0.70273
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14878         0.01082        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15589          142.94          2.0789


 TIME FOR THE TIME STEP              759:        0.48703E+02

===============================================================


 INSTANT    0.760000000E+02   TIME STEP NUMBER             760
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.231261187E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31698E+02 0.15736E+02
   Friction velocity        uet   :  0.22689E-02 0.28531E+01
   Friction velocity        uk    :  0.63982E-02 0.32112E+01
   Dimensionless distance   yplus :  0.53490E-01 0.37119E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        430
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2182   0.45180E-02   0.50074E+00 
c  VelocityY    0.29414E+04    2182   0.45180E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2182   0.45180E-02   0.00000E+00 
c  Pressure     0.43162E+00    6990   0.31475E-01   0.20434E+00 
c  k            0.21538E+04    1415   0.59609E-04   0.56509E+00 
c  omega        0.12561E+08     290   0.49683E-04   0.26811E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -41416                             1
a  Local Time Step      1.1474e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.82655         0.71185       0.0034223      6.5664e-06
v  Velocity[Y]                 -15.227          34.021          6.7165          20.057
v  Velocity[Z]                 -28.404          28.906       -0.093926      -0.0045959
v  ǁVelocityǁ                 0.016112          34.331          10.506          20.216
v  Pressure                    -394.03          344.36         -56.894          30.856
v  k                        8.7649e-08          40.986          4.1912          1.6725
v  omega                         1e-24      1.8609e+07          8345.3          11.864
v  turbulent_viscosity      4.7365e-14          1.2998         0.01594          0.1114
v  CourantNb                   0.02454          2024.4          43.914          1.3763
v  FourierNb                   0.01087           15397          98.447         0.70284
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14899         0.01082        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15474          142.36          2.0791


 TIME FOR THE TIME STEP              760:        0.48662E+02

===============================================================


 INSTANT    0.761000000E+02   TIME STEP NUMBER             761
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.149608782E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30486E+02 0.23223E+02
   Friction velocity        uet   :  0.49905E-03 0.27839E+01
   Friction velocity        uk    :  0.12301E-01 0.31382E+01
   Dimensionless distance   yplus :  0.92387E-01 0.38054E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2176   0.45374E-02   0.50371E+00 
c  VelocityY    0.29414E+04    2176   0.45374E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2176   0.45374E-02   0.00000E+00 
c  Pressure     0.42151E+00    6890   0.31614E-01   0.20115E+00 
c  k            0.21485E+04    1228   0.56132E-04   0.55993E+00 
c  omega        0.10827E+08     265   0.30635E-04   0.15822E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5369e+05                             1
a  Local Time Step      1.1807e-05                         44528


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.71695         0.83392       0.0038357      8.8842e-06
v  Velocity[Y]                 -15.114          31.352          6.7071          20.057
v  Velocity[Z]                 -28.996          28.652        -0.10111      -0.0043537
v  ǁVelocityǁ                 0.011268          34.067           10.51          20.216
v  Pressure                    -381.21           345.7         -56.818           30.61
v  k                        4.4775e-08          37.411          4.1497          1.6728
v  omega                         1e-24      1.2223e+07            8193          11.849
v  turbulent_viscosity      3.6591e-14          1.2988        0.015932         0.11139
v  CourantNb                  0.025923          1997.3           43.75          1.3766
v  FourierNb                  0.010872           15288          98.205         0.70261
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010819        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15332          141.95          2.0792


 TIME FOR THE TIME STEP              761:        0.49026E+02

===============================================================


 INSTANT    0.762000000E+02   TIME STEP NUMBER             762
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.457047447E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30090E+02 0.21163E+02
   Friction velocity        uet   :  0.18501E-02 0.25756E+01
   Friction velocity        uk    :  0.95571E-02 0.30146E+01
   Dimensionless distance   yplus :  0.84153E-01 0.31233E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        471
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2194   0.44035E-02   0.49194E+00 
c  VelocityY    0.29411E+04    2194   0.44035E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2194   0.44035E-02   0.00000E+00 
c  Pressure     0.44374E+00    6966   0.29829E-01   0.21155E+00 
c  k            0.21447E+04    1127   0.57654E-04   0.67139E+00 
c  omega        0.10312E+08     263   0.26620E-04   0.90484E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -72127                             2
a  Local Time Step      1.1725e-05                         44520


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.5475          1.0068       0.0040514      7.3784e-06
v  Velocity[Y]                 -15.261           30.59          6.7248          20.057
v  Velocity[Z]                 -31.481          28.866        -0.10283      -0.0039659
v  ǁVelocityǁ                 0.004767          36.681          10.531          20.216
v  Pressure                    -354.01          348.14         -55.579          30.893
v  k                        2.9116e-09          46.974          4.1046          1.6732
v  omega                         1e-24      1.1824e+07          8077.6          11.839
v  turbulent_viscosity      3.7011e-14          1.2972        0.015921         0.11139
v  CourantNb                  0.028284          2005.5          43.942          1.3769
v  FourierNb                  0.010876           15373          97.465         0.70217
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010818        0.045735


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15425          141.41           2.079


 TIME FOR THE TIME STEP              762:        0.49223E+02

===============================================================


 INSTANT    0.763000000E+02   TIME STEP NUMBER             763
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.134171342E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31104E+02 0.18550E+02
   Friction velocity        uet   :  0.69384E-03 0.30173E+01
   Friction velocity        uk    :  0.22201E-01 0.30358E+01
   Dimensionless distance   yplus :  0.13191E+00 0.28392E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        410
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2226   0.44028E-02   0.46634E+00 
c  VelocityY    0.29411E+04    2226   0.44028E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2226   0.44028E-02   0.00000E+00 
c  Pressure     0.42678E+00    7112   0.31701E-01   0.20321E+00 
c  k            0.21446E+04    1429   0.64376E-04   0.82291E+00 
c  omega        0.10136E+08     255   0.28598E-04   0.82126E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0069e+05                             2
a  Local Time Step      1.1483e-05                         44508


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.60474          1.2267       0.0041781      7.6743e-06
v  Velocity[Y]                  -15.06           30.53          6.7747          20.057
v  Velocity[Z]                 -31.992          28.835       -0.087967      -0.0035035
v  ǁVelocityǁ                 0.012251          36.651          10.585          20.216
v  Pressure                    -403.81          350.21         -53.933          31.141
v  k                        1.0915e-08          60.204          4.0711          1.6737
v  omega                         1e-24      1.1775e+07          8005.2          11.821
v  turbulent_viscosity      5.2466e-16          1.2949        0.015901         0.11139
v  CourantNb                   0.01208          2031.2          44.014          1.3768
v  FourierNb                  0.010879           15477          96.213         0.70147
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010818        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15538          140.23          2.0783


 TIME FOR THE TIME STEP              763:        0.49107E+02

===============================================================


 INSTANT    0.764000000E+02   TIME STEP NUMBER             764
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.108922779E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31541E+02 0.14344E+02
   Friction velocity        uet   :  0.31099E-02 0.30995E+01
   Friction velocity        uk    :  0.19294E-01 0.30821E+01
   Dimensionless distance   yplus :  0.83298E-01 0.27645E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2175   0.44232E-02   0.45130E+00 
c  VelocityY    0.29410E+04    2175   0.44232E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2175   0.44232E-02   0.00000E+00 
c  Pressure     0.44639E+00    7143   0.36095E-01   0.21217E+00 
c  k            0.21510E+04    1561   0.67408E-04   0.93423E+00 
c  omega        0.10189E+08     289   0.32157E-04   0.12264E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1655e+05                             3
a  Local Time Step      1.1848e-05                         44483


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.64753          1.4585       0.0042108      7.0837e-06
v  Velocity[Y]                  -15.25          32.117          6.8455          20.056
v  Velocity[Z]                 -32.947          29.096       -0.045186        -0.00273
v  ǁVelocityǁ                 0.012511          35.291           10.65          20.215
v  Pressure                    -436.83          350.93         -52.351          31.406
v  k                        2.6898e-07          68.478           4.038          1.6742
v  omega                         1e-24      1.5659e+07          7956.5          11.815
v  turbulent_viscosity      1.5685e-14          1.2922         0.01586         0.11139
v  CourantNb                 0.0025717          2463.3           44.23          1.3768
v  FourierNb                  0.010882           15447          95.392         0.70068
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010816        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15517          139.62          2.0775


 TIME FOR THE TIME STEP              764:        0.48526E+02

===============================================================


 INSTANT    0.765000000E+02   TIME STEP NUMBER             765
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.379366254E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31760E+02 0.14337E+02
   Friction velocity        uet   :  0.71798E-03 0.31518E+01
   Friction velocity        uk    :  0.18865E-01 0.29271E+01
   Dimensionless distance   yplus :  0.12800E+00 0.26842E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        362
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2096   0.44398E-02   0.43912E+00 
c  VelocityY    0.29410E+04    2096   0.44398E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2096   0.44398E-02   0.00000E+00 
c  Pressure     0.42806E+00    7124   0.38926E-01   0.20321E+00 
c  k            0.21630E+04    1564   0.67283E-04   0.97461E+00 
c  omega        0.10333E+08     345   0.25857E-03   0.25693E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.339e+05                             1
a  Local Time Step       1.163e-05                         44470


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.72873          1.5722       0.0043441      2.8907e-06
v  Velocity[Y]                 -20.714          30.165          6.9032          20.056
v  Velocity[Z]                 -32.612          28.913        0.018982      -0.0021365
v  ǁVelocityǁ                 0.018167           34.13          10.684          20.214
v  Pressure                    -444.57          350.34         -51.099          31.813
v  k                         1.439e-07          65.838          3.9871          1.6747
v  omega                         1e-24      8.4531e+07          8757.3          11.897
v  turbulent_viscosity      1.5365e-13          1.2891        0.015806          0.1114
v  CourantNb                  0.033738          2772.9          44.657          1.3769
v  FourierNb                  0.010885           15332          94.323         0.70002
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14868        0.010817        0.045721


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15380          138.98           2.077


 TIME FOR THE TIME STEP              765:        0.48088E+02

===============================================================


 INSTANT    0.766000000E+02   TIME STEP NUMBER             766
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.372058891E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30598E+02 0.14579E+02
   Friction velocity        uet   :  0.15605E-02 0.29173E+01
   Friction velocity        uk    :  0.32413E-01 0.32235E+01
   Dimensionless distance   yplus :  0.13686E+00 0.27274E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        357
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    2055   0.45177E-02   0.39296E+00 
c  VelocityY    0.29411E+04    2055   0.45177E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    2055   0.45177E-02   0.00000E+00 
c  Pressure     0.46194E+00    7086   0.37149E-01   0.21882E+00 
c  k            0.21758E+04    1472   0.67318E-04   0.10144E+01 
c  omega        0.41885E+08     136   0.35489E-04   0.12820E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3182e+05                             2
a  Local Time Step      1.1397e-05                         44441


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86404          1.6286       0.0049223     -7.1832e-07
v  Velocity[Y]                 -24.956          29.972          6.8878          20.056
v  Velocity[Z]                 -32.573          29.151        0.092873      -0.0017029
v  ǁVelocityǁ                 0.017347          33.308          10.641          20.214
v  Pressure                    -433.17          349.19         -50.219          31.984
v  k                        1.1912e-07          53.576          3.9324           1.675
v  omega                         1e-24      4.2906e+07          8745.9          11.919
v  turbulent_viscosity      1.6263e-13          1.2866        0.015741         0.11141
v  CourantNb                  0.036125          2430.6          45.025          1.3772
v  FourierNb                  0.010889           15266          93.302         0.69927
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14826        0.010818        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15310          138.33          2.0765


 TIME FOR THE TIME STEP              766:        0.46142E+02

===============================================================


 INSTANT    0.767000000E+02   TIME STEP NUMBER             767
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.449793255E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30620E+02 0.17625E+02
   Friction velocity        uet   :  0.59550E-03 0.28350E+01
   Friction velocity        uk    :  0.21108E-01 0.33242E+01
   Dimensionless distance   yplus :  0.12930E+00 0.27610E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        325
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2037   0.46204E-02   0.34499E+00 
c  VelocityY    0.29412E+04    2037   0.46204E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2037   0.46204E-02   0.00000E+00 
c  Pressure     0.42835E+00    7100   0.32374E-01   0.20258E+00 
c  k            0.21842E+04    1325   0.77338E-04   0.97625E+00 
c  omega        0.18127E+08     209   0.42209E-04   0.50273E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9184e+05                             1
a  Local Time Step      1.1579e-05                         44438


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.91931          1.5977       0.0060598     -2.2445e-06
v  Velocity[Y]                 -32.601          29.795          6.7998          20.056
v  Velocity[Z]                 -30.237          28.997         0.13207      -0.0012809
v  ǁVelocityǁ                 0.011272          33.213          10.607          20.214
v  Pressure                    -408.41          349.97         -49.709          32.026
v  k                        9.7551e-08          67.606          3.9323          1.6752
v  omega                         1e-24      2.2699e+07            8464          11.901
v  turbulent_viscosity      1.9025e-13          1.2834        0.015685         0.11143
v  CourantNb                  0.017276          2020.4          44.916          1.3773
v  FourierNb                  0.010893           15181          92.673         0.69884
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14803        0.010819        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15227          137.59          2.0761


 TIME FOR THE TIME STEP              767:        0.47411E+02

===============================================================


 INSTANT    0.768000000E+02   TIME STEP NUMBER             768
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.240951310E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31244E+02 0.22274E+02
   Friction velocity        uet   :  0.21664E-02 0.28633E+01
   Friction velocity        uk    :  0.14234E-01 0.27675E+01
   Dimensionless distance   yplus :  0.15528E+00 0.27793E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    2056   0.47413E-02   0.32030E+00 
c  VelocityY    0.29413E+04    2056   0.47413E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    2056   0.47413E-02   0.00000E+00 
c  Pressure     0.43174E+00    7084   0.31949E-01   0.20502E+00 
c  k            0.21838E+04    1255   0.90839E-04   0.84655E+00 
c  omega        0.11446E+08     345   0.50002E-04   0.31963E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -24581                             1
a  Local Time Step      1.1355e-05                         44412


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90796          1.5857       0.0069054     -3.2621e-06
v  Velocity[Y]                 -35.593          29.848          6.7193          20.057
v  Velocity[Z]                 -29.097          28.896         0.15629     -0.00091837
v  ǁVelocityǁ                  0.01248          41.415          10.595          20.215
v  Pressure                    -404.01          349.56         -50.209          32.057
v  k                        3.2916e-08          86.221          3.9849          1.6753
v  omega                         1e-24      1.3605e+07            8352          11.892
v  turbulent_viscosity      1.0842e-14            1.28        0.015641         0.11145
v  CourantNb                   0.01575          2014.1          44.929          1.3773
v  FourierNb                  0.010897           15051          91.974          0.6989
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14849        0.010819          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15104           136.9          2.0762


 TIME FOR THE TIME STEP              768:        0.47112E+02

===============================================================


 INSTANT    0.769000000E+02   TIME STEP NUMBER             769
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.338168574E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.63578E+02 0.14238E+02
   Friction velocity        uet   :  0.33428E-02 0.35299E+01
   Friction velocity        uk    :  0.22493E-01 0.44467E+01
   Dimensionless distance   yplus :  0.18988E+00 0.32553E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        402
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    2005   0.47367E-02   0.31278E+00 
c  VelocityY    0.29414E+04    2005   0.47367E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    2005   0.47367E-02   0.00000E+00 
c  Pressure     0.45684E+00    7181   0.35970E-01   0.21660E+00 
c  k            0.21783E+04    1364   0.92610E-04   0.66937E+00 
c  omega        0.10557E+08     397   0.35144E-04   0.43622E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.4142e+05                             1
a  Local Time Step      1.1307e-05                         44387


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.87574          1.5026        0.006723     -3.2512e-06
v  Velocity[Y]                 -33.538          30.093          6.6836          20.056
v  Velocity[Z]                 -28.586          28.851         0.16834      -0.0004744
v  ǁVelocityǁ                 0.017274          34.542          10.582          20.215
v  Pressure                    -405.45          348.52         -51.425          32.164
v  k                         3.277e-10          54.691          4.0091          1.6756
v  omega                         1e-24      1.1739e+07          8489.2          11.923
v  turbulent_viscosity      3.6636e-15          1.2765         0.01561         0.11147
v  CourantNb                  0.058763          1993.4          44.977          1.3774
v  FourierNb                  0.010899           14965          91.889         0.69919
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14762         0.01082        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15026          136.87          2.0766


 TIME FOR THE TIME STEP              769:        0.48410E+02

===============================================================


 INSTANT    0.770000000E+02   TIME STEP NUMBER             770
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.926049210E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31715E+02 0.14324E+02
   Friction velocity        uet   :  0.13363E-02 0.32108E+01
   Friction velocity        uk    :  0.27982E-01 0.30367E+01
   Dimensionless distance   yplus :  0.12210E+00 0.27552E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1846   0.46344E-02   0.30082E+00 
c  VelocityY    0.29415E+04    1846   0.46344E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1846   0.46344E-02   0.00000E+00 
c  Pressure     0.44483E+00    7164   0.38904E-01   0.21032E+00 
c  k            0.21728E+04    1423   0.62309E-04   0.55905E+00 
c  omega        0.10565E+08     353   0.14822E-03   0.17607E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -1789.3                             1
a  Local Time Step      1.0978e-05                         44372


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85627          1.5132       0.0055107     -4.8037e-06
v  Velocity[Y]                 -18.334          30.689          6.6711          20.056
v  Velocity[Z]                 -28.681          28.973         0.15635     -2.0258e-05
v  ǁVelocityǁ                0.0092418          33.425          10.556          20.215
v  Pressure                    -406.18          346.55         -52.704          32.266
v  k                        2.2543e-09          41.543          4.0418          1.6758
v  omega                         1e-24      6.6828e+07          8854.8          11.965
v  turbulent_viscosity      1.3614e-15          1.2732        0.015596         0.11149
v  CourantNb                  0.021183          3163.2           45.21          1.3774
v  FourierNb                  0.010901           14909          91.182         0.69935
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14778         0.01082        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98461           14977          136.39          2.0768


 TIME FOR THE TIME STEP              770:        0.46383E+02

===============================================================


 INSTANT    0.771000000E+02   TIME STEP NUMBER             771
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.142014007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30390E+02 0.14262E+02
   Friction velocity        uet   :  0.25659E-03 0.28386E+01
   Friction velocity        uk    :  0.16878E-01 0.32107E+01
   Dimensionless distance   yplus :  0.13638E+00 0.26906E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :        990
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1725   0.45109E-02   0.30741E+00 
c  VelocityY    0.29416E+04    1725   0.45109E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1725   0.45109E-02   0.00000E+00 
c  Pressure     0.43716E+00    7131   0.38245E-01   0.20738E+00 
c  k            0.21688E+04    1416   0.55797E-04   0.45736E+00 
c  omega        0.30826E+08     203   0.25657E-04   0.10723E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.4674e+05                             2
a  Local Time Step      1.0723e-05                         44334


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86055          1.5719       0.0040028     -5.8893e-06
v  Velocity[Y]                 -17.287          32.856          6.6783          20.056
v  Velocity[Z]                 -28.609          28.868         0.12261      0.00041869
v  ǁVelocityǁ                0.0098428            33.9          10.534          20.215
v  Pressure                    -405.06          343.88         -53.679          32.153
v  k                        4.3561e-08          44.547          4.1034           1.676
v  omega                         1e-24      3.3532e+07          8565.5          11.934
v  turbulent_viscosity      3.9946e-15          1.2717        0.015596         0.11152
v  CourantNb                  0.061069          2322.2          44.859          1.3772
v  FourierNb                  0.010902           14821          90.957         0.69948
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814         0.01082        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14895          135.82          2.0767


 TIME FOR THE TIME STEP              771:        0.43485E+02

===============================================================


 INSTANT    0.772000000E+02   TIME STEP NUMBER             772
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.469303237E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30360E+02 0.13988E+02
   Friction velocity        uet   :  0.85547E-03 0.29132E+01
   Friction velocity        uk    :  0.22507E-01 0.31505E+01
   Dimensionless distance   yplus :  0.14971E+00 0.29654E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1768   0.46500E-02   0.33069E+00 
c  VelocityY    0.29418E+04    1768   0.46500E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1768   0.46500E-02   0.00000E+00 
c  Pressure     0.45278E+00    7113   0.36540E-01   0.21410E+00 
c  k            0.21656E+04    1373   0.62183E-04   0.50358E+00 
c  omega        0.16955E+08     185   0.26201E-04   0.44112E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62723                             1
a  Local Time Step      1.1622e-05                         44331


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85674           1.458       0.0031236     -6.1326e-06
v  Velocity[Y]                 -16.503          33.553          6.6998          20.056
v  Velocity[Z]                 -28.595          28.865        0.073174      0.00070708
v  ǁVelocityǁ                0.0096187           33.63          10.523          20.215
v  Pressure                     -399.6          342.96          -54.27           31.85
v  k                        1.3463e-07          55.273          4.1421          1.6762
v  omega                         1e-24      1.7032e+07          8354.2          11.907
v  turbulent_viscosity      1.7182e-14          1.2707        0.015633         0.11154
v  CourantNb                  0.037107          2028.7          44.317           1.377
v  FourierNb                  0.010902           14675          92.125          0.7002
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1493         0.01082        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14754          136.44          2.0772


 TIME FOR THE TIME STEP              772:        0.43761E+02

===============================================================


 INSTANT    0.773000000E+02   TIME STEP NUMBER             773
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.300085964E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31841E+02 0.14216E+02
   Friction velocity        uet   :  0.95690E-03 0.28623E+01
   Friction velocity        uk    :  0.14579E-01 0.28206E+01
   Dimensionless distance   yplus :  0.11370E+00 0.33939E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        411
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29420E+04    1786   0.46587E-02   0.35932E+00 
c  VelocityY    0.29420E+04    1786   0.46587E-02   0.00000E+00 
c  VelocityZ    0.29420E+04    1786   0.46587E-02   0.00000E+00 
c  Pressure     0.44362E+00    7011   0.33746E-01   0.20857E+00 
c  k            0.21626E+04    1343   0.55728E-04   0.53261E+00 
c  omega        0.11110E+08     349   0.33209E-04   0.26648E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2705e+05                             3
a  Local Time Step      1.1763e-05                         44267


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8173          1.1039       0.0025398     -7.4084e-06
v  Velocity[Y]                 -16.779          33.055          6.7139          20.057
v  Velocity[Z]                 -28.873          28.764        0.023172      0.00097917
v  ǁVelocityǁ                 0.013806          33.444          10.526          20.215
v  Pressure                    -382.93          340.85         -55.305          31.377
v  k                        1.9773e-09          44.837          4.1302          1.6763
v  omega                         1e-24      1.1675e+07          8342.8          11.895
v  turbulent_viscosity      5.8601e-14          1.2703        0.015675         0.11155
v  CourantNb                   0.03244          2050.5          44.025          1.3771
v  FourierNb                  0.010901           14699          94.117         0.70119
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14844        0.010821         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14740          138.14          2.0783


 TIME FOR THE TIME STEP              773:        0.45409E+02

===============================================================


 INSTANT    0.774000000E+02   TIME STEP NUMBER             774
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.793906466E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31320E+02 0.21992E+02
   Friction velocity        uet   :  0.44906E-03 0.27188E+01
   Friction velocity        uk    :  0.24620E-01 0.30972E+01
   Dimensionless distance   yplus :  0.15139E+00 0.37360E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1791   0.45604E-02   0.38489E+00 
c  VelocityY    0.29421E+04    1791   0.45604E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1791   0.45604E-02   0.00000E+00 
c  Pressure     0.42957E+00    7024   0.31585E-01   0.20218E+00 
c  k            0.21591E+04    1349   0.54004E-04   0.54257E+00 
c  omega        0.10250E+08     351   0.43055E-04   0.15650E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8298e+05                             1
a  Local Time Step      1.1271e-05                         44242


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.75859          1.0343       0.0018825     -5.3084e-06
v  Velocity[Y]                 -15.568          31.313          6.6986          20.057
v  Velocity[Z]                 -28.688          29.028       -0.010904       0.0008698
v  ǁVelocityǁ                0.0041745          32.926          10.528          20.215
v  Pressure                    -367.19           341.3         -55.276          31.032
v  k                        3.8874e-09          36.766          4.1112          1.6764
v  omega                         1e-24      1.1792e+07          8262.7          11.876
v  turbulent_viscosity      4.3005e-16          1.2702        0.015712         0.11157
v  CourantNb                   0.03999          2066.7          43.974          1.3773
v  FourierNb                    0.0109           14768          95.347         0.70181
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14814         0.01082        0.045661


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14818          139.32          2.0791


 TIME FOR THE TIME STEP              774:        0.44620E+02

===============================================================


 INSTANT    0.775000000E+02   TIME STEP NUMBER             775
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.477169625E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31209E+02 0.20469E+02
   Friction velocity        uet   :  0.19488E-02 0.25019E+01
   Friction velocity        uk    :  0.14740E-01 0.31843E+01
   Dimensionless distance   yplus :  0.13113E+00 0.30246E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        463
   Nb of faces within the viscous sub-layer     :       1023
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1703   0.45062E-02   0.40717E+00 
c  VelocityY    0.29421E+04    1703   0.45062E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1703   0.45062E-02   0.00000E+00 
c  Pressure     0.43389E+00    6995   0.32015E-01   0.20578E+00 
c  k            0.21560E+04    1417   0.59747E-04   0.63544E+00 
c  omega        0.11906E+08     227   0.25790E-04   0.84965E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -94132                             2
a  Local Time Step      1.1303e-05                         44284


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98522           1.103       0.0018208     -3.3004e-06
v  Velocity[Y]                 -15.148          30.849          6.6928          20.057
v  Velocity[Z]                 -30.141            29.1       -0.022798      0.00091646
v  ǁVelocityǁ                 0.010765          35.648          10.536          20.214
v  Pressure                    -350.35          342.01          -54.46          30.903
v  k                        8.0668e-08          45.345          4.0922          1.6766
v  omega                         1e-24      1.1841e+07          8146.6          11.862
v  turbulent_viscosity      1.6871e-15          1.2704         0.01574         0.11158
v  CourantNb                  0.066693          2073.8          43.972          1.3773
v  FourierNb                  0.010899           14960          95.781         0.70195
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14863        0.010819        0.045664


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15021          139.75          2.0792


 TIME FOR THE TIME STEP              775:        0.43512E+02

===============================================================


 INSTANT    0.776000000E+02   TIME STEP NUMBER             776
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.108099867E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30669E+02 0.20089E+02
   Friction velocity        uet   :  0.15907E-02 0.29234E+01
   Friction velocity        uk    :  0.17974E-01 0.31754E+01
   Dimensionless distance   yplus :  0.42000E-01 0.27491E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1575   0.46094E-02   0.43464E+00 
c  VelocityY    0.29422E+04    1575   0.46094E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1575   0.46094E-02   0.00000E+00 
c  Pressure     0.45436E+00    6751   0.31231E-01   0.21522E+00 
c  k            0.21538E+04    1470   0.64630E-04   0.77529E+00 
c  omega        0.99960E+07     253   0.34652E-04   0.63331E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9864e+05                             2
a  Local Time Step      1.2068e-05                         44312


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1769          1.1493       0.0025427      7.2382e-07
v  Velocity[Y]                  -15.35            31.9          6.7017          20.056
v  Velocity[Z]                 -31.914          29.198       -0.034918      0.00090943
v  ǁVelocityǁ                 0.010162          37.024          10.548          20.214
v  Pressure                    -373.55          343.04         -52.412          31.055
v  k                        7.6894e-09          55.093           4.094          1.6769
v  omega                         1e-24      1.1788e+07          7916.5          11.836
v  turbulent_viscosity      2.0445e-13          1.2707        0.015755         0.11158
v  CourantNb                   0.06224          2069.6          44.014          1.3772
v  FourierNb                  0.010896           15125          95.071         0.70167
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14934        0.010819         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15197          139.09          2.0788


 TIME FOR THE TIME STEP              776:        0.41906E+02

===============================================================


 INSTANT    0.777000000E+02   TIME STEP NUMBER             777
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.241148287E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31720E+02 0.20744E+02
   Friction velocity        uet   :  0.14021E-02 0.31011E+01
   Friction velocity        uk    :  0.25854E-01 0.29610E+01
   Dimensionless distance   yplus :  0.19907E+00 0.26691E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1010
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1714   0.45605E-02   0.44212E+00 
c  VelocityY    0.29421E+04    1714   0.45605E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1714   0.45605E-02   0.00000E+00 
c  Pressure     0.41656E+00    7103   0.34928E-01   0.19586E+00 
c  k            0.21555E+04    1465   0.71524E-04   0.90772E+00 
c  omega        0.99364E+07     299   0.25967E-04   0.59818E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -88334                             1
a  Local Time Step      1.1977e-05                         44340


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1882          1.2601       0.0035474      7.9222e-07
v  Velocity[Y]                  -15.26          32.717          6.7312          20.057
v  Velocity[Z]                 -33.397          29.203       -0.032437      0.00092938
v  ǁVelocityǁ                 0.010342          35.785          10.588          20.214
v  Pressure                    -423.41          343.06         -50.676          31.337
v  k                        1.0045e-07          63.462          4.0841          1.6771
v  omega                         1e-24      1.1747e+07          7802.8          11.832
v  turbulent_viscosity      4.4811e-15          1.2714        0.015776         0.11159
v  CourantNb                  0.040284          2124.1          43.973           1.377
v  FourierNb                  0.010893           15226          94.371         0.70151
v  total_pressure            1.009e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14936         0.01082        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15307          138.34          2.0785


 TIME FOR THE TIME STEP              777:        0.43553E+02

===============================================================


 INSTANT    0.778000000E+02   TIME STEP NUMBER             778
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.379139036E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32188E+02 0.19342E+02
   Friction velocity        uet   :  0.12192E-02 0.30870E+01
   Friction velocity        uk    :  0.27456E-01 0.29023E+01
   Dimensionless distance   yplus :  0.18644E+00 0.27013E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        363
   Nb of faces within the viscous sub-layer     :        942
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1730   0.45004E-02   0.45379E+00 
c  VelocityY    0.29421E+04    1730   0.45004E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1730   0.45004E-02   0.00000E+00 
c  Pressure     0.42978E+00    7126   0.38618E-01   0.20290E+00 
c  k            0.21620E+04    1367   0.73157E-04   0.99365E+00 
c  omega        0.99113E+07     266   0.24462E-03   0.17426E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8723e+05                             2
a  Local Time Step      1.1782e-05                         44395


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2117          1.4301       0.0041871      1.3996e-06
v  Velocity[Y]                 -19.409          30.035          6.7653          20.056
v  Velocity[Z]                 -33.442          29.057       0.0083585       0.0010507
v  ǁVelocityǁ                 0.018716          35.359          10.619          20.214
v  Pressure                    -443.69          342.54         -49.613          31.473
v  k                        3.0014e-07          64.094          4.0485          1.6773
v  omega                         1e-24      6.6341e+07          8355.8          11.871
v  turbulent_viscosity      4.9524e-14          1.2727        0.015774         0.11159
v  CourantNb                  0.043582          2526.7          44.034          1.3767
v  FourierNb                  0.010889           15372          94.155         0.70116
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010819        0.045755


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15414          138.19          2.0779


 TIME FOR THE TIME STEP              778:        0.43758E+02

===============================================================


 INSTANT    0.779000000E+02   TIME STEP NUMBER             779
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.207085229E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31833E+02 0.17669E+02
   Friction velocity        uet   :  0.66095E-03 0.30389E+01
   Friction velocity        uk    :  0.17989E-01 0.29087E+01
   Dimensionless distance   yplus :  0.14410E+00 0.27728E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        367
   Nb of faces within the viscous sub-layer     :        943
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1799   0.45313E-02   0.44569E+00 
c  VelocityY    0.29422E+04    1799   0.45313E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1799   0.45313E-02   0.00000E+00 
c  Pressure     0.40631E+00    7125   0.38154E-01   0.19179E+00 
c  k            0.21701E+04    1096   0.74774E-04   0.10380E+01 
c  omega        0.28375E+08     143   0.38029E-04   0.50505E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -63414                             2
a  Local Time Step      1.1535e-05                         44423


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0577          1.5197       0.0039294        1.12e-06
v  Velocity[Y]                 -25.076          29.852          6.7694          20.056
v  Velocity[Z]                 -33.181          29.107        0.066766      0.00064276
v  ǁVelocityǁ                 0.012074           34.41          10.609          20.213
v  Pressure                    -441.39          344.47          -48.93          31.661
v  k                        3.1522e-07          54.889               4          1.6774
v  omega                         1e-24      3.3964e+07          8069.4          11.854
v  turbulent_viscosity       2.873e-13          1.2739        0.015747         0.11159
v  CourantNb                   0.03239          2518.5          44.239          1.3766
v  FourierNb                  0.010885           15457          92.824         0.70061
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14914        0.010819        0.045762


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15502          137.06          2.0772


 TIME FOR THE TIME STEP              779:        0.43465E+02

===============================================================


 INSTANT    0.780000000E+02   TIME STEP NUMBER             780
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.573085171E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30725E+02 0.13548E+02
   Friction velocity        uet   :  0.64278E-03 0.29142E+01
   Friction velocity        uk    :  0.16808E-01 0.31729E+01
   Dimensionless distance   yplus :  0.60714E-01 0.27954E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        333
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1812   0.46392E-02   0.41721E+00 
c  VelocityY    0.29424E+04    1812   0.46392E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1812   0.46392E-02   0.00000E+00 
c  Pressure     0.43325E+00    7033   0.35065E-01   0.20523E+00 
c  k            0.21763E+04     966   0.74014E-04   0.10713E+01 
c  omega        0.12256E+08     213   0.82645E-04   0.46614E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6014e+05                             4
a  Local Time Step      1.1851e-05                         44417


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93261          1.4096       0.0023285      3.0413e-06
v  Velocity[Y]                 -31.632            29.7          6.7113          20.056
v  Velocity[Z]                 -31.305          28.939         0.10416      0.00054754
v  ǁVelocityǁ                0.0075086          32.942          10.583          20.213
v  Pressure                    -422.61          345.79         -48.578          31.668
v  k                        3.5598e-08          61.354          3.9813          1.6774
v  omega                         1e-24      1.8541e+07          8243.4          11.892
v  turbulent_viscosity      5.0521e-14          1.2754          0.0157          0.1116
v  CourantNb                  0.015516          2050.2          44.366          1.3765
v  FourierNb                  0.010881           15498          92.346         0.69999
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14932         0.01082        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9148           15550          136.71          2.0765


 TIME FOR THE TIME STEP              780:        0.43906E+02

===============================================================


 INSTANT    0.781000000E+02   TIME STEP NUMBER             781
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.100385183E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29812E+02 0.21765E+02
   Friction velocity        uet   :  0.97462E-03 0.29307E+01
   Friction velocity        uk    :  0.21673E-01 0.27396E+01
   Dimensionless distance   yplus :  0.89578E-01 0.28055E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        382
   Nb of faces within the viscous sub-layer     :        994
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1742   0.45431E-02   0.39922E+00 
c  VelocityY    0.29426E+04    1742   0.45431E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1742   0.45431E-02   0.00000E+00 
c  Pressure     0.43167E+00    7089   0.32664E-01   0.20378E+00 
c  k            0.21771E+04    1310   0.99816E-04   0.10179E+01 
c  omega        0.16226E+08     294   0.34872E-04   0.30771E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2182e+05                             1
a  Local Time Step      1.1714e-05                         44424


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.91707          1.1969      0.00038555      1.2984e-06
v  Velocity[Y]                 -23.364          29.653          6.6244          20.056
v  Velocity[Z]                 -29.558           28.99         0.11958      0.00042838
v  ǁVelocityǁ                0.0082551          33.072          10.587          20.213
v  Pressure                    -404.58          345.37          -49.24          31.583
v  k                        6.7801e-08          109.24          4.0377          1.6775
v  omega                         1e-24      1.2054e+07          8112.5          11.884
v  turbulent_viscosity      3.5391e-14          1.2775        0.015673          0.1116
v  CourantNb                  0.013528          2064.2          44.451          1.3763
v  FourierNb                  0.010878           15506          92.706         0.69988
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14868         0.01082         0.04568


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15565          137.16          2.0762


 TIME FOR THE TIME STEP              781:        0.43588E+02

===============================================================


 INSTANT    0.782000000E+02   TIME STEP NUMBER             782
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.551990659E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31590E+02 0.19124E+02
   Friction velocity        uet   :  0.11954E-02 0.25181E+01
   Friction velocity        uk    :  0.25076E-01 0.34694E+01
   Dimensionless distance   yplus :  0.17091E+00 0.34994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        428
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1642   0.46173E-02   0.39957E+00 
c  VelocityY    0.29426E+04    1642   0.46173E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1642   0.46173E-02   0.00000E+00 
c  Pressure     0.44528E+00    6990   0.35274E-01   0.21025E+00 
c  k            0.21724E+04    1424   0.16115E-03   0.89975E+00 
c  omega        0.11776E+08     486   0.13398E-03   0.85388E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0364e+05                             2
a  Local Time Step      1.1567e-05                         44402


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8236          1.0134      -0.0010662     -6.3069e-07
v  Velocity[Y]                 -36.721          30.096          6.5981          20.055
v  Velocity[Z]                 -28.591          28.786         0.12828     -7.2186e-05
v  ǁVelocityǁ                0.0092189          37.497          10.589          20.213
v  Pressure                    -406.34          343.64         -50.891          31.569
v  k                        1.3987e-08           110.5          4.1141          1.6778
v  omega                         1e-24      3.6629e+07          8408.7          11.897
v  turbulent_viscosity      8.3064e-14          1.2809        0.015677         0.11161
v  CourantNb                  0.027292          2068.7          44.533          1.3762
v  FourierNb                  0.010875           15542          93.443         0.70048
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14789        0.010821        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98136           15609          137.98          2.0767


 TIME FOR THE TIME STEP              782:        0.43100E+02

===============================================================


 INSTANT    0.783000000E+02   TIME STEP NUMBER             783
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.257693495E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41614E+02 0.13831E+02
   Friction velocity        uet   :  0.40589E-03 0.34525E+01
   Friction velocity        uk    :  0.13474E-01 0.40239E+01
   Dimensionless distance   yplus :  0.99074E-01 0.38844E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29427E+04    1716   0.44916E-02   0.40435E+00 
c  VelocityY    0.29427E+04    1716   0.44916E-02   0.00000E+00 
c  VelocityZ    0.29427E+04    1716   0.44916E-02   0.00000E+00 
c  Pressure     0.44633E+00    7117   0.38411E-01   0.21241E+00 
c  k            0.21671E+04    1432   0.13457E-03   0.84695E+00 
c  omega        0.14825E+08     407   0.20835E-03   0.24778E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5946e+05                             2
a  Local Time Step      1.0503e-05                         44359


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86085          1.0688      -0.0016091     -2.8496e-06
v  Velocity[Y]                 -23.574          30.644          6.6153          20.056
v  Velocity[Z]                 -28.673          28.673         0.12397     -0.00030577
v  ǁVelocityǁ                0.0066914          33.447          10.583          20.214
v  Pressure                    -407.49          341.38         -53.033          31.697
v  k                        2.0139e-08          52.029          4.1394          1.6783
v  omega                         1e-24      6.4649e+07          9110.9          11.944
v  turbulent_viscosity      7.6357e-14          1.2844        0.015703         0.11162
v  CourantNb                 0.0088796          3018.9          44.759          1.3762
v  FourierNb                  0.010872           15612          93.536         0.70106
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14874        0.010822        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15685          138.29          2.0772


 TIME FOR THE TIME STEP              783:        0.43401E+02

===============================================================


 INSTANT    0.784000000E+02   TIME STEP NUMBER             784
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.286016358E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31996E+02 0.13400E+02
   Friction velocity        uet   :  0.17742E-02 0.26841E+01
   Friction velocity        uk    :  0.16114E-01 0.31424E+01
   Dimensionless distance   yplus :  0.12998E+00 0.27614E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        539
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1941   0.47099E-02   0.41809E+00 
c  VelocityY    0.29426E+04    1941   0.47099E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1941   0.47099E-02   0.00000E+00 
c  Pressure     0.44246E+00    7141   0.36642E-01   0.20909E+00 
c  k            0.21641E+04    1423   0.68016E-04   0.69108E+00 
c  omega        0.29110E+08     262   0.45871E-04   0.10445E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.6694e+05                             2
a  Local Time Step      1.1279e-05                         44288


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93979          1.0797      -0.0025034     -4.0133e-06
v  Velocity[Y]                 -17.587          31.069          6.6469          20.056
v  Velocity[Z]                 -28.772          28.789         0.10062      -0.0007947
v  ǁVelocityǁ                 0.017744          33.647          10.563          20.214
v  Pressure                    -408.75          339.35         -54.766          31.516
v  k                        5.2741e-09          50.303          4.1991           1.679
v  omega                         1e-24      3.3249e+07          8630.4          11.922
v  turbulent_viscosity      2.4678e-14          1.2881        0.015737         0.11165
v  CourantNb                  0.016542          2713.8          44.561          1.3761
v  FourierNb                   0.01087           15622          93.967         0.70154
v  total_pressure           1.0092e+05      1.0166e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14898        0.010822         0.04573


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15703          138.53          2.0776


 TIME FOR THE TIME STEP              784:        0.46059E+02

===============================================================


 INSTANT    0.785000000E+02   TIME STEP NUMBER             785
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.369643193E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30674E+02 0.12908E+02
   Friction velocity        uet   :  0.21532E-02 0.28506E+01
   Friction velocity        uk    :  0.14616E-01 0.28103E+01
   Dimensionless distance   yplus :  0.11473E+00 0.28061E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        555
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29427E+04    1971   0.45239E-02   0.43971E+00 
c  VelocityY    0.29427E+04    1971   0.45239E-02   0.00000E+00 
c  VelocityZ    0.29427E+04    1971   0.45239E-02   0.00000E+00 
c  Pressure     0.43453E+00    7123   0.31840E-01   0.20534E+00 
c  k            0.21639E+04    1388   0.78594E-04   0.73554E+00 
c  omega        0.13955E+08     449   0.16580E-03   0.15592E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1096e-05                         44246


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98511           1.001      -0.0040437     -4.7511e-06
v  Velocity[Y]                 -16.641          32.819          6.6874          20.057
v  Velocity[Z]                 -29.044          29.956        0.071683     -0.00090114
v  ǁVelocityǁ                 0.010669          33.419          10.536          20.215
v  Pressure                    -407.17          341.99         -55.432          31.554
v  k                        1.9465e-08          51.001          4.2481          1.6798
v  omega                         1e-24      7.3874e+07          8791.7          11.919
v  turbulent_viscosity      2.0493e-15          1.2916        0.015797         0.11167
v  CourantNb                  0.047447          2042.2          44.264          1.3762
v  FourierNb                  0.010869           15617          96.193         0.70263
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14917        0.010822        0.045742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15659          140.46          2.0788


 TIME FOR THE TIME STEP              785:        0.46598E+02

===============================================================


 INSTANT    0.786000000E+02   TIME STEP NUMBER             786
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.496149429E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30927E+02 0.16429E+02
   Friction velocity        uet   :  0.25436E-02 0.28699E+01
   Friction velocity        uk    :  0.22986E-01 0.28851E+01
   Dimensionless distance   yplus :  0.22624E+00 0.31492E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :       1002
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1921   0.46801E-02   0.46531E+00 
c  VelocityY    0.29426E+04    1921   0.46801E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1921   0.46801E-02   0.00000E+00 
c  Pressure     0.44120E+00    7000   0.30515E-01   0.20754E+00 
c  k            0.21634E+04    1296   0.67401E-04   0.78191E+00 
c  omega        0.26639E+08     367   0.28486E-03   0.15346E+11 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5393e+05                             1
a  Local Time Step      1.1155e-05                         44324


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.99303          1.0021      -0.0059203     -4.4787e-06
v  Velocity[Y]                 -14.649          32.892          6.7063          20.056
v  Velocity[Z]                 -29.154          28.936        0.042798      -0.0013743
v  ǁVelocityǁ                 0.026777          33.358          10.528          20.215
v  Pressure                    -396.89          341.41         -56.393          31.029
v  k                        4.1984e-07           47.61          4.2402          1.6807
v  omega                         1e-24      7.2469e+08           10543          12.131
v  turbulent_viscosity      6.4044e-15          1.2949        0.015852         0.11171
v  CourantNb                   0.02498          2028.4          44.004          1.3764
v  FourierNb                  0.010869           15804          98.949         0.70382
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14878        0.010821        0.045748


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15854          142.95          2.0802


 TIME FOR THE TIME STEP              786:        0.45106E+02

===============================================================


 INSTANT    0.787000000E+02   TIME STEP NUMBER             787
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.546780761E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31344E+02 0.18117E+02
   Friction velocity        uet   :  0.32858E-02 0.27903E+01
   Friction velocity        uk    :  0.18940E-01 0.32507E+01
   Dimensionless distance   yplus :  0.88438E-01 0.40858E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        471
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    2024   0.46281E-02   0.48188E+00 
c  VelocityY    0.29426E+04    2024   0.46281E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    2024   0.46281E-02   0.00000E+00 
c  Pressure     0.44507E+00    6977   0.31680E-01   0.21187E+00 
c  k            0.21638E+04    1332   0.62120E-04   0.72823E+00 
c  omega        0.45787E+10      16   0.77640E-06   0.38453E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.452e+05                             1
a  Local Time Step      1.0598e-05                         44402


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95899         0.96388      -0.0076731     -3.1688e-06
v  Velocity[Y]                 -15.238          33.945          6.6984          20.057
v  Velocity[Z]                 -28.896          28.963        0.025193      -0.0018218
v  ǁVelocityǁ                0.0082129          34.193          10.536          20.215
v  Pressure                    -379.01          341.51         -57.499          30.542
v  k                        1.4804e-07          41.899          4.2104          1.6819
v  omega                         1e-24      3.6235e+08          9413.7           12.02
v  turbulent_viscosity      9.7538e-14          1.2995         0.01587         0.11176
v  CourantNb                  0.024961          2015.6           43.81          1.3768
v  FourierNb                  0.010869           16019          98.882         0.70397
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010819        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16080          142.69          2.0808


 TIME FOR THE TIME STEP              787:        0.44928E+02

===============================================================


 INSTANT    0.788000000E+02   TIME STEP NUMBER             788
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.654189221E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31975E+02 0.20255E+02
   Friction velocity        uet   :  0.24108E-02 0.27386E+01
   Friction velocity        uk    :  0.11190E-01 0.32309E+01
   Dimensionless distance   yplus :  0.11071E+00 0.33507E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2019   0.45063E-02   0.49361E+00 
c  VelocityY    0.29424E+04    2019   0.45063E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2019   0.45063E-02   0.00000E+00 
c  Pressure     0.44675E+00    6865   0.30660E-01   0.21182E+00 
c  k            0.21662E+04    1523   0.62475E-04   0.76259E+00 
c  omega        0.11450E+10      54   0.16388E-05   0.96776E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4677e+05                             2
a  Local Time Step      1.1835e-05                         44465


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0206         0.80053      -0.0083751     -4.1519e-06
v  Velocity[Y]                  -15.15            30.5          6.7061          20.057
v  Velocity[Z]                 -29.471          29.068        0.019677       -0.002054
v  ǁVelocityǁ                  0.01145          34.431          10.545          20.215
v  Pressure                    -364.28           342.3         -57.325          30.522
v  k                        1.6045e-07          41.939          4.1659          1.6831
v  omega                         1e-24       1.812e+08            8767          11.939
v  turbulent_viscosity      1.4962e-14          1.3046        0.015874         0.11182
v  CourantNb                  0.033596            2021          43.798          1.3774
v  FourierNb                  0.010871           16013          98.626         0.70378
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14941        0.010818        0.045726


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94985           16085          142.42          2.0812


 TIME FOR THE TIME STEP              788:        0.45429E+02

===============================================================


 INSTANT    0.789000000E+02   TIME STEP NUMBER             789
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.584211826E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32150E+02 0.20116E+02
   Friction velocity        uet   :  0.14947E-02 0.27934E+01
   Friction velocity        uk    :  0.15788E-01 0.28318E+01
   Dimensionless distance   yplus :  0.14255E+00 0.27065E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        448
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2011   0.45063E-02   0.48912E+00 
c  VelocityY    0.29423E+04    2011   0.45063E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2011   0.45063E-02   0.00000E+00 
c  Pressure     0.44853E+00    6974   0.29360E-01   0.21251E+00 
c  k            0.21705E+04    1548   0.62082E-04   0.87583E+00 
c  omega        0.28666E+09      76   0.34247E-05   0.24573E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4923e+05                             2
a  Local Time Step      1.1833e-05                         44499


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2242         0.80848      -0.0084656     -4.5896e-06
v  Velocity[Y]                  -15.28          30.331          6.7391          20.056
v  Velocity[Z]                 -31.246          29.132        0.020791      -0.0024072
v  ǁVelocityǁ                 0.012462          36.375          10.575          20.214
v  Pressure                    -349.45           343.3         -56.292          30.715
v  k                        2.3981e-08          48.166          4.1214          1.6845
v  omega                         1e-24       9.064e+07          8336.4          11.881
v  turbulent_viscosity      5.0508e-14          1.3101         0.01586          0.1119
v  CourantNb                  0.025961            2020          44.066          1.3777
v  FourierNb                  0.010874           16228          97.815         0.70329
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14931        0.010818        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78921           16276          141.88           2.081


 TIME FOR THE TIME STEP              789:        0.46157E+02

===============================================================


 INSTANT    0.790000000E+02   TIME STEP NUMBER             790
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.315294896E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31107E+02 0.15998E+02
   Friction velocity        uet   :  0.28036E-02 0.30859E+01
   Friction velocity        uk    :  0.27313E-01 0.29562E+01
   Dimensionless distance   yplus :  0.95176E-01 0.27400E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        387
   Nb of faces within the viscous sub-layer     :       1019
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1956   0.46340E-02   0.48038E+00 
c  VelocityY    0.29423E+04    1956   0.46340E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1956   0.46340E-02   0.00000E+00 
c  Pressure     0.44665E+00    7060   0.32329E-01   0.21159E+00 
c  k            0.21792E+04    1475   0.66919E-04   0.10340E+01 
c  omega        0.72423E+08     148   0.88080E-05   0.76523E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6947e+05                             3
a  Local Time Step      1.1991e-05                         44526


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5087         0.96699      -0.0082917      -4.359e-06
v  Velocity[Y]                 -15.336          30.446          6.7978          20.056
v  Velocity[Z]                 -33.079          28.966        0.034087      -0.0026018
v  ǁVelocityǁ                0.0076681          36.173          10.629          20.214
v  Pressure                    -407.19          344.63         -54.796          31.182
v  k                        2.5471e-08          60.606          4.0823          1.6862
v  omega                         1e-24      4.5333e+07          8158.2          11.851
v  turbulent_viscosity      3.0113e-14          1.3137        0.015838         0.11198
v  CourantNb                  0.033641          2029.4          44.191          1.3778
v  FourierNb                  0.010877           16564           96.94         0.70257
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010817        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16611          141.13          2.0803


 TIME FOR THE TIME STEP              790:        0.46307E+02

===============================================================


 INSTANT    0.791000000E+02   TIME STEP NUMBER             791
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.258035923E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30202E+02 0.13555E+02
   Friction velocity        uet   :  0.12157E-02 0.31431E+01
   Friction velocity        uk    :  0.18168E-01 0.29645E+01
   Dimensionless distance   yplus :  0.93495E-01 0.27983E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1920   0.45152E-02   0.48774E+00 
c  VelocityY    0.29424E+04    1920   0.45152E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1920   0.45152E-02   0.00000E+00 
c  Pressure     0.46303E+00    7113   0.36329E-01   0.21949E+00 
c  k            0.21934E+04    1346   0.69667E-04   0.11427E+01 
c  omega        0.20882E+08     225   0.82016E-04   0.10449E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0998e+05                             1
a  Local Time Step      1.1393e-05                         44550


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7246          1.0595      -0.0077597     -3.2099e-06
v  Velocity[Y]                 -15.705          31.171          6.8704          20.056
v  Velocity[Z]                 -32.972          29.035        0.074086       -0.002749
v  ǁVelocityǁ                0.0074699          35.001          10.693          20.215
v  Pressure                    -435.73          347.75         -53.384            31.5
v  k                        7.4587e-08          66.338          4.0457          1.6878
v  omega                         1e-24      6.7016e+07          8346.5          11.871
v  turbulent_viscosity      5.3831e-14          1.3173        0.015805         0.11208
v  CourantNb                  0.031866          2603.2          44.496          1.3778
v  FourierNb                  0.010882           16676          96.284         0.70189
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1489        0.010815        0.045659


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89184           16726          140.78          2.0797


 TIME FOR THE TIME STEP              791:        0.45768E+02

===============================================================


 INSTANT    0.792000000E+02   TIME STEP NUMBER             792
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.398220960E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31476E+02 0.13804E+02
   Friction velocity        uet   :  0.30188E-03 0.31262E+01
   Friction velocity        uk    :  0.11285E-01 0.31896E+01
   Dimensionless distance   yplus :  0.13971E+00 0.28157E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        323
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1998   0.45831E-02   0.47964E+00 
c  VelocityY    0.29423E+04    1998   0.45831E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1998   0.45831E-02   0.00000E+00 
c  Pressure     0.45287E+00    6954   0.38715E-01   0.21559E+00 
c  k            0.22105E+04    1508   0.70586E-04   0.12105E+01 
c  omega        0.22476E+08     202   0.11958E-03   0.36163E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1461e-05                         44542


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7707          1.0946       -0.006772     -4.5198e-06
v  Velocity[Y]                 -23.814          29.932          6.9146          20.056
v  Velocity[Z]                 -32.226          28.787         0.12359      -0.0028262
v  ǁVelocityǁ                0.0057172           33.57          10.695          20.215
v  Pressure                    -439.43          350.09         -52.039          31.795
v  k                        4.5818e-08          60.996          3.9949          1.6894
v  omega                         1e-24      9.9257e+07          8887.6          11.919
v  turbulent_viscosity      8.3121e-15          1.3216        0.015768         0.11218
v  CourantNb                  0.033625          2771.2          44.906          1.3779
v  FourierNb                  0.010887           16546          95.346         0.70148
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14817        0.010815        0.045662


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92821           16602          140.25          2.0794


 TIME FOR THE TIME STEP              792:        0.45896E+02

===============================================================


 INSTANT    0.793000000E+02   TIME STEP NUMBER             793
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.430968544E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31496E+02 0.16130E+02
   Friction velocity        uet   :  0.47935E-03 0.28474E+01
   Friction velocity        uk    :  0.21972E-01 0.31858E+01
   Dimensionless distance   yplus :  0.12825E+00 0.28306E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        342
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1953   0.45363E-02   0.43845E+00 
c  VelocityY    0.29423E+04    1953   0.45363E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1953   0.45363E-02   0.00000E+00 
c  Pressure     0.43317E+00    7042   0.35823E-01   0.20506E+00 
c  k            0.22261E+04    1583   0.73629E-04   0.12682E+01 
c  omega        0.67226E+08     130   0.23532E-04   0.15388E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6955e+05                             3
a  Local Time Step      1.1195e-05                         44536


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7613          1.0565      -0.0061859     -3.2584e-06
v  Velocity[Y]                 -25.328          29.759          6.8716          20.056
v  Velocity[Z]                 -31.274          28.829         0.17187      -0.0029042
v  ǁVelocityǁ                0.0086833          32.529          10.635          20.215
v  Pressure                    -424.89          351.83         -50.647           31.96
v  k                         1.942e-07          49.197          3.9595          1.6908
v  omega                         1e-24      4.9713e+07          8811.6          11.927
v  turbulent_viscosity      1.1426e-14          1.3255        0.015736          0.1123
v  CourantNb                  0.033803          2255.3          45.093           1.378
v  FourierNb                  0.010893           16330          94.728         0.70118
v  total_pressure            1.009e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14842        0.010814         0.04569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16394          139.82          2.0792


 TIME FOR THE TIME STEP              793:        0.46558E+02

===============================================================


 INSTANT    0.794000000E+02   TIME STEP NUMBER             794
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.193151504E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31198E+02 0.18311E+02
   Friction velocity        uet   :  0.41075E-02 0.27008E+01
   Friction velocity        uk    :  0.30330E-01 0.27447E+01
   Dimensionless distance   yplus :  0.10881E+00 0.27662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        358
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1944   0.44024E-02   0.40021E+00 
c  VelocityY    0.29424E+04    1944   0.44024E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1944   0.44024E-02   0.00000E+00 
c  Pressure     0.41842E+00    7092   0.31393E-01   0.19885E+00 
c  k            0.22350E+04    1587   0.87445E-04   0.12436E+01 
c  omega        0.24701E+08     188   0.31440E-04   0.52606E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.964e+05                             2
a  Local Time Step      1.1394e-05                         44524


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5871          1.0401      -0.0063188     -1.6178e-06
v  Velocity[Y]                 -25.732          29.656          6.7687          20.057
v  Velocity[Z]                 -30.321          28.526         0.17579      -0.0030486
v  ǁVelocityǁ                 0.016717          33.017          10.601          20.216
v  Pressure                     -400.6          351.31          -49.94           31.95
v  k                         4.151e-07          76.237          3.9933          1.6923
v  omega                         1e-24      2.5044e+07          8356.7          11.894
v  turbulent_viscosity      9.7849e-14          1.3294        0.015732         0.11243
v  CourantNb                  0.061157          2046.5          44.864          1.3778
v  FourierNb                  0.010899           16005          94.332         0.70157
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14884        0.010812        0.045661


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16079           139.2          2.0794


 TIME FOR THE TIME STEP              794:        0.45776E+02

===============================================================


 INSTANT    0.795000000E+02   TIME STEP NUMBER             795
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.484258828E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30201E+02 0.17943E+02
   Friction velocity        uet   :  0.15270E-02 0.25689E+01
   Friction velocity        uk    :  0.13305E-01 0.29215E+01
   Dimensionless distance   yplus :  0.11044E+00 0.28323E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1969   0.43839E-02   0.37966E+00 
c  VelocityY    0.29423E+04    1969   0.43839E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1969   0.43839E-02   0.00000E+00 
c  Pressure     0.44147E+00    7026   0.31974E-01   0.20957E+00 
c  k            0.22353E+04    1526   0.98436E-04   0.11479E+01 
c  omega        0.12924E+08     411   0.81920E-04   0.79299E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8352e+05                             2
a  Local Time Step      1.1069e-05                         44499


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5184          1.1266      -0.0061711     -2.2325e-06
v  Velocity[Y]                 -40.881          29.942          6.7031          20.056
v  Velocity[Z]                 -28.575           28.46         0.17684      -0.0030818
v  ǁVelocityǁ                 0.012016          41.167          10.582          20.215
v  Pressure                    -405.41          349.61         -50.143          31.885
v  k                        1.2301e-09          89.625          4.0595          1.6938
v  omega                         1e-24      4.5541e+07          8492.5          11.923
v  turbulent_viscosity      6.7367e-14          1.3314        0.015731         0.11257
v  CourantNb                   0.01656          2024.1          44.753          1.3776
v  FourierNb                  0.010904           15673           93.88         0.70244
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14903        0.010813        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99984           15753          138.63            2.08


 TIME FOR THE TIME STEP              795:        0.46189E+02

===============================================================


 INSTANT    0.796000000E+02   TIME STEP NUMBER             796
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.294341567E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54177E+02 0.13451E+02
   Friction velocity        uet   :  0.13030E-02 0.36738E+01
   Friction velocity        uk    :  0.21046E-01 0.39250E+01
   Dimensionless distance   yplus :  0.12321E+00 0.38464E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2084   0.44424E-02   0.36813E+00 
c  VelocityY    0.29423E+04    2084   0.44424E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2084   0.44424E-02   0.00000E+00 
c  Pressure     0.41736E+00    7105   0.36461E-01   0.19768E+00 
c  k            0.22318E+04    1399   0.10725E-03   0.10465E+01 
c  omega        0.17026E+08     344   0.32773E-04   0.42184E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2667e+05                             2
a  Local Time Step      1.0665e-05                         44483


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4479          1.2725      -0.0053407     -3.3259e-06
v  Velocity[Y]                  -29.14          30.387           6.671          20.056
v  Velocity[Z]                 -28.777          28.486         0.15397      -0.0027945
v  ǁVelocityǁ                0.0096859          33.435           10.56          20.215
v  Pressure                    -407.27          347.73         -51.144          32.055
v  k                        2.3293e-09          40.861          4.0776          1.6953
v  omega                         1e-24       2.295e+07          8313.9          11.914
v  turbulent_viscosity      1.7771e-16          1.3322        0.015738         0.11272
v  CourantNb                  0.047214          2469.9          44.875          1.3775
v  FourierNb                  0.010908           15517          93.178         0.70305
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.148        0.010813        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15588          138.05          2.0806


 TIME FOR THE TIME STEP              796:        0.47285E+02

===============================================================


 INSTANT    0.797000000E+02   TIME STEP NUMBER             797
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.372897553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31107E+02 0.13277E+02
   Friction velocity        uet   :  0.64499E-03 0.29953E+01
   Friction velocity        uk    :  0.16431E-01 0.31434E+01
   Dimensionless distance   yplus :  0.14114E+00 0.28101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    2115   0.44132E-02   0.35800E+00 
c  VelocityY    0.29423E+04    2115   0.44132E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    2115   0.44132E-02   0.00000E+00 
c  Pressure     0.45750E+00    7151   0.38342E-01   0.21644E+00 
c  k            0.22284E+04    1084   0.66548E-04   0.92963E+00 
c  omega        0.11309E+08     325   0.33152E-04   0.17685E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9787e+05                             1
a  Local Time Step      1.1203e-05                         44444


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2978          1.4449       -0.004091     -2.7914e-06
v  Velocity[Y]                 -17.466           32.71          6.6535          20.056
v  Velocity[Z]                 -28.783          28.313          0.1136      -0.0028651
v  ǁVelocityǁ                0.0045716           33.36          10.531          20.216
v  Pressure                    -408.38          347.86         -52.373          32.035
v  k                        6.3828e-10          50.179          4.1286          1.6968
v  omega                         1e-24      1.1873e+07          8121.8          11.894
v  turbulent_viscosity      2.1296e-15          1.3336        0.015757         0.11287
v  CourantNb                  0.032541            2977          44.789          1.3773
v  FourierNb                  0.010911           15539          92.309         0.70354
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14801        0.010813        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15584           137.1          2.0808


 TIME FOR THE TIME STEP              797:        0.47033E+02

===============================================================


 INSTANT    0.798000000E+02   TIME STEP NUMBER             798
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.755955730E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30611E+02 0.13523E+02
   Friction velocity        uet   :  0.74189E-03 0.29657E+01
   Friction velocity        uk    :  0.18644E-01 0.28845E+01
   Dimensionless distance   yplus :  0.17091E+00 0.28311E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        587
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2053   0.45706E-02   0.36120E+00 
c  VelocityY    0.29424E+04    2053   0.45706E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2053   0.45706E-02   0.00000E+00 
c  Pressure     0.41144E+00    7074   0.35934E-01   0.19475E+00 
c  k            0.22263E+04    1155   0.65365E-04   0.90989E+00 
c  omega        0.10206E+08     243   0.41752E-04   0.29259E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3695e+05                             1
a  Local Time Step      1.1162e-05                         44434


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2188          1.5056      -0.0027488     -2.4522e-06
v  Velocity[Y]                  -18.01          33.384           6.661          20.056
v  Velocity[Z]                 -29.164          29.357        0.060295      -0.0027861
v  ǁVelocityǁ                0.0060384          34.044          10.508          20.215
v  Pressure                    -407.26          347.69         -53.256          31.895
v  k                        4.1839e-08          48.849          4.1961          1.6983
v  omega                         1e-24      1.6885e+07          8038.6          11.878
v  turbulent_viscosity      2.0256e-15          1.3335          0.0158         0.11303
v  CourantNb                  0.021822          2056.9            44.3           1.377
v  FourierNb                  0.010909           15566          92.823          0.7045
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010813        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15616          137.12          2.0815


 TIME FOR THE TIME STEP              798:        0.46048E+02

===============================================================


 INSTANT    0.799000000E+02   TIME STEP NUMBER             799
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.228457905E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30127E+02 0.14805E+02
   Friction velocity        uet   :  0.92105E-04 0.29594E+01
   Friction velocity        uk    :  0.10696E-01 0.29422E+01
   Dimensionless distance   yplus :  0.92042E-01 0.31426E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        500
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29425E+04    2046   0.46334E-02   0.37625E+00 
c  VelocityY    0.29425E+04    2046   0.46334E-02   0.00000E+00 
c  VelocityZ    0.29425E+04    2046   0.46334E-02   0.00000E+00 
c  Pressure     0.45274E+00    7026   0.33507E-01   0.21519E+00 
c  k            0.22248E+04    1421   0.72039E-04   0.10301E+01 
c  omega        0.10746E+08     364   0.31519E-04   0.19470E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5586e+05                             2
a  Local Time Step      1.1118e-05                         44414


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0683          1.3558      -0.0016393      1.9124e-06
v  Velocity[Y]                 -19.004          33.542           6.683          20.056
v  Velocity[Z]                 -28.438          28.665       0.0081758      -0.0023934
v  ǁVelocityǁ                  0.01056          33.845            10.5          20.216
v  Pressure                    -399.27          346.74         -54.299          31.677
v  k                        6.0566e-08          50.472          4.2077          1.6998
v  omega                         1e-24      1.1675e+07          8144.4          11.873
v  turbulent_viscosity      7.1261e-14          1.3318        0.015873         0.11319
v  CourantNb                  0.036324            2078          43.736          1.3769
v  FourierNb                  0.010906           15579          95.295         0.70641
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14873        0.010812        0.045648


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15638          139.03          2.0833


 TIME FOR THE TIME STEP              799:        0.46588E+02

===============================================================


 INSTANT    0.800000000E+02   TIME STEP NUMBER             800
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.343351290E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31949E+02 0.13960E+02
   Friction velocity        uet   :  0.70097E-03 0.28674E+01
   Friction velocity        uk    :  0.66224E-02 0.29855E+01
   Dimensionless distance   yplus :  0.87345E-01 0.34664E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1949   0.46312E-02   0.38613E+00 
c  VelocityY    0.29424E+04    1949   0.46312E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1949   0.46312E-02   0.00000E+00 
c  Pressure     0.44772E+00    6933   0.30745E-01   0.21159E+00 
c  k            0.22228E+04    1509   0.72696E-04   0.10063E+01 
c  omega        0.19246E+17       2   0.14323E-12   0.23246E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.708e+05                             3
a  Local Time Step      1.0956e-05                         44408


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0068          1.2696     -0.00057855      5.2249e-07
v  Velocity[Y]                 -17.564          33.457          6.6757          20.056
v  Velocity[Z]                 -28.589          28.869       -0.041607      -0.0024948
v  ǁVelocityǁ                 0.012917          33.785           10.51          20.216
v  Pressure                    -383.93          344.93         -55.469          31.122
v  k                        1.7081e-08          39.178            4.17          1.7012
v  omega                         1e-24      1.1927e+07          8197.4           11.88
v  turbulent_viscosity      5.0121e-14          1.3302        0.015927         0.11334
v  CourantNb                  0.047991          2083.8          43.537           1.377
v  FourierNb                  0.010903           15549          96.977         0.70795
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010811        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15617          140.51           2.085


 TIME FOR THE TIME STEP              800:        0.45255E+02

===============================================================


 INSTANT    0.801000000E+02   TIME STEP NUMBER             801
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.275249312E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31995E+02 0.20427E+02
   Friction velocity        uet   :  0.97265E-03 0.27473E+01
   Friction velocity        uk    :  0.22973E-01 0.32374E+01
   Dimensionless distance   yplus :  0.16464E+00 0.35330E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        495
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1763   0.44332E-02   0.38521E+00 
c  VelocityY    0.29423E+04    1763   0.44332E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1763   0.44332E-02   0.00000E+00 
c  Pressure     0.44121E+00    6950   0.29050E-01   0.21009E+00 
c  k            0.22203E+04    1560   0.68768E-04   0.10622E+01 
c  omega        0.16838E+28       2   0.16325E-15   0.18385E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9759e+05                             3
a  Local Time Step      1.1644e-05                         44375


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1306          1.2093      0.00034119     -5.4992e-08
v  Velocity[Y]                 -15.858          31.062          6.6607          20.056
v  Velocity[Z]                 -28.559          28.988       -0.060746      -0.0022122
v  ǁVelocityǁ                 0.012783          33.272          10.514          20.216
v  Pressure                    -370.21          343.73         -55.826          30.782
v  k                        1.2538e-09          39.242          4.1301          1.7026
v  omega                         1e-24      1.3872e+07            8113          11.858
v  turbulent_viscosity      1.7602e-14          1.3292        0.015907          0.1135
v  CourantNb                  0.018343          2078.2          43.482          1.3774
v  FourierNb                  0.010899           15538          96.685          0.7082
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1482        0.010812        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15581          140.17          2.0856


 TIME FOR THE TIME STEP              801:        0.43143E+02

===============================================================


 INSTANT    0.802000000E+02   TIME STEP NUMBER             802
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.158405486E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32467E+02 0.20339E+02
   Friction velocity        uet   :  0.72712E-03 0.26620E+01
   Friction velocity        uk    :  0.20202E-01 0.28219E+01
   Dimensionless distance   yplus :  0.16392E+00 0.29354E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        446
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1796   0.45437E-02   0.39025E+00 
c  VelocityY    0.29422E+04    1796   0.45437E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1796   0.45437E-02   0.00000E+00 
c  Pressure     0.42679E+00    6974   0.28341E-01   0.20245E+00 
c  k            0.22178E+04    1517   0.73790E-04   0.12384E+01 
c  omega        0.98082E+27       2   0.14013E-15   0.10137E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1463e+05                             1
a  Local Time Step      1.1819e-05                         44349


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2443          1.0998       0.0016117      1.5798e-06
v  Velocity[Y]                 -15.301          30.338          6.6757          20.056
v  Velocity[Z]                 -31.094          29.291       -0.077571      -0.0018613
v  ǁVelocityǁ                 0.013404          36.686          10.521          20.215
v  Pressure                    -345.18          345.78         -54.499          31.003
v  k                        7.3965e-10          49.349           4.112          1.7041
v  omega                         1e-24      1.1691e+07          7949.6          11.842
v  turbulent_viscosity      1.2241e-15           1.326        0.015903         0.11364
v  CourantNb                  0.050458            2063          43.685          1.3776
v  FourierNb                  0.010895           16037          96.115         0.70857
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14838        0.010812        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16080           139.8          2.0862


 TIME FOR THE TIME STEP              802:        0.43997E+02

===============================================================


 INSTANT    0.803000000E+02   TIME STEP NUMBER             803
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.310612507E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30084E+02 0.20659E+02
   Friction velocity        uet   :  0.11707E-02 0.30728E+01
   Friction velocity        uk    :  0.21363E-01 0.29584E+01
   Dimensionless distance   yplus :  0.12934E+00 0.28491E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1980   0.45314E-02   0.38627E+00 
c  VelocityY    0.29423E+04    1980   0.45314E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1980   0.45314E-02   0.00000E+00 
c  Pressure     0.43235E+00    7077   0.31739E-01   0.20458E+00 
c  k            0.22185E+04    1328   0.81616E-04   0.13727E+01 
c  omega        0.11541E+08     297   0.24949E-04   0.88941E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8112e+05                             2
a  Local Time Step      1.2029e-05                         44390


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3945          1.2332       0.0030385     -1.3775e-06
v  Velocity[Y]                 -15.327          32.524          6.7158          20.056
v  Velocity[Z]                 -32.408          29.151        -0.08766      -0.0014045
v  ǁVelocityǁ                 0.015075          36.851          10.547          20.216
v  Pressure                    -399.08          349.09         -52.814          31.266
v  k                        4.1927e-08          58.712          4.0916          1.7056
v  omega                         1e-24       1.169e+07            7843           11.85
v  turbulent_viscosity        2.29e-15          1.3251        0.015936         0.11378
v  CourantNb                  0.039599          2040.7          43.814          1.3777
v  FourierNb                  0.010891           16518          95.678          0.7095
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1488        0.010813        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16566          139.49          2.0872


 TIME FOR THE TIME STEP              803:        0.46630E+02

===============================================================


 INSTANT    0.804000000E+02   TIME STEP NUMBER             804
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.498933293E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30504E+02 0.16877E+02
   Friction velocity        uet   :  0.17814E-02 0.31790E+01
   Friction velocity        uk    :  0.18441E-01 0.32436E+01
   Dimensionless distance   yplus :  0.17163E+00 0.28609E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        365
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29423E+04    1982   0.45024E-02   0.39784E+00 
c  VelocityY    0.29423E+04    1982   0.45024E-02   0.00000E+00 
c  VelocityZ    0.29423E+04    1982   0.45024E-02   0.00000E+00 
c  Pressure     0.44243E+00    7118   0.36542E-01   0.20930E+00 
c  k            0.22267E+04    1406   0.80505E-04   0.14782E+01 
c  omega        0.61668E+27       2   0.22341E-22   0.11860E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5567e+05                             3
a  Local Time Step      1.1632e-05                         44432


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5827          1.4729       0.0037236      -2.483e-06
v  Velocity[Y]                 -15.397          32.863           6.774          20.057
v  Velocity[Z]                  -33.27          29.071       -0.068213      -0.0011357
v  ǁVelocityǁ                 0.020706          35.786          10.585          20.217
v  Pressure                    -432.64          351.16         -51.424          31.408
v  k                        3.3175e-08          67.246          4.0268           1.707
v  omega                         1e-24      1.5824e+07          7740.1          11.836
v  turbulent_viscosity      8.8792e-14           1.319        0.015942         0.11392
v  CourantNb                  0.027505          2498.3          43.874          1.3776
v  FourierNb                  0.010889           16338          95.189         0.70975
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14888        0.010814        0.045706


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16395          139.06          2.0874


 TIME FOR THE TIME STEP              804:        0.45685E+02

===============================================================


 INSTANT    0.805000000E+02   TIME STEP NUMBER             805
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.268330451E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30944E+02 0.15217E+02
   Friction velocity        uet   :  0.16339E-02 0.32571E+01
   Friction velocity        uk    :  0.12819E-01 0.34373E+01
   Dimensionless distance   yplus :  0.16807E+00 0.28648E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        330
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1943   0.47416E-02   0.40266E+00 
c  VelocityY    0.29422E+04    1943   0.47416E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1943   0.47416E-02   0.00000E+00 
c  Pressure     0.44985E+00    7126   0.37679E-01   0.21255E+00 
c  k            0.22385E+04    1605   0.82697E-04   0.15782E+01 
c  omega        0.99727E+07     276   0.23311E-03   0.18065E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7777e+05                             2
a  Local Time Step      1.0734e-05                         44433


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6932          1.4633       0.0035757     -1.0686e-06
v  Velocity[Y]                  -20.32          30.001          6.8186          20.056
v  Velocity[Z]                 -32.977          28.813       -0.018326     -0.00045124
v  ǁVelocityǁ                  0.01395          34.465          10.599          20.216
v  Pressure                    -441.43          352.15         -50.209          31.567
v  k                        1.2603e-07          62.866          3.9585          1.7083
v  omega                         1e-24      7.0354e+07          8288.5          11.893
v  turbulent_viscosity      3.0188e-14          1.3161         0.01592         0.11405
v  CourantNb                  0.015309          2788.8          44.121          1.3775
v  FourierNb                  0.010886           16113          93.722         0.70981
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14854        0.010816        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16179          137.84          2.0873


 TIME FOR THE TIME STEP              805:        0.45696E+02

===============================================================


 INSTANT    0.806000000E+02   TIME STEP NUMBER             806
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.323308299E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31643E+02 0.14555E+02
   Friction velocity        uet   :  0.12657E-02 0.29305E+01
   Friction velocity        uk    :  0.23624E-01 0.31040E+01
   Dimensionless distance   yplus :  0.16222E+00 0.28012E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        370
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1792   0.46714E-02   0.38756E+00 
c  VelocityY    0.29422E+04    1792   0.46714E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1792   0.46714E-02   0.00000E+00 
c  Pressure     0.44801E+00    7077   0.35311E-01   0.21238E+00 
c  k            0.22531E+04    1590   0.78187E-04   0.15426E+01 
c  omega        0.31101E+08     146   0.58910E-04   0.12549E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5174e+05                             1
a  Local Time Step      1.1518e-05                         44440


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6926          1.2241       0.0031445     -3.9856e-08
v  Velocity[Y]                 -24.954          29.858            6.81          20.056
v  Velocity[Z]                 -32.465          28.737        0.023015      7.4275e-05
v  ǁVelocityǁ                0.0089261          33.237          10.575          20.217
v  Pressure                    -431.69          352.08         -49.246          31.698
v  k                        3.5789e-07          51.748          3.9076          1.7095
v  omega                         1e-24       3.948e+07          8371.3          11.908
v  turbulent_viscosity      6.5946e-14          1.3095        0.015885         0.11418
v  CourantNb                   0.02016          2514.7           44.35          1.3775
v  FourierNb                  0.010885           15633          92.689          0.7102
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14851        0.010818        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15707          137.04          2.0877


 TIME FOR THE TIME STEP              806:        0.43705E+02

===============================================================


 INSTANT    0.807000000E+02   TIME STEP NUMBER             807
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.519356796E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31221E+02 0.16493E+02
   Friction velocity        uet   :  0.16809E-02 0.28227E+01
   Friction velocity        uk    :  0.16077E-01 0.28493E+01
   Dimensionless distance   yplus :  0.14666E+00 0.27352E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :       1066
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1655   0.47001E-02   0.36264E+00 
c  VelocityY    0.29421E+04    1655   0.47001E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1655   0.47001E-02   0.00000E+00 
c  Pressure     0.44663E+00    7092   0.31956E-01   0.21185E+00 
c  k            0.22600E+04    1513   0.77826E-04   0.15298E+01 
c  omega        0.18524E+08     247   0.44914E-04   0.70913E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.6167e-05                             1
a  omega               -1.1983e+05                             1
a  Local Time Step      1.1404e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5288          1.1597       0.0027626      7.9604e-07
v  Velocity[Y]                 -36.987          29.689          6.7358          20.056
v  Velocity[Z]                  -29.17           28.66        0.044281      0.00033566
v  ǁVelocityǁ                0.0070616          37.115          10.561          20.217
v  Pressure                    -406.64          351.32         -48.543          31.761
v  k                        2.0407e-08           70.68          3.9334          1.7105
v  omega                         1e-24      1.9741e+07          8228.1          11.924
v  turbulent_viscosity      3.9835e-14          1.3016        0.015855          0.1143
v  CourantNb                  0.017878          2021.2          44.538          1.3774
v  FourierNb                  0.010884           15123           92.49         0.71105
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14925        0.010821        0.045746


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96922           15201          137.03          2.0884


 TIME FOR THE TIME STEP              807:        0.42666E+02

===============================================================


 INSTANT    0.808000000E+02   TIME STEP NUMBER             808
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.419980756E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30610E+02 0.25316E+02
   Friction velocity        uet   :  0.68121E-03 0.31517E+01
   Friction velocity        uk    :  0.19157E-01 0.29193E+01
   Dimensionless distance   yplus :  0.12341E+00 0.28841E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        379
   Nb of faces within the viscous sub-layer     :       1056
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1717   0.44565E-02   0.35026E+00 
c  VelocityY    0.29421E+04    1717   0.44565E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1717   0.44565E-02   0.00000E+00 
c  Pressure     0.43604E+00    7062   0.32122E-01   0.20570E+00 
c  k            0.22586E+04    1391   0.10247E-03   0.14576E+01 
c  omega        0.12416E+08     373   0.11980E-03   0.12197E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -1.2862e-06                             1
a  omega               -1.9235e+05                             1
a  Local Time Step      1.1432e-05                         44388


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2964          1.0166       0.0022349      4.3455e-06
v  Velocity[Y]                 -31.254          29.835           6.667          20.056
v  Velocity[Z]                 -28.625          28.521        0.051986      0.00091828
v  ǁVelocityǁ                0.0074588          38.457          10.574          20.217
v  Pressure                    -405.62          349.13         -49.087           31.73
v  k                        4.7409e-10          109.06          4.0149          1.7113
v  omega                         1e-24       5.751e+07          8441.6          11.909
v  turbulent_viscosity      4.1353e-14          1.2913         0.01584         0.11441
v  CourantNb                  0.040051          2120.6          44.579          1.3772
v  FourierNb                  0.010883           14981          92.115          0.7121
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010822        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15022          136.69          2.0893


 TIME FOR THE TIME STEP              808:        0.42965E+02

===============================================================


 INSTANT    0.809000000E+02   TIME STEP NUMBER             809
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.484151393E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.54093E+02 0.16313E+02
   Friction velocity        uet   :  0.34062E-02 0.33371E+01
   Friction velocity        uk    :  0.11174E-01 0.47382E+01
   Dimensionless distance   yplus :  0.95878E-01 0.39505E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        432
   Nb of faces within the viscous sub-layer     :       1076
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29420E+04    1797   0.44847E-02   0.35594E+00 
c  VelocityY    0.29420E+04    1797   0.44847E-02   0.00000E+00 
c  VelocityZ    0.29420E+04    1797   0.44847E-02   0.00000E+00 
c  Pressure     0.45068E+00    7054   0.35405E-01   0.21179E+00 
c  k            0.22505E+04    1215   0.13176E-03   0.13441E+01 
c  omega        0.19018E+08     439   0.15816E-02   0.61307E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1103e-05                         44308


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0642         0.85953       0.0011263       7.214e-06
v  Velocity[Y]                 -31.642          30.221          6.6631          20.056
v  Velocity[Z]                 -28.797          28.639        0.060288       0.0012349
v  ǁVelocityǁ                0.0048258          33.372          10.592          20.217
v  Pressure                    -406.41          349.51         -50.772          31.538
v  k                        5.9695e-09           77.63          4.0684           1.712
v  omega                         1e-24      2.9392e+08           11268          12.559
v  turbulent_viscosity       2.424e-15          1.2823         0.01584         0.11451
v  CourantNb                  0.030086          2007.1          44.628          1.3772
v  FourierNb                  0.010883           14877          92.051         0.71358
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14889        0.010822        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.80597           14922          136.68          2.0908


 TIME FOR THE TIME STEP              809:        0.43481E+02

===============================================================


 INSTANT    0.810000000E+02   TIME STEP NUMBER             810
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.617279098E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31120E+02 0.13883E+02
   Friction velocity        uet   :  0.12522E-02 0.30640E+01
   Friction velocity        uk    :  0.15347E-01 0.35318E+01
   Dimensionless distance   yplus :  0.11790E+00 0.31194E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        489
   Nb of faces within the viscous sub-layer     :       1067
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1827   0.47657E-02   0.36463E+00 
c  VelocityY    0.29419E+04    1827   0.47657E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1827   0.47657E-02   0.00000E+00 
c  Pressure     0.42679E+00    7116   0.36482E-01   0.20022E+00 
c  k            0.22400E+04    1159   0.87384E-04   0.12762E+01 
c  omega        0.11151E+10      83   0.38072E-05   0.17087E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3198e+05                             1
a  Local Time Step      1.0946e-05                         44311


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95862         0.70492      0.00030715      6.9134e-06
v  Velocity[Y]                 -17.866          30.611          6.6823          20.056
v  Velocity[Z]                 -29.242          28.732        0.057898       0.0016274
v  ǁVelocityǁ                0.0052585          33.278          10.589          20.217
v  Pressure                    -406.53          349.75         -52.281          31.929
v  k                         1.203e-08          50.491          4.1045          1.7125
v  omega                         1e-24      1.4695e+08           10304          12.256
v  turbulent_viscosity      1.2475e-14          1.2735        0.015853          0.1146
v  CourantNb                  0.018718          2978.8          44.785          1.3772
v  FourierNb                  0.010883           14893          92.181         0.71476
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14848        0.010823        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93802           14944          136.97          2.0919


 TIME FOR THE TIME STEP              810:        0.43839E+02

===============================================================


 INSTANT    0.811000000E+02   TIME STEP NUMBER             811
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.456927672E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31397E+02 0.13981E+02
   Friction velocity        uet   :  0.61852E-03 0.26892E+01
   Friction velocity        uk    :  0.21097E-01 0.31855E+01
   Dimensionless distance   yplus :  0.94319E-01 0.28294E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        542
   Nb of faces within the viscous sub-layer     :       1068
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    2018   0.47306E-02   0.38290E+00 
c  VelocityY    0.29419E+04    2018   0.47306E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    2018   0.47306E-02   0.00000E+00 
c  Pressure     0.45778E+00    7111   0.33217E-01   0.21542E+00 
c  k            0.22298E+04    1415   0.69542E-04   0.11719E+01 
c  omega        0.27956E+09     104   0.71367E-05   0.44465E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -84848                             1
a  Local Time Step      1.1834e-05                         44349


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90619         0.66313      0.00065045      8.2861e-06
v  Velocity[Y]                 -17.548          31.725          6.7075          20.056
v  Velocity[Z]                 -28.581          28.618        0.048266       0.0019412
v  ǁVelocityǁ                0.0061378          33.778          10.576          20.218
v  Pressure                    -406.62          349.55         -53.207          31.872
v  k                        1.3324e-08          50.135          4.1728           1.713
v  omega                         1e-24      7.3461e+07          9112.9          12.064
v  turbulent_viscosity      2.5669e-14          1.2652        0.015906         0.11468
v  CourantNb                  0.015793          2307.3          44.496          1.3771
v  FourierNb                  0.010884           14878          93.889         0.71637
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010824        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91366           14936          138.39          2.0935


 TIME FOR THE TIME STEP              811:        0.48534E+02

===============================================================


 INSTANT    0.812000000E+02   TIME STEP NUMBER             812
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.332348068E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31936E+02 0.14237E+02
   Friction velocity        uet   :  0.68660E-03 0.28782E+01
   Friction velocity        uk    :  0.20967E-01 0.29309E+01
   Dimensionless distance   yplus :  0.15613E+00 0.28294E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        526
   Nb of faces within the viscous sub-layer     :       1072
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1801   0.44635E-02   0.40533E+00 
c  VelocityY    0.29418E+04    1801   0.44635E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1801   0.44635E-02   0.00000E+00 
c  Pressure     0.45434E+00    7083   0.30186E-01   0.21575E+00 
c  k            0.22204E+04    1509   0.73287E-04   0.12653E+01 
c  omega        0.70800E+08     300   0.13950E-04   0.11595E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1824e+05                             1
a  Local Time Step       1.187e-05                         44356


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89041         0.59198       0.0017449      4.8375e-06
v  Velocity[Y]                 -15.813          32.909          6.7254          20.056
v  Velocity[Z]                 -28.733          29.061        0.038109       0.0018353
v  ǁVelocityǁ                0.0070201          33.661          10.552          20.217
v  Pressure                    -402.32          348.51         -53.717          31.759
v  k                        1.6037e-10          55.143           4.176          1.7132
v  omega                         1e-24      3.6718e+07          8545.4          11.961
v  turbulent_viscosity       1.451e-14          1.2589        0.015973         0.11474
v  CourantNb                  0.025418          2027.1          44.129          1.3771
v  FourierNb                  0.010884           14711          96.703         0.71828
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14901        0.010824        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14777          140.83          2.0954


 TIME FOR THE TIME STEP              812:        0.44748E+02

===============================================================


 INSTANT    0.813000000E+02   TIME STEP NUMBER             813
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.384654933E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32146E+02 0.14639E+02
   Friction velocity        uet   :  0.27278E-02 0.28503E+01
   Friction velocity        uk    :  0.22063E-01 0.30722E+01
   Dimensionless distance   yplus :  0.56072E-01 0.32045E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :       1051
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1678   0.44771E-02   0.42240E+00 
c  VelocityY    0.29417E+04    1678   0.44771E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1678   0.44771E-02   0.00000E+00 
c  Pressure     0.41349E+00    6770   0.30944E-01   0.19726E+00 
c  k            0.22097E+04    1499   0.69838E-04   0.12622E+01 
c  omega        0.24276E+08     277   0.70876E-03   0.60226E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -76985                             2
a  Local Time Step      1.0925e-05                         44364


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.87792         0.62046       0.0035539      3.9378e-06
v  Velocity[Y]                 -15.335          33.294          6.7008          20.056
v  Velocity[Z]                 -28.789          28.821         0.02907       0.0016772
v  ǁVelocityǁ                0.0048385          33.748          10.545          20.218
v  Pressure                     -385.9          346.11         -54.736          31.213
v  k                        1.4351e-09          43.026           4.133          1.7133
v  omega                         1e-24      6.7804e+08           10204          12.019
v  turbulent_viscosity      3.9987e-17          1.2535        0.015984         0.11479
v  CourantNb                  0.036623            2021          43.829          1.3772
v  FourierNb                  0.010886           14747          96.375         0.71871
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14777        0.010821        0.045692


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14787           140.2          2.0959


 TIME FOR THE TIME STEP              813:        0.42549E+02

===============================================================


 INSTANT    0.814000000E+02   TIME STEP NUMBER             814
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.330029222E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31176E+02 0.22891E+02
   Friction velocity        uet   :  0.23901E-02 0.27429E+01
   Friction velocity        uk    :  0.23288E-01 0.31703E+01
   Dimensionless distance   yplus :  0.13904E+00 0.36427E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :        976
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1783   0.44905E-02   0.42775E+00 
c  VelocityY    0.29415E+04    1783   0.44905E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1783   0.44905E-02   0.00000E+00 
c  Pressure     0.41643E+00    6985   0.30269E-01   0.19758E+00 
c  k            0.22004E+04    1434   0.68174E-04   0.12460E+01 
c  omega        0.17882E+10      50   0.40756E-05   0.15116E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0764e+05                             2
a  Local Time Step      1.1656e-05                         44338


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.78681         0.73613       0.0050579      1.9674e-06
v  Velocity[Y]                 -15.681          31.799          6.6757          20.057
v  Velocity[Z]                 -28.858          29.287        0.031323       0.0012422
v  ǁVelocityǁ                 0.011269          32.782          10.535          20.218
v  Pressure                    -369.62          344.65         -55.047          31.017
v  k                        9.6414e-09          43.804          4.0682          1.7132
v  omega                         1e-24       3.391e+08          9020.4          11.917
v  turbulent_viscosity      2.6606e-15          1.2497         0.01596         0.11483
v  CourantNb                  0.040443          2020.3          43.704          1.3776
v  FourierNb                  0.010889           14875          95.301         0.71842
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14895        0.010818        0.045666


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14916          139.01           2.096


 TIME FOR THE TIME STEP              814:        0.43538E+02

===============================================================


 INSTANT    0.815000000E+02   TIME STEP NUMBER             815
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.422731711E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30715E+02 0.20913E+02
   Friction velocity        uet   :  0.48598E-03 0.25454E+01
   Friction velocity        uk    :  0.22204E-01 0.32479E+01
   Dimensionless distance   yplus :  0.10541E+00 0.28549E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        468
   Nb of faces within the viscous sub-layer     :        957
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1921   0.44146E-02   0.42574E+00 
c  VelocityY    0.29414E+04    1921   0.44146E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1921   0.44146E-02   0.00000E+00 
c  Pressure     0.44708E+00    7025   0.27352E-01   0.21191E+00 
c  k            0.21927E+04    1278   0.69535E-04   0.13294E+01 
c  omega        0.44774E+09      66   0.81425E-05   0.38582E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3532e+05                             3
a  Local Time Step      1.1645e-05                         44332


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.78129         0.93049       0.0059623      3.4664e-07
v  Velocity[Y]                 -15.256          30.317          6.6812          20.057
v  Velocity[Z]                 -30.072          29.116        0.038911       0.0012631
v  ǁVelocityǁ                0.0090196          36.105          10.532          20.218
v  Pressure                    -347.84          347.37         -54.001          31.276
v  k                        6.3326e-08          44.362          3.9956          1.7131
v  omega                         1e-24       1.697e+08            8423          11.871
v  turbulent_viscosity      3.0188e-14          1.2458        0.015923         0.11486
v  CourantNb                  0.034878          2040.3          44.041          1.3779
v  FourierNb                  0.010892           15218          95.187         0.71796
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14843        0.010818        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15264          139.23          2.0959


 TIME FOR THE TIME STEP              815:        0.44530E+02

===============================================================


 INSTANT    0.816000000E+02   TIME STEP NUMBER             816
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.427095188E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31460E+02 0.19731E+02
   Friction velocity        uet   :  0.94064E-03 0.29048E+01
   Friction velocity        uk    :  0.19395E-01 0.28954E+01
   Dimensionless distance   yplus :  0.11143E+00 0.28759E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        396
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    1878   0.45066E-02   0.42009E+00 
c  VelocityY    0.29412E+04    1878   0.45066E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    1878   0.45066E-02   0.00000E+00 
c  Pressure     0.45262E+00    7099   0.28655E-01   0.21394E+00 
c  k            0.21880E+04    1183   0.71780E-04   0.14472E+01 
c  omega        0.11292E+09     173   0.17209E-04   0.12973E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0464e+05                             2
a  Local Time Step      1.1569e-05                         44411


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85843          1.1115       0.0064059      1.0455e-06
v  Velocity[Y]                 -16.058           30.25          6.7245          20.056
v  Velocity[Z]                 -31.319          29.293         0.04619       0.0013755
v  ǁVelocityǁ                 0.019107           36.14          10.556          20.217
v  Pressure                    -374.86           349.7         -52.486          31.468
v  k                        2.0048e-08          54.744          3.9295          1.7129
v  omega                         1e-24      8.5168e+07          8295.1          11.876
v  turbulent_viscosity      1.9094e-13          1.2422        0.015862         0.11486
v  CourantNb                  0.023511            2071          44.251          1.3779
v  FourierNb                  0.010894           15408          93.199         0.71651
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14907        0.010818        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15464          137.45          2.0944


 TIME FOR THE TIME STEP              816:        0.44535E+02

===============================================================


 INSTANT    0.817000000E+02   TIME STEP NUMBER             817
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.130254903E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31096E+02 0.14398E+02
   Friction velocity        uet   :  0.55471E-03 0.30487E+01
   Friction velocity        uk    :  0.11095E-01 0.29710E+01
   Dimensionless distance   yplus :  0.97684E-01 0.28847E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :       1003
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1885   0.45274E-02   0.42120E+00 
c  VelocityY    0.29410E+04    1885   0.45274E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1885   0.45274E-02   0.00000E+00 
c  Pressure     0.46701E+00    7138   0.33368E-01   0.22102E+00 
c  k            0.21892E+04    1478   0.74103E-04   0.15548E+01 
c  omega        0.31470E+08     241   0.50189E-03   0.53447E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6691e+05                             2
a  Local Time Step       1.115e-05                         44476


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90744          1.3707        0.006222      1.4254e-06
v  Velocity[Y]                 -15.212          31.599          6.8038          20.056
v  Velocity[Z]                   -33.3          29.126        0.068835      0.00093833
v  ǁVelocityǁ                0.0086655          35.789           10.61          20.217
v  Pressure                    -418.55          351.23         -50.676          31.882
v  k                        7.8959e-08          63.607           3.884          1.7126
v  omega                         1e-24      5.8143e+08           10802          12.058
v  turbulent_viscosity      9.5294e-14           1.238        0.015804         0.11486
v  CourantNb                  0.006366          2339.5          44.436          1.3778
v  FourierNb                   0.01089           15347          91.529         0.71507
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1484        0.010818        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15412          135.96          2.0928


 TIME FOR THE TIME STEP              817:        0.46014E+02

===============================================================


 INSTANT    0.818000000E+02   TIME STEP NUMBER             818
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.831139313E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30320E+02 0.14491E+02
   Friction velocity        uet   :  0.45155E-03 0.31636E+01
   Friction velocity        uk    :  0.19096E-01 0.31910E+01
   Dimensionless distance   yplus :  0.92194E-01 0.28072E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        378
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    1808   0.44385E-02   0.42320E+00 
c  VelocityY    0.29409E+04    1808   0.44385E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    1808   0.44385E-02   0.00000E+00 
c  Pressure     0.45272E+00    7129   0.36764E-01   0.21489E+00 
c  k            0.21967E+04    1520   0.74652E-04   0.15963E+01 
c  omega        0.13285E+10      50   0.40386E-05   0.15203E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6495e+05                             3
a  Local Time Step      1.1197e-05                         44496


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.91871           1.536       0.0055126      1.7491e-06
v  Velocity[Y]                 -18.196           29.92          6.8825          20.056
v  Velocity[Z]                 -32.781          29.321         0.11207      0.00024636
v  ǁVelocityǁ                0.0049949          34.564          10.651          20.218
v  Pressure                    -434.57          351.07         -49.293          32.272
v  k                        1.8739e-08          64.748          3.8444           1.712
v  omega                         1e-24      2.9078e+08          9850.4          12.001
v  turbulent_viscosity      1.0175e-13          1.2338        0.015765         0.11484
v  CourantNb                  0.026907          2751.9          44.751          1.3777
v  FourierNb                  0.010887           15204          90.042         0.71368
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14798        0.010818        0.045699


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15279          134.79          2.0914


 TIME FOR THE TIME STEP              818:        0.44794E+02

===============================================================


 INSTANT    0.819000000E+02   TIME STEP NUMBER             819
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.195072829E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31569E+02 0.14313E+02
   Friction velocity        uet   :  0.18837E-03 0.29648E+01
   Friction velocity        uk    :  0.22425E-01 0.31195E+01
   Dimensionless distance   yplus :  0.21088E+00 0.27047E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1715   0.44837E-02   0.39393E+00 
c  VelocityY    0.29408E+04    1715   0.44837E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1715   0.44837E-02   0.00000E+00 
c  Pressure     0.43249E+00    7082   0.36278E-01   0.20452E+00 
c  k            0.22065E+04    1488   0.74027E-04   0.16244E+01 
c  omega        0.33386E+09      66   0.85310E-05   0.47071E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3162e+05                             5
a  Local Time Step      1.1648e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88753          1.5243       0.0037897      3.0393e-06
v  Velocity[Y]                 -23.916          29.728           6.896          20.056
v  Velocity[Z]                 -32.523          29.081         0.17253     -0.00028644
v  ǁVelocityǁ                 0.022109          33.608          10.629          20.218
v  Pressure                    -428.29           350.1         -48.251          32.302
v  k                        3.2741e-08          54.698          3.8163          1.7111
v  omega                         1e-24      1.4556e+08          9242.7          11.968
v  turbulent_viscosity       5.152e-15          1.2294        0.015742          0.1148
v  CourantNb                 0.0094639          2604.9          45.065          1.3778
v  FourierNb                  0.010884           14743          89.541         0.71278
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14748        0.010819        0.045681


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89435           14825          134.61          2.0905


 TIME FOR THE TIME STEP              819:        0.43319E+02

===============================================================


 INSTANT    0.820000000E+02   TIME STEP NUMBER             820
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.343189957E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31759E+02 0.16107E+02
   Friction velocity        uet   :  0.66384E-03 0.28564E+01
   Friction velocity        uk    :  0.26155E-01 0.29407E+01
   Dimensionless distance   yplus :  0.16706E+00 0.27277E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        380
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1705   0.45200E-02   0.35109E+00 
c  VelocityY    0.29407E+04    1705   0.45200E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1705   0.45200E-02   0.00000E+00 
c  Pressure     0.45689E+00    7058   0.33660E-01   0.21683E+00 
c  k            0.22138E+04    1379   0.76971E-04   0.16139E+01 
c  omega        0.85595E+08      97   0.19165E-04   0.17289E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0103e+05                             1
a  Local Time Step      1.1419e-05                         44484


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.81921          1.3779       0.0021371        3.59e-06
v  Velocity[Y]                 -30.614          29.515          6.8241          20.057
v  Velocity[Z]                 -30.052          29.065         0.20955     -0.00088477
v  ǁVelocityǁ                 0.021124          32.841          10.593          20.218
v  Pressure                    -407.03          349.41         -47.369          32.383
v  k                        6.8226e-08           60.86          3.8405          1.7097
v  omega                         1e-24      7.3148e+07          9023.2           11.95
v  turbulent_viscosity      3.9821e-14          1.2387        0.015724         0.11475
v  CourantNb                  0.026306          2056.2          45.072          1.3777
v  FourierNb                  0.010881           14796          88.618         0.71222
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14761         0.01082        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14838          133.69          2.0899


 TIME FOR THE TIME STEP              820:        0.43407E+02

===============================================================


 INSTANT    0.821000000E+02   TIME STEP NUMBER             821
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.333079692E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31822E+02 0.21148E+02
   Friction velocity        uet   :  0.16211E-02 0.27725E+01
   Friction velocity        uk    :  0.26092E-01 0.30503E+01
   Dimensionless distance   yplus :  0.15990E+00 0.28027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        381
   Nb of faces within the viscous sub-layer     :       1054
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1741   0.45540E-02   0.32463E+00 
c  VelocityY    0.29406E+04    1741   0.45540E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1741   0.45540E-02   0.00000E+00 
c  Pressure     0.44571E+00    7071   0.32511E-01   0.21192E+00 
c  k            0.22140E+04    1235   0.92884E-04   0.15048E+01 
c  omega        0.24550E+08     235   0.34938E-04   0.70017E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.441e+05                             2
a  Local Time Step      1.0891e-05                         44420


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.7989          1.1913      0.00079911      5.4169e-06
v  Velocity[Y]                 -23.304          29.492          6.7315          20.057
v  Velocity[Z]                 -28.801          28.638         0.21953      -0.0015883
v  ǁVelocityǁ                 0.018018          32.919          10.597          20.218
v  Pressure                    -391.15          350.07         -47.338          32.392
v  k                        1.0715e-08           88.15          3.9414          1.7082
v  omega                         1e-24      3.7352e+07          8653.9          11.938
v  turbulent_viscosity      9.8643e-15          1.2512        0.015723         0.11469
v  CourantNb                  0.050832          2027.5          45.033          1.3775
v  FourierNb                  0.010878           14901          88.678          0.7121
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14846         0.01082        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14946          133.71          2.0896


 TIME FOR THE TIME STEP              821:        0.43963E+02

===============================================================


 INSTANT    0.822000000E+02   TIME STEP NUMBER             822
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.497406169E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.36171E+02 0.14284E+02
   Friction velocity        uet   :  0.13305E-02 0.26757E+01
   Friction velocity        uk    :  0.23264E-01 0.36742E+01
   Dimensionless distance   yplus :  0.11687E+00 0.28525E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :       1045
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1768   0.46145E-02   0.31469E+00 
c  VelocityY    0.29405E+04    1768   0.46145E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1768   0.46145E-02   0.00000E+00 
c  Pressure     0.44048E+00    7129   0.34743E-01   0.20863E+00 
c  k            0.22082E+04    1206   0.10033E-03   0.13297E+01 
c  omega        0.12166E+08     450   0.37351E-04   0.30016E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1725e+05                             2
a  Local Time Step      1.1002e-05                         44365


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80331          1.1865     -0.00061508      1.8014e-06
v  Velocity[Y]                 -35.821          29.853          6.6874          20.057
v  Velocity[Z]                 -29.192          28.488         0.22142      -0.0025667
v  ǁVelocityǁ                 0.005953          36.519          10.601          20.218
v  Pressure                    -394.21          350.14         -48.108          32.437
v  k                        7.8159e-10          77.288          4.0306          1.7065
v  omega                         1e-24      2.0258e+07          8402.6          11.919
v  turbulent_viscosity      2.5667e-15          1.2667        0.015731         0.11461
v  CourantNb                  0.049264          2011.2          45.025          1.3775
v  FourierNb                  0.010876           14895           89.88         0.71233
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14829         0.01082        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14947          134.91          2.0898


 TIME FOR THE TIME STEP              822:        0.44982E+02

===============================================================


 INSTANT    0.823000000E+02   TIME STEP NUMBER             823
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.125021472E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37107E+02 0.14435E+02
   Friction velocity        uet   :  0.51295E-03 0.33982E+01
   Friction velocity        uk    :  0.18408E-01 0.32795E+01
   Dimensionless distance   yplus :  0.12276E+00 0.31101E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        489
   Nb of faces within the viscous sub-layer     :       1020
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1685   0.45487E-02   0.30824E+00 
c  VelocityY    0.29404E+04    1685   0.45487E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1685   0.45487E-02   0.00000E+00 
c  Pressure     0.41816E+00    6977   0.37278E-01   0.19861E+00 
c  k            0.22003E+04    1355   0.90354E-04   0.12276E+01 
c  omega        0.10598E+08     354   0.58155E-04   0.18273E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4178e+05                             3
a  Local Time Step      1.1498e-05                         44330


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.81521          1.1517      -0.0018551      6.1262e-07
v  Velocity[Y]                 -21.528          30.454          6.6685          20.057
v  Velocity[Z]                 -28.563          28.531         0.21131      -0.0038411
v  ǁVelocityǁ                  0.01113          33.264          10.594          20.219
v  Pressure                    -396.64          349.35         -49.387          32.536
v  k                        7.0791e-09           45.21          4.0856          1.7046
v  omega                         1e-24      1.4532e+07          8336.4          11.906
v  turbulent_viscosity      1.0416e-15           1.278        0.015769         0.11452
v  CourantNb                  0.026765          3140.4          45.266          1.3776
v  FourierNb                  0.010874           14931          90.811          0.7126
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1486        0.010822        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14991          136.08          2.0902


 TIME FOR THE TIME STEP              823:        0.43095E+02

===============================================================


 INSTANT    0.824000000E+02   TIME STEP NUMBER             824
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.755810146E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31178E+02 0.14190E+02
   Friction velocity        uet   :  0.83054E-03 0.27747E+01
   Friction velocity        uk    :  0.21016E-01 0.29458E+01
   Dimensionless distance   yplus :  0.14663E+00 0.27714E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        516
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1574   0.44546E-02   0.31078E+00 
c  VelocityY    0.29404E+04    1574   0.44546E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1574   0.44546E-02   0.00000E+00 
c  Pressure     0.42330E+00    7139   0.36522E-01   0.19978E+00 
c  k            0.21930E+04    1441   0.61935E-04   0.10871E+01 
c  omega        0.10349E+08     292   0.34492E-04   0.10829E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -97365                             1
a  Local Time Step      1.1601e-05                         44320


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95359          1.0804      -0.0024064      1.5506e-06
v  Velocity[Y]                 -17.339          32.575          6.6634          20.057
v  Velocity[Z]                  -28.59          28.602         0.18636      -0.0050162
v  ǁVelocityǁ                0.0061293          33.532          10.577          20.219
v  Pressure                    -397.72          347.58         -50.455          32.492
v  k                        6.6865e-08          47.404          4.1598          1.7027
v  omega                         1e-24      1.1817e+07            8134          11.882
v  turbulent_viscosity      7.8181e-15           1.288        0.015824         0.11442
v  CourantNb                  0.056802          2668.6          44.922          1.3775
v  FourierNb                  0.010872           15017          92.252          0.7129
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010821        0.045719


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15085          137.17          2.0903


 TIME FOR THE TIME STEP              824:        0.42406E+02

===============================================================


 INSTANT    0.825000000E+02   TIME STEP NUMBER             825
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.668505203E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31114E+02 0.14007E+02
   Friction velocity        uet   :  0.88355E-03 0.29502E+01
   Friction velocity        uk    :  0.28529E-01 0.29775E+01
   Dimensionless distance   yplus :  0.90997E-01 0.27414E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        552
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1646   0.46352E-02   0.33112E+00 
c  VelocityY    0.29405E+04    1646   0.46352E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1646   0.46352E-02   0.00000E+00 
c  Pressure     0.43185E+00    7049   0.35440E-01   0.20441E+00 
c  k            0.21871E+04    1481   0.66890E-04   0.11092E+01 
c  omega        0.10148E+08     262   0.39249E-04   0.25763E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.1398e+05                             3
a  Local Time Step      1.1467e-05                         44326


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98685         0.90058      -0.0020128      2.2116e-06
v  Velocity[Y]                 -16.692          33.413          6.6697          20.056
v  Velocity[Z]                 -28.723           28.71         0.15328      -0.0059269
v  ǁVelocityǁ                0.0084739          33.516          10.571          20.218
v  Pressure                    -396.15          345.32         -51.106          32.244
v  k                        1.3016e-07          51.593           4.208          1.7006
v  omega                         1e-24      1.1676e+07          8199.2           11.91
v  turbulent_viscosity      3.6222e-14          1.2954        0.015899         0.11431
v  CourantNb                   0.05987          2031.4          44.322          1.3773
v  FourierNb                  0.010871           15050          93.861         0.71295
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14884        0.010819        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15123          138.18          2.0903


 TIME FOR THE TIME STEP              825:        0.43002E+02

===============================================================


 INSTANT    0.826000000E+02   TIME STEP NUMBER             826
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.112676425E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32119E+02 0.16621E+02
   Friction velocity        uet   :  0.13159E-02 0.28999E+01
   Friction velocity        uk    :  0.29492E-01 0.32269E+01
   Dimensionless distance   yplus :  0.12977E+00 0.29310E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        504
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1787   0.45246E-02   0.36825E+00 
c  VelocityY    0.29404E+04    1787   0.45246E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1787   0.45246E-02   0.00000E+00 
c  Pressure     0.44044E+00    6986   0.33135E-01   0.20798E+00 
c  k            0.21817E+04    1495   0.68575E-04   0.11823E+01 
c  omega        0.10373E+08     376   0.60427E-04   0.54683E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3548e+05                             1
a  Local Time Step      1.1248e-05                         44339


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1737         0.91974     -0.00095451      3.8183e-06
v  Velocity[Y]                 -17.958          32.845          6.6722          20.056
v  Velocity[Z]                 -28.802          29.015         0.11059      -0.0066949
v  ǁVelocityǁ                 0.016161          33.471          10.566          20.218
v  Pressure                     -384.6          342.17         -52.216          31.812
v  k                        6.9363e-07          44.537           4.187          1.6986
v  omega                         1e-24      1.5675e+07          8431.4          11.957
v  turbulent_viscosity      2.8809e-14          1.3027        0.015954         0.11418
v  CourantNb                  0.056692          2024.7          43.857          1.3773
v  FourierNb                  0.010869           15011          95.926         0.71304
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14843        0.010818        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15090          139.78          2.0903


 TIME FOR THE TIME STEP              826:        0.44438E+02

===============================================================


 INSTANT    0.827000000E+02   TIME STEP NUMBER             827
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.288950533E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30092E+02 0.20760E+02
   Friction velocity        uet   :  0.28259E-02 0.27491E+01
   Friction velocity        uk    :  0.18312E-01 0.32251E+01
   Dimensionless distance   yplus :  0.14572E+00 0.37893E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        502
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1934   0.46848E-02   0.40109E+00 
c  VelocityY    0.29404E+04    1934   0.46848E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1934   0.46848E-02   0.00000E+00 
c  Pressure     0.42948E+00    6975   0.31152E-01   0.20284E+00 
c  k            0.21765E+04    1443   0.68885E-04   0.11435E+01 
c  omega        0.16452E+08     322   0.27175E-04   0.42124E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3411e+05                             1
a  Local Time Step      1.1677e-05                         44359


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4034         0.99271      0.00013645      3.4446e-06
v  Velocity[Y]                 -23.192          32.191          6.6406          20.056
v  Velocity[Z]                 -29.058           28.96        0.070946      -0.0078728
v  ǁVelocityǁ                 0.011531          33.012          10.554          20.219
v  Pressure                    -368.39          343.09         -52.726          31.365
v  k                        3.7661e-07          43.052          4.1449          1.6966
v  omega                         1e-24      1.2058e+07          8282.1          11.936
v  turbulent_viscosity      1.7463e-13          1.3093        0.015966         0.11405
v  CourantNb                  0.027984          2011.9          43.774          1.3776
v  FourierNb                  0.010869           15195          96.928         0.71233
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14828        0.010817        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15237           140.7          2.0899


 TIME FOR THE TIME STEP              827:        0.45490E+02

===============================================================


 INSTANT    0.828000000E+02   TIME STEP NUMBER             828
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.242378610E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30752E+02 0.20138E+02
   Friction velocity        uet   :  0.37477E-02 0.26473E+01
   Friction velocity        uk    :  0.10263E-01 0.30396E+01
   Dimensionless distance   yplus :  0.11757E+00 0.29891E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :       1027
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2023   0.46828E-02   0.43088E+00 
c  VelocityY    0.29403E+04    2023   0.46828E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2023   0.46828E-02   0.00000E+00 
c  Pressure     0.41877E+00    6973   0.30066E-01   0.19718E+00 
c  k            0.21725E+04    1434   0.68204E-04   0.11906E+01 
c  omega        0.12407E+08     230   0.29514E-04   0.21687E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -14737                             1
a  Local Time Step      1.1426e-05                         44386


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6457          1.0425       0.0021295      2.9904e-06
v  Velocity[Y]                 -22.399          30.481          6.6244          20.056
v  Velocity[Z]                 -30.343          29.353        0.039791       -0.008455
v  ǁVelocityǁ                 0.020599          35.017          10.535          20.219
v  Pressure                    -353.91           344.4          -52.66          31.117
v  k                        1.4009e-07          42.382          4.0922          1.6949
v  omega                         1e-24      1.1794e+07            8094          11.909
v  turbulent_viscosity      1.2915e-13           1.313        0.015949         0.11391
v  CourantNb                  0.015598          2024.6           43.84          1.3779
v  FourierNb                  0.010868           15469          95.917         0.71054
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14774        0.010817        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85303           15521          139.76          2.0884


 TIME FOR THE TIME STEP              828:        0.46171E+02

===============================================================


 INSTANT    0.829000000E+02   TIME STEP NUMBER             829
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.689277983E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31022E+02 0.19831E+02
   Friction velocity        uet   :  0.12232E-02 0.28389E+01
   Friction velocity        uk    :  0.18051E-01 0.31201E+01
   Dimensionless distance   yplus :  0.15223E+00 0.28739E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1932   0.46667E-02   0.46340E+00 
c  VelocityY    0.29401E+04    1932   0.46667E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1932   0.46667E-02   0.00000E+00 
c  Pressure     0.42705E+00    7090   0.30076E-01   0.20181E+00 
c  k            0.21710E+04    1448   0.69828E-04   0.13112E+01 
c  omega        0.10354E+08     260   0.97829E-04   0.76204E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2966e+05                             1
a  Local Time Step      1.0923e-05                         44427


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9229          1.0754       0.0043454      3.3741e-06
v  Velocity[Y]                 -16.896           31.27          6.6446          20.057
v  Velocity[Z]                 -30.732          28.973       0.0020762      -0.0092678
v  ǁVelocityǁ                 0.020903           36.55          10.518          20.219
v  Pressure                    -350.87          346.77          -50.99          31.399
v  k                        5.3597e-09          53.004          4.0546          1.6933
v  omega                         1e-24      5.4738e+07          8056.3          11.877
v  turbulent_viscosity      2.0865e-13          1.3152        0.015933         0.11375
v  CourantNb                  0.046343          2028.9          44.102           1.378
v  FourierNb                  0.010868           15744          94.727         0.70884
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14784        0.010817        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15807          138.83          2.0868


 TIME FOR THE TIME STEP              829:        0.45807E+02

===============================================================


 INSTANT    0.830000000E+02   TIME STEP NUMBER             830
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.113138307E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31767E+02 0.19294E+02
   Friction velocity        uet   :  0.73311E-03 0.30620E+01
   Friction velocity        uk    :  0.31363E-01 0.30961E+01
   Dimensionless distance   yplus :  0.16714E+00 0.28105E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1920   0.44374E-02   0.47881E+00 
c  VelocityY    0.29400E+04    1920   0.44374E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1920   0.44374E-02   0.00000E+00 
c  Pressure     0.42770E+00    7115   0.34547E-01   0.20284E+00 
c  k            0.21737E+04    1498   0.75431E-04   0.14423E+01 
c  omega        0.20905E+28       2   0.13149E-15   0.26102E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -92312                             2
a  Local Time Step      1.1874e-05                         44450


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1133          1.1986       0.0060437      1.5003e-06
v  Velocity[Y]                 -14.535          33.007          6.6959          20.057
v  Velocity[Z]                 -33.419          29.054       -0.031688      -0.0097025
v  ǁVelocityǁ                 0.024728          36.111          10.524          20.219
v  Pressure                    -410.34          347.68         -49.622          31.582
v  k                        1.1559e-09           63.05          4.0228          1.6919
v  omega                         1e-24      2.7543e+07          7807.6          11.849
v  turbulent_viscosity      2.4004e-15          1.3193        0.015936         0.11359
v  CourantNb                  0.039541            2174          44.135          1.3778
v  FourierNb                  0.010869           15922          93.379         0.70713
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14699        0.010815        0.045711


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15996          137.51           2.085


 TIME FOR THE TIME STEP              830:        0.45694E+02

===============================================================


 INSTANT    0.831000000E+02   TIME STEP NUMBER             831
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.147828425E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31079E+02 0.16300E+02
   Friction velocity        uet   :  0.11990E-02 0.31840E+01
   Friction velocity        uk    :  0.26552E-01 0.30200E+01
   Dimensionless distance   yplus :  0.11940E+00 0.27449E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1927   0.43618E-02   0.49718E+00 
c  VelocityY    0.29400E+04    1927   0.43618E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1927   0.43618E-02   0.00000E+00 
c  Pressure     0.43902E+00    7126   0.38670E-01   0.20878E+00 
c  k            0.21821E+04    1588   0.77153E-04   0.15756E+01 
c  omega        0.10863E+08     304   0.17309E-03   0.13217E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9315e+05                             3
a  Local Time Step      1.1695e-05                         44452


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.1673          1.3732       0.0068233      1.7694e-06
v  Velocity[Y]                 -16.304          31.596          6.7542          20.056
v  Velocity[Z]                 -33.024          28.942        -0.02608         -0.0102
v  ǁVelocityǁ                0.0056906          35.041          10.541          20.219
v  Pressure                    -438.77           347.2         -48.547          31.781
v  k                        1.3935e-08          64.874          4.0014          1.6906
v  omega                         1e-24      6.6414e+07          8223.2          11.894
v  turbulent_viscosity      1.0279e-15          1.3224        0.015944          0.1134
v  CourantNb                  0.026514          2676.2          44.019          1.3775
v  FourierNb                  0.010871           15951          92.312         0.70518
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14671        0.010815        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15995          136.33          2.0826


 TIME FOR THE TIME STEP              831:        0.46161E+02

===============================================================


 INSTANT    0.832000000E+02   TIME STEP NUMBER             832
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.780847249E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30317E+02 0.13875E+02
   Friction velocity        uet   :  0.63147E-03 0.30946E+01
   Friction velocity        uk    :  0.29911E-01 0.30056E+01
   Dimensionless distance   yplus :  0.11983E+00 0.28115E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :        985
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1950   0.45317E-02   0.50036E+00 
c  VelocityY    0.29399E+04    1950   0.45317E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1950   0.45317E-02   0.00000E+00 
c  Pressure     0.42894E+00    6868   0.37689E-01   0.20275E+00 
c  k            0.21956E+04    1465   0.75587E-04   0.15386E+01 
c  omega        0.22425E+08     154   0.14533E-03   0.34525E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -97925                             1
a  Local Time Step      1.1397e-05                         44466


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2116          1.4506        0.006313      1.3335e-06
v  Velocity[Y]                 -23.652          29.894          6.7799          20.056
v  Velocity[Z]                 -32.726          28.909       0.0050618       -0.010268
v  ǁVelocityǁ                 0.011454          34.406          10.533          20.218
v  Pressure                    -443.81          346.11         -48.067          31.829
v  k                        3.8719e-07          58.758          3.9758          1.6894
v  omega                         1e-24      6.2345e+07            9179           11.95
v  turbulent_viscosity       2.411e-14          1.3208        0.015955         0.11322
v  CourantNb                 0.0051617          2741.5          44.045          1.3771
v  FourierNb                  0.010872           16031          91.738         0.70379
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14844        0.010815        0.045714


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16074          135.78          2.0809


 TIME FOR THE TIME STEP              832:        0.44990E+02

===============================================================


 INSTANT    0.833000000E+02   TIME STEP NUMBER             833
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.382189339E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31293E+02 0.13500E+02
   Friction velocity        uet   :  0.29745E-02 0.29232E+01
   Friction velocity        uk    :  0.24225E-01 0.30131E+01
   Dimensionless distance   yplus :  0.16945E+00 0.28639E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1981   0.43804E-02   0.48115E+00 
c  VelocityY    0.29400E+04    1981   0.43804E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1981   0.43804E-02   0.00000E+00 
c  Pressure     0.44278E+00    7093   0.33409E-01   0.20918E+00 
c  k            0.22055E+04    1349   0.75823E-04   0.15373E+01 
c  omega        0.35346E+08     133   0.42834E-04   0.12291E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4288e+05                             2
a  Local Time Step      1.0894e-05                         44482


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0353          1.3483       0.0041778      1.6908e-06
v  Velocity[Y]                 -27.626          29.773          6.7392          20.056
v  Velocity[Z]                 -32.377          28.559        0.023983       -0.010134
v  ǁVelocityǁ                 0.018865          32.819          10.521          20.218
v  Pressure                    -430.53          347.47         -47.818          31.747
v  k                        1.4276e-08          44.762          3.9873          1.6881
v  omega                         1e-24      3.2126e+07          8577.9          11.938
v  turbulent_viscosity      5.4982e-14          1.3183        0.015953         0.11305
v  CourantNb                  0.031039          2283.5          44.174          1.3768
v  FourierNb                  0.010874           16025          91.755          0.7027
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010816        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16072          135.93          2.0795


 TIME FOR THE TIME STEP              833:        0.46106E+02

===============================================================


 INSTANT    0.834000000E+02   TIME STEP NUMBER             834
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.247151608E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30584E+02 0.18791E+02
   Friction velocity        uet   :  0.20677E-02 0.27959E+01
   Friction velocity        uk    :  0.18797E-01 0.31742E+01
   Dimensionless distance   yplus :  0.46689E-01 0.28822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :        975
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1977   0.46243E-02   0.46563E+00 
c  VelocityY    0.29400E+04    1977   0.46243E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1977   0.46243E-02   0.00000E+00 
c  Pressure     0.40933E+00    7012   0.31101E-01   0.19335E+00 
c  k            0.22088E+04    1350   0.86300E-04   0.14743E+01 
c  omega        0.14112E+08     256   0.70811E-04   0.11204E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -55062                             2
a  Local Time Step      1.1339e-05                         44496


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7302          1.1361       0.0014643      1.7098e-06
v  Velocity[Y]                 -33.174           29.72          6.6476          20.055
v  Velocity[Z]                 -30.402          28.596        0.019217      -0.0097394
v  ǁVelocityǁ                0.0085523          33.454          10.544          20.218
v  Pressure                    -406.28          347.72         -48.464          31.572
v  k                        1.6454e-08          84.801            4.07          1.6869
v  omega                         1e-24       3.634e+07          8352.8          11.922
v  turbulent_viscosity      1.5887e-15          1.3149        0.015953         0.11287
v  CourantNb                  0.035185          2058.2          44.248          1.3766
v  FourierNb                  0.010876           15942          92.372         0.70195
v  total_pressure           1.0092e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010816        0.045701


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15997          136.62          2.0785


 TIME FOR THE TIME STEP              834:        0.46804E+02

===============================================================


 INSTANT    0.835000000E+02   TIME STEP NUMBER             835
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.928811993E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30365E+02 0.22406E+02
   Friction velocity        uet   :  0.28515E-02 0.27852E+01
   Friction velocity        uk    :  0.22423E-01 0.30506E+01
   Dimensionless distance   yplus :  0.18710E+00 0.33081E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        474
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    2012   0.46852E-02   0.46541E+00 
c  VelocityY    0.29400E+04    2012   0.46852E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    2012   0.46852E-02   0.00000E+00 
c  Pressure     0.44265E+00    7107   0.34870E-01   0.20934E+00 
c  k            0.22043E+04    1441   0.12998E-03   0.13364E+01 
c  omega        0.18979E+08     405   0.59832E-04   0.85647E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2637e+05                             1
a  Local Time Step      1.1327e-05                         44496


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5565         0.99509     -0.00068141      1.2316e-06
v  Velocity[Y]                 -38.266          30.217          6.6033          20.056
v  Velocity[Z]                 -28.872          28.466        0.018087      -0.0095022
v  ǁVelocityǁ                0.0096725           38.64          10.577          20.218
v  Pressure                    -409.99          346.68         -50.471          31.686
v  k                        8.9534e-08           113.7          4.1859          1.6857
v  omega                         1e-24      4.3514e+07          8322.6          11.908
v  turbulent_viscosity      1.4055e-15          1.3116        0.015962         0.11269
v  CourantNb                  0.021849          2068.8          44.248          1.3764
v  FourierNb                  0.010879           15878          93.011         0.70177
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010816        0.045695


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15941          137.26          2.0782


 TIME FOR THE TIME STEP              835:        0.46658E+02

===============================================================


 INSTANT    0.836000000E+02   TIME STEP NUMBER             836
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.558362332E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49525E+02 0.14566E+02
   Friction velocity        uet   :  0.23856E-03 0.34543E+01
   Friction velocity        uk    :  0.19626E-01 0.48283E+01
   Dimensionless distance   yplus :  0.15382E+00 0.41755E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    2017   0.44371E-02   0.46910E+00 
c  VelocityY    0.29401E+04    2017   0.44371E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    2017   0.44371E-02   0.00000E+00 
c  Pressure     0.43193E+00    7120   0.39170E-01   0.20527E+00 
c  k            0.21961E+04    1485   0.14214E-03   0.11856E+01 
c  omega        0.15237E+08     447   0.12495E-03   0.18685E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2839e+05                             3
a  Local Time Step      1.1417e-05                         44515


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5593          1.0605      -0.0014565     -1.3718e-06
v  Velocity[Y]                  -26.77          30.604          6.6186          20.056
v  Velocity[Z]                 -28.822          28.577        0.018578      -0.0086224
v  ǁVelocityǁ                0.0081683          33.599          10.599          20.219
v  Pressure                    -412.26          344.69         -53.443          31.679
v  k                        4.9019e-08          53.838           4.227          1.6847
v  omega                         1e-24      5.5617e+07          8990.1          11.942
v  turbulent_viscosity      4.2781e-14          1.3074        0.015982         0.11252
v  CourantNb                  0.016233          2544.7          44.255          1.3764
v  FourierNb                  0.010881           15932           93.88         0.70169
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010815        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16004          138.14          2.0781


 TIME FOR THE TIME STEP              836:        0.46781E+02

===============================================================


 INSTANT    0.837000000E+02   TIME STEP NUMBER             837
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.262633153E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31381E+02 0.14896E+02
   Friction velocity        uet   :  0.16075E-02 0.27866E+01
   Friction velocity        uk    :  0.20266E-01 0.30440E+01
   Dimensionless distance   yplus :  0.17484E+00 0.27308E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    2043   0.44311E-02   0.47272E+00 
c  VelocityY    0.29400E+04    2043   0.44311E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    2043   0.44311E-02   0.00000E+00 
c  Pressure     0.42392E+00    6973   0.37824E-01   0.20139E+00 
c  k            0.21883E+04    1488   0.75607E-04   0.10320E+01 
c  omega        0.21922E+08     252   0.11692E-03   0.17768E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9336e+05                             1
a  Local Time Step      1.1502e-05                         44523


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.449          1.0825      -0.0016784      -2.826e-06
v  Velocity[Y]                 -17.851          30.865          6.6568          20.056
v  Velocity[Z]                 -28.895          28.746        0.019446      -0.0076242
v  ǁVelocityǁ                 0.008637          33.591          10.603          20.218
v  Pressure                    -414.28          342.87         -55.997           31.62
v  k                        8.9444e-08          53.447          4.2711          1.6836
v  omega                         1e-24      6.5162e+07          9020.1          11.933
v  turbulent_viscosity      2.0425e-14          1.3033        0.016017         0.11236
v  CourantNb                  0.011338          2790.1          44.206          1.3764
v  FourierNb                  0.010884           15948          95.685         0.70164
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14754        0.010814        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16024          139.89          2.0781


 TIME FOR THE TIME STEP              837:        0.46446E+02

===============================================================


 INSTANT    0.838000000E+02   TIME STEP NUMBER             838
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.378099096E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31997E+02 0.13756E+02
   Friction velocity        uet   :  0.12923E-02 0.27986E+01
   Friction velocity        uk    :  0.22967E-01 0.30717E+01
   Dimensionless distance   yplus :  0.12119E+00 0.27816E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    2064   0.44229E-02   0.47794E+00 
c  VelocityY    0.29401E+04    2064   0.44229E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    2064   0.44229E-02   0.00000E+00 
c  Pressure     0.42160E+00    7067   0.32664E-01   0.19908E+00 
c  k            0.21817E+04    1443   0.81972E-04   0.10135E+01 
c  omega        0.23453E+08     373   0.45298E-04   0.50275E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6686e+05                             2
a  Local Time Step      1.0995e-05                         44507


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4266          1.0004      -0.0022683     -1.1112e-06
v  Velocity[Y]                 -16.798           32.55          6.6945          20.056
v  Velocity[Z]                 -28.739          29.709        0.020002      -0.0067923
v  ǁVelocityǁ                 0.017421          33.539          10.578          20.218
v  Pressure                    -414.19          342.67         -57.447          31.439
v  k                        1.0049e-08          49.926          4.2923          1.6826
v  omega                         1e-24      3.3511e+07          8404.2          11.877
v  turbulent_viscosity      2.3463e-14          1.2978         0.01605          0.1122
v  CourantNb                  0.039191          2044.5          44.029          1.3766
v  FourierNb                  0.010888           15786          98.333         0.70196
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14845        0.010813        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15865          142.36          2.0786


 TIME FOR THE TIME STEP              838:        0.47061E+02

===============================================================


 INSTANT    0.839000000E+02   TIME STEP NUMBER             839
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.206980574E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31030E+02 0.14845E+02
   Friction velocity        uet   :  0.48082E-03 0.28697E+01
   Friction velocity        uk    :  0.27594E-01 0.32021E+01
   Dimensionless distance   yplus :  0.14888E+00 0.30803E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2155   0.43319E-02   0.48060E+00 
c  VelocityY    0.29402E+04    2155   0.43319E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2155   0.43319E-02   0.00000E+00 
c  Pressure     0.42687E+00    7019   0.30032E-01   0.20102E+00 
c  k            0.21741E+04    1241   0.72491E-04   0.10634E+01 
c  omega        0.11688E+08     429   0.83753E-04   0.32222E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.373e+05                             2
a  Local Time Step      1.2004e-05                         44475


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3043          1.0175      -0.0031344     -1.7155e-06
v  Velocity[Y]                 -15.256          32.862          6.7034          20.056
v  Velocity[Z]                  -29.14          29.108        0.021464      -0.0055185
v  ǁVelocityǁ                0.0065701          33.665          10.546          20.218
v  Pressure                    -405.37          344.53         -58.285          31.139
v  k                          2.16e-09          49.139          4.2481          1.6817
v  omega                         1e-24      2.4462e+07          8309.6          11.866
v  turbulent_viscosity      1.1201e-15          1.2911        0.016053         0.11205
v  CourantNb                  0.027023            2022          43.854          1.3768
v  FourierNb                  0.010891           15680          99.533         0.70211
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14727        0.010812        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15721          143.39          2.0789


 TIME FOR THE TIME STEP              839:        0.47446E+02

===============================================================


 INSTANT    0.840000000E+02   TIME STEP NUMBER             840
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.198970289E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30512E+02 0.13605E+02
   Friction velocity        uet   :  0.26344E-03 0.27706E+01
   Friction velocity        uk    :  0.21807E-01 0.28445E+01
   Dimensionless distance   yplus :  0.15387E+00 0.34662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        485
   Nb of faces within the viscous sub-layer     :        904
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2234   0.44198E-02   0.47640E+00 
c  VelocityY    0.29403E+04    2234   0.44198E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2234   0.44198E-02   0.00000E+00 
c  Pressure     0.39614E+00    7042   0.30679E-01   0.18689E+00 
c  k            0.21665E+04    1110   0.66893E-04   0.97278E+00 
c  omega        0.21081E+08     236   0.24047E-04   0.14944E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0115e+05                             1
a  Local Time Step      1.2092e-05                         44456


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2323         0.95102      -0.0045738     -2.1201e-06
v  Velocity[Y]                 -15.297          33.789          6.6804          20.056
v  Velocity[Z]                 -29.269           29.16        0.013639      -0.0036903
v  ǁVelocityǁ                  0.01255          34.034          10.533          20.217
v  Pressure                    -388.43          345.64         -59.257          30.558
v  k                        6.8293e-08          40.326          4.1806          1.6809
v  omega                         1e-24      1.2631e+07          8139.9          11.849
v  turbulent_viscosity      8.0153e-15          1.2861        0.016014         0.11192
v  CourantNb                  0.030614          2030.8           43.66           1.377
v  FourierNb                  0.010894           15835           99.47         0.70125
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14756        0.010811        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15884          143.13          2.0782


 TIME FOR THE TIME STEP              840:        0.48299E+02

===============================================================


 INSTANT    0.841000000E+02   TIME STEP NUMBER             841
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.578477512E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31266E+02 0.20990E+02
   Friction velocity        uet   :  0.18646E-02 0.26722E+01
   Friction velocity        uk    :  0.18303E-01 0.33927E+01
   Dimensionless distance   yplus :  0.97227E-01 0.31313E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :        892
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2147   0.43206E-02   0.47346E+00 
c  VelocityY    0.29402E+04    2147   0.43206E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2147   0.43206E-02   0.00000E+00 
c  Pressure     0.40418E+00    7025   0.28989E-01   0.19004E+00 
c  k            0.21609E+04    1452   0.65920E-04   0.97163E+00 
c  omega        0.14758E+08     249   0.22355E-04   0.10618E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -56455                             1
a  Local Time Step      1.2395e-05                         44435


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1365         0.80036      -0.0057402      -1.614e-06
v  Velocity[Y]                 -17.022          30.677          6.6792          20.055
v  Velocity[Z]                  -29.01          29.097        0.012025      -0.0023232
v  ǁVelocityǁ                 0.021255          33.895           10.53          20.216
v  Pressure                    -373.25          347.53         -58.933          30.496
v  k                        4.4542e-08          37.412          4.0822          1.6803
v  omega                         1e-24      1.1801e+07          7993.8          11.822
v  turbulent_viscosity      1.2224e-13           1.279        0.015953          0.1118
v  CourantNb                  0.038434          2049.8          43.714          1.3774
v  FourierNb                  0.010892           15927          98.711         0.70006
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14921        0.010811         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15988          142.42          2.0774


 TIME FOR THE TIME STEP              841:        0.47818E+02

===============================================================


 INSTANT    0.842000000E+02   TIME STEP NUMBER             842
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.755384882E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31725E+02 0.20016E+02
   Friction velocity        uet   :  0.15578E-02 0.27469E+01
   Friction velocity        uk    :  0.25298E-01 0.31224E+01
   Dimensionless distance   yplus :  0.10288E+00 0.28198E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :        910
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2106   0.43651E-02   0.47207E+00 
c  VelocityY    0.29402E+04    2106   0.43651E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2106   0.43651E-02   0.00000E+00 
c  Pressure     0.40212E+00    7029   0.28202E-01   0.18813E+00 
c  k            0.21574E+04    1551   0.63162E-04   0.10543E+01 
c  omega        0.12154E+08     279   0.26615E-04   0.57080E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.006e+05                             1
a  Local Time Step      1.2053e-05                         44473


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1461          0.6376       -0.006104     -3.4107e-06
v  Velocity[Y]                 -15.579           30.48          6.7163          20.055
v  Velocity[Z]                 -32.048          29.293      0.00035122       -0.001021
v  ǁVelocityǁ                0.0052438          36.475          10.544          20.215
v  Pressure                    -345.63          349.81         -57.026          30.725
v  k                        1.0506e-07          47.801          3.9971          1.6798
v  omega                         1e-24      1.1792e+07          7859.5          11.795
v  turbulent_viscosity      6.0218e-14          1.2736        0.015882         0.11169
v  CourantNb                  0.039679          2058.5          44.173          1.3776
v  FourierNb                  0.010892           15917          97.085         0.69875
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14911        0.010811        0.045663


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15990          141.26          2.0764


 TIME FOR THE TIME STEP              842:        0.47851E+02

===============================================================


 INSTANT    0.843000000E+02   TIME STEP NUMBER             843
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.489412196E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31338E+02 0.17169E+02
   Friction velocity        uet   :  0.30225E-02 0.30748E+01
   Friction velocity        uk    :  0.29004E-01 0.32692E+01
   Dimensionless distance   yplus :  0.10108E+00 0.27628E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        348
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2099   0.44041E-02   0.45633E+00 
c  VelocityY    0.29403E+04    2099   0.44041E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2099   0.44041E-02   0.00000E+00 
c  Pressure     0.44282E+00    7069   0.31552E-01   0.20695E+00 
c  k            0.21581E+04    1565   0.64997E-04   0.11839E+01 
c  omega        0.11038E+08     239   0.11364E-03   0.92250E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4436e+05                             1
a  Local Time Step      1.1841e-05                         44500


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.382          0.7975      -0.0060361     -5.0712e-06
v  Velocity[Y]                 -15.237           30.45          6.7892          20.055
v  Velocity[Z]                 -32.603          29.154       -0.001357      0.00022148
v  ǁVelocityǁ                0.0099895          36.392          10.588          20.215
v  Pressure                    -402.64          351.08         -54.522          31.246
v  k                        6.2403e-09          60.704          3.9381          1.6796
v  omega                         1e-24      6.1986e+07          8179.8           11.82
v  turbulent_viscosity      3.3874e-13          1.2686        0.015819          0.1116
v  CourantNb                  0.011047          2054.9          44.498          1.3776
v  FourierNb                  0.010892           15814          94.539         0.69726
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1494        0.010811        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15896          139.04          2.0749


 TIME FOR THE TIME STEP              843:        0.47642E+02

===============================================================


 INSTANT    0.844000000E+02   TIME STEP NUMBER             844
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.109315897E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31991E+02 0.14273E+02
   Friction velocity        uet   :  0.20911E-02 0.30524E+01
   Friction velocity        uk    :  0.32071E-01 0.34167E+01
   Dimensionless distance   yplus :  0.13707E+00 0.28016E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        359
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2076   0.44284E-02   0.44468E+00 
c  VelocityY    0.29403E+04    2076   0.44284E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2076   0.44284E-02   0.00000E+00 
c  Pressure     0.42116E+00    7118   0.35321E-01   0.19666E+00 
c  k            0.21654E+04    1555   0.66313E-04   0.12546E+01 
c  omega        0.27937E+08     174   0.87651E-04   0.20235E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -24189                             1
a  Local Time Step      1.0929e-05                         44516


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6587         0.93705      -0.0057629     -3.3766e-06
v  Velocity[Y]                  -15.26          30.662          6.8696          20.056
v  Velocity[Z]                 -32.959          28.922         0.01955       0.0013284
v  ǁVelocityǁ                  0.01074          34.902           10.64          20.215
v  Pressure                    -431.18          351.59         -52.193          31.752
v  k                        5.4814e-08          67.593          3.9092          1.6794
v  omega                         1e-24      7.6826e+07          8712.8          11.866
v  turbulent_viscosity      2.0969e-14          1.2617         0.01577         0.11152
v  CourantNb                  0.023775          2554.2          44.841          1.3775
v  FourierNb                  0.010892           15881          92.818         0.69569
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14866         0.01081         0.04566


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15927          137.66          2.0732


 TIME FOR THE TIME STEP              844:        0.49334E+02

===============================================================


 INSTANT    0.845000000E+02   TIME STEP NUMBER             845
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.953757113E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30298E+02 0.14041E+02
   Friction velocity        uet   :  0.22241E-02 0.30881E+01
   Friction velocity        uk    :  0.22367E-01 0.31269E+01
   Dimensionless distance   yplus :  0.10096E+00 0.28147E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        362
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2053   0.43277E-02   0.42855E+00 
c  VelocityY    0.29403E+04    2053   0.43277E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2053   0.43277E-02   0.00000E+00 
c  Pressure     0.40638E+00    7109   0.37462E-01   0.19005E+00 
c  k            0.21776E+04    1553   0.66150E-04   0.12867E+01 
c  omega        0.33305E+08     127   0.36206E-04   0.79709E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2861e+05                             1
a  Local Time Step      1.1652e-05                         44515


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7689          1.0515      -0.0050629      -2.401e-06
v  Velocity[Y]                 -21.053          30.103          6.9147          20.057
v  Velocity[Z]                 -32.714          28.805        0.065264       0.0026226
v  ǁVelocityǁ                 0.010075          34.235          10.656          20.216
v  Pressure                    -436.41          353.11         -50.604           32.06
v  k                        4.8297e-10          63.328          3.8956          1.6792
v  omega                         1e-24      3.9069e+07          8535.9          11.887
v  turbulent_viscosity      1.4875e-13           1.259        0.015738         0.11146
v  CourantNb                  0.033267          2725.1          45.138          1.3773
v  FourierNb                  0.010892           15782          91.621         0.69438
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14906        0.010811        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15831          136.76          2.0717


 TIME FOR THE TIME STEP              845:        0.47240E+02

===============================================================


 INSTANT    0.846000000E+02   TIME STEP NUMBER             846
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.225362434E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30360E+02 0.13747E+02
   Friction velocity        uet   :  0.25989E-02 0.29142E+01
   Friction velocity        uk    :  0.12079E-01 0.27888E+01
   Dimensionless distance   yplus :  0.66124E-01 0.28300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        380
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    2071   0.43779E-02   0.38338E+00 
c  VelocityY    0.29403E+04    2071   0.43779E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    2071   0.43779E-02   0.00000E+00 
c  Pressure     0.42886E+00    6973   0.35984E-01   0.20223E+00 
c  k            0.21899E+04    1571   0.67481E-04   0.13271E+01 
c  omega        0.13721E+08     203   0.58393E-04   0.54497E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -7862.3                             1
a  Local Time Step      1.1634e-05                         44488


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8014           1.138      -0.0041436     -9.9094e-07
v  Velocity[Y]                 -24.137          29.902          6.8698          20.057
v  Velocity[Z]                 -32.146          28.654         0.11696       0.0036146
v  ǁVelocityǁ                 0.017091          32.668           10.62          20.215
v  Pressure                    -423.93          353.69           -49.5          32.015
v  k                         3.601e-08          50.036          3.9052          1.6788
v  omega                         1e-24      2.0869e+07          8519.8          11.888
v  turbulent_viscosity       1.203e-16           1.257        0.015703          0.1114
v  CourantNb                  0.039876            2280          45.313          1.3772
v  FourierNb                  0.010894           15472          90.926         0.69324
v  total_pressure            1.009e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14908        0.010813        0.045707


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15530          136.24          2.0704


 TIME FOR THE TIME STEP              846:        0.46785E+02

===============================================================


 INSTANT    0.847000000E+02   TIME STEP NUMBER             847
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.341499200E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31161E+02 0.16497E+02
   Friction velocity        uet   :  0.10942E-02 0.27710E+01
   Friction velocity        uk    :  0.15367E-01 0.28289E+01
   Dimensionless distance   yplus :  0.38171E-01 0.28151E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :       1001
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1988   0.43163E-02   0.34162E+00 
c  VelocityY    0.29404E+04    1988   0.43163E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1988   0.43163E-02   0.00000E+00 
c  Pressure     0.40780E+00    6979   0.31099E-01   0.19201E+00 
c  k            0.21971E+04    1567   0.80168E-04   0.12775E+01 
c  omega        0.11344E+08     227   0.41687E-04   0.32276E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1281e+05                             1
a  Local Time Step      1.1416e-05                         44461


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6961          1.1845       -0.003739      8.0974e-07
v  Velocity[Y]                 -30.671           29.76          6.7562          20.056
v  Velocity[Z]                 -29.859          28.619         0.13648       0.0046567
v  ǁVelocityǁ                 0.016055          33.009          10.614          20.215
v  Pressure                    -398.18          352.86         -48.997          32.126
v  k                        1.1899e-07          71.076          3.9772          1.6784
v  omega                         1e-24      1.2914e+07          8334.4          11.869
v  turbulent_viscosity       3.628e-15          1.2558        0.015681         0.11136
v  CourantNb                  0.045174          2011.6          45.057          1.3769
v  FourierNb                  0.010896           15115          90.743         0.69257
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14823        0.010813        0.045692


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15181           135.8          2.0695


 TIME FOR THE TIME STEP              847:        0.46086E+02

===============================================================


 INSTANT    0.848000000E+02   TIME STEP NUMBER             848
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.234831179E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31703E+02 0.20493E+02
   Friction velocity        uet   :  0.22854E-02 0.26089E+01
   Friction velocity        uk    :  0.25958E-01 0.29250E+01
   Dimensionless distance   yplus :  0.11204E+00 0.27400E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1901   0.46057E-02   0.32066E+00 
c  VelocityY    0.29404E+04    1901   0.46057E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1901   0.46057E-02   0.00000E+00 
c  Pressure     0.40897E+00    7040   0.31127E-01   0.19343E+00 
c  k            0.21949E+04    1491   0.91490E-04   0.11316E+01 
c  omega        0.10438E+08     399   0.44006E-04   0.22946E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5458e+05                             1
a  Local Time Step      1.1288e-05                         44451


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7517          1.1816      -0.0035705      1.0815e-06
v  Velocity[Y]                 -40.251          29.797          6.6721          20.056
v  Velocity[Z]                 -28.587          28.494         0.15721       0.0052472
v  ǁVelocityǁ                 0.016297          41.977          10.617          20.214
v  Pressure                    -401.92          350.63         -49.748          32.242
v  k                        4.4083e-08          87.857          4.0861           1.678
v  omega                         1e-24      1.1769e+07          8280.1          11.868
v  turbulent_viscosity      1.1996e-14          1.2546        0.015686         0.11133
v  CourantNb                   0.02315          2005.9            44.9          1.3768
v  FourierNb                  0.010899           14777          91.206         0.69287
v  total_pressure           1.0092e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010814        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84384           14851          136.11          2.0697


 TIME FOR THE TIME STEP              848:        0.45904E+02

===============================================================


 INSTANT    0.849000000E+02   TIME STEP NUMBER             849
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.600624015E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.60292E+02 0.14367E+02
   Friction velocity        uet   :  0.17790E-02 0.36983E+01
   Friction velocity        uk    :  0.35112E-01 0.44622E+01
   Dimensionless distance   yplus :  0.87213E-01 0.37363E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1971   0.45553E-02   0.31783E+00 
c  VelocityY    0.29405E+04    1971   0.45553E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1971   0.45553E-02   0.00000E+00 
c  Pressure     0.44309E+00    7119   0.35805E-01   0.21090E+00 
c  k            0.21872E+04    1387   0.97880E-04   0.95195E+00 
c  omega        0.10377E+08     384   0.59238E-04   0.18154E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0145e+05                             2
a  Local Time Step      1.0653e-05                         44434


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7039          1.1644       -0.003156      8.9301e-07
v  Velocity[Y]                 -32.403          30.201          6.6301          20.056
v  Velocity[Z]                 -28.679          28.511         0.17295       0.0055848
v  ǁVelocityǁ                  0.01863          33.312          10.616          20.214
v  Pressure                    -403.75          348.05         -51.441          32.517
v  k                         4.576e-09          44.674          4.1274          1.6776
v  omega                         1e-24      1.4162e+07          8203.9           11.86
v  turbulent_viscosity      8.5867e-14          1.2558         0.01573         0.11131
v  CourantNb                   0.06784          2057.7           44.82          1.3768
v  FourierNb                  0.010903           14597          92.731         0.69378
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14841        0.010814        0.045716


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14674          137.55          2.0706


 TIME FOR THE TIME STEP              849:        0.46509E+02

===============================================================


 INSTANT    0.850000000E+02   TIME STEP NUMBER             850
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.293827425E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30820E+02 0.14220E+02
   Friction velocity        uet   :  0.34309E-02 0.31449E+01
   Friction velocity        uk    :  0.24474E-01 0.31785E+01
   Dimensionless distance   yplus :  0.14608E+00 0.27152E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        488
   Nb of faces within the viscous sub-layer     :        989
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    2023   0.45005E-02   0.30934E+00 
c  VelocityY    0.29405E+04    2023   0.45005E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    2023   0.45005E-02   0.00000E+00 
c  Pressure     0.41958E+00    7126   0.37851E-01   0.20019E+00 
c  k            0.21793E+04    1314   0.62456E-04   0.81192E+00 
c  omega        0.10355E+08     365   0.61891E-04   0.20758E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5736e+05                             3
a  Local Time Step      1.1445e-05                         44403


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4847          1.1258      -0.0026508      3.5544e-07
v  Velocity[Y]                  -17.21           31.33          6.6123          20.056
v  Velocity[Z]                 -28.685          28.709          0.1778        0.005646
v  ǁVelocityǁ                 0.020146          33.361          10.597          20.214
v  Pressure                    -404.47          345.55         -53.415          32.548
v  k                         8.928e-10          46.346          4.1595          1.6772
v  omega                         1e-24      1.4477e+07          8264.5          11.864
v  turbulent_viscosity      2.5061e-15          1.2577         0.01579          0.1113
v  CourantNb                  0.024774          3092.4          44.799          1.3769
v  FourierNb                  0.010907           14414          93.413         0.69451
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869        0.010816        0.045756


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14470          138.21          2.0714


 TIME FOR THE TIME STEP              850:        0.47378E+02

===============================================================


 INSTANT    0.851000000E+02   TIME STEP NUMBER             851
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.332325155E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31874E+02 0.13969E+02
   Friction velocity        uet   :  0.17769E-02 0.29026E+01
   Friction velocity        uk    :  0.22111E-01 0.29168E+01
   Dimensionless distance   yplus :  0.11000E+00 0.27848E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        510
   Nb of faces within the viscous sub-layer     :       1006
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    2028   0.45838E-02   0.31181E+00 
c  VelocityY    0.29406E+04    2028   0.45838E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    2028   0.45838E-02   0.00000E+00 
c  Pressure     0.44613E+00    7110   0.35715E-01   0.21283E+00 
c  k            0.21729E+04    1311   0.64669E-04   0.72706E+00 
c  omega        0.15283E+08     257   0.31319E-04   0.24256E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -43826                             1
a  Local Time Step      1.1526e-05                         44398


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.437           1.061      -0.0024835     -1.7283e-06
v  Velocity[Y]                 -17.115          32.852          6.6234          20.056
v  Velocity[Z]                 -28.864          29.018         0.16961       0.0055502
v  ǁVelocityǁ                  0.01076          33.898          10.575          20.213
v  Pressure                    -403.24          345.62          -54.98          32.533
v  k                        7.4434e-09          46.766          4.1921          1.6769
v  omega                         1e-24      1.5598e+07          8211.2           11.87
v  turbulent_viscosity       1.628e-15          1.2605         0.01583         0.11129
v  CourantNb                  0.038931          2178.7          44.364          1.3768
v  FourierNb                  0.010911           14465          94.377         0.69488
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14818        0.010816         0.04576


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14505          138.74          2.0717


 TIME FOR THE TIME STEP              851:        0.46540E+02

===============================================================


 INSTANT    0.852000000E+02   TIME STEP NUMBER             852
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.269735922E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31749E+02 0.14022E+02
   Friction velocity        uet   :  0.36113E-02 0.29143E+01
   Friction velocity        uk    :  0.10178E-01 0.32063E+01
   Dimensionless distance   yplus :  0.12075E+00 0.30541E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        508
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    2021   0.46830E-02   0.32739E+00 
c  VelocityY    0.29408E+04    2021   0.46830E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    2021   0.46830E-02   0.00000E+00 
c  Pressure     0.42689E+00    7081   0.34246E-01   0.20320E+00 
c  k            0.21679E+04    1401   0.74189E-04   0.79055E+00 
c  omega        0.30991E+19       2   0.71253E-14   0.26718E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2771e+05                             2
a  Local Time Step      1.0371e-05                         44405


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3612         0.97562      -0.0031784     -2.6864e-06
v  Velocity[Y]                 -16.079          33.218          6.6525          20.056
v  Velocity[Z]                 -29.145           29.22         0.14946       0.0053697
v  ǁVelocityǁ                0.0096056          33.689          10.557          20.213
v  Pressure                     -395.9          345.68         -56.177          32.228
v  k                        2.3383e-08           53.57          4.1691          1.6765
v  omega                         1e-24      1.3762e+08            8450          11.873
v  turbulent_viscosity      1.3492e-14          1.2634        0.015853         0.11129
v  CourantNb                  0.029974          2085.4          43.915          1.3767
v  FourierNb                  0.010916           14581          96.238         0.69545
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010816        0.045733


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99209           14628          140.15          2.0722


 TIME FOR THE TIME STEP              852:        0.45972E+02

===============================================================


 INSTANT    0.853000000E+02   TIME STEP NUMBER             853
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.464982310E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31637E+02 0.14318E+02
   Friction velocity        uet   :  0.17164E-02 0.28521E+01
   Friction velocity        uk    :  0.25229E-01 0.32291E+01
   Dimensionless distance   yplus :  0.13012E+00 0.34411E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        484
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1950   0.45206E-02   0.34539E+00 
c  VelocityY    0.29411E+04    1950   0.45206E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1950   0.45206E-02   0.00000E+00 
c  Pressure     0.42034E+00    7031   0.31975E-01   0.19933E+00 
c  k            0.21623E+04    1523   0.77372E-04   0.81792E+00 
c  omega        0.74772E+08     200   0.19192E-04   0.86978E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4377e+05                             2
a  Local Time Step      1.0465e-05                         44422


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1813         0.91214      -0.0044129     -2.5267e-06
v  Velocity[Y]                 -17.307          32.869          6.6751          20.057
v  Velocity[Z]                 -28.686          29.212         0.11758       0.0048418
v  ǁVelocityǁ                 0.021637          33.372          10.548          20.214
v  Pressure                    -376.45          345.35         -56.927          31.944
v  k                        1.3446e-07          46.267          4.0901          1.6761
v  omega                         1e-24      6.9229e+07          8398.8          11.901
v  turbulent_viscosity      3.3876e-15          1.2661        0.015814         0.11125
v  CourantNb                   0.02717          2094.2          43.874          1.3769
v  FourierNb                  0.010922           14772          96.459         0.69524
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010816        0.045708


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87369           14828          140.33          2.0721


 TIME FOR THE TIME STEP              853:        0.45966E+02

===============================================================


 INSTANT    0.854000000E+02   TIME STEP NUMBER             854
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.366514614E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31446E+02 0.22013E+02
   Friction velocity        uet   :  0.25260E-02 0.27299E+01
   Friction velocity        uk    :  0.22881E-01 0.31185E+01
   Dimensionless distance   yplus :  0.12415E+00 0.38564E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1787   0.44680E-02   0.35332E+00 
c  VelocityY    0.29413E+04    1787   0.44680E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1787   0.44680E-02   0.00000E+00 
c  Pressure     0.44151E+00    7029   0.29326E-01   0.20861E+00 
c  k            0.21574E+04    1503   0.65141E-04   0.76622E+00 
c  omega        0.21578E+08     261   0.35068E-04   0.28130E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8028e+05                             2
a  Local Time Step      1.1376e-05                         44384


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3074         0.90895       -0.005743     -3.8751e-06
v  Velocity[Y]                 -17.511          30.907          6.6872          20.057
v  Velocity[Z]                 -28.663          29.396        0.086155       0.0040345
v  ǁVelocityǁ                0.0062965          32.821          10.523          20.213
v  Pressure                    -360.38          345.34         -56.351          31.595
v  k                        1.7457e-08           40.14          3.9961          1.6758
v  omega                         1e-24      3.5496e+07          8152.2          11.868
v  turbulent_viscosity      6.0269e-14          1.2705        0.015752         0.11126
v  CourantNb                  0.053497            2090          44.117          1.3773
v  FourierNb                  0.010927           14952           95.03         0.69442
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14928        0.010818        0.045722


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99351           14998          139.15          2.0717


 TIME FOR THE TIME STEP              854:        0.44392E+02

===============================================================


 INSTANT    0.855000000E+02   TIME STEP NUMBER             855
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.515275950E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30760E+02 0.20484E+02
   Friction velocity        uet   :  0.32915E-03 0.24693E+01
   Friction velocity        uk    :  0.23471E-01 0.27770E+01
   Dimensionless distance   yplus :  0.15830E+00 0.32087E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        337
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1632   0.43669E-02   0.37174E+00 
c  VelocityY    0.29415E+04    1632   0.43669E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1632   0.43669E-02   0.00000E+00 
c  Pressure     0.40089E+00    6721   0.28889E-01   0.19004E+00 
c  k            0.21550E+04    1450   0.63089E-04   0.83078E+00 
c  omega        0.11300E+08     208   0.43351E-04   0.29861E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4682e+05                             2
a  Local Time Step      1.1558e-05                         44359


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4983          1.0047      -0.0070307     -2.1023e-06
v  Velocity[Y]                 -16.762          32.201          6.7123          20.057
v  Velocity[Z]                 -30.077          29.352        0.053276        0.003143
v  ǁVelocityǁ                0.0057375          35.981          10.504          20.213
v  Pressure                    -357.23          345.44         -54.663          31.558
v  k                         3.825e-08           46.97          3.9455          1.6758
v  omega                         1e-24      2.0689e+07          8113.9          11.862
v  turbulent_viscosity      2.0695e-13          1.2764        0.015715         0.11127
v  CourantNb                  0.037577          2071.3          44.268          1.3773
v  FourierNb                  0.010932           15036          94.255         0.69371
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010818        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9447           15079          138.52           2.071


 TIME FOR THE TIME STEP              855:        0.41973E+02

===============================================================


 INSTANT    0.856000000E+02   TIME STEP NUMBER             856
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.347740112E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31420E+02 0.21764E+02
   Friction velocity        uet   :  0.73211E-03 0.30688E+01
   Friction velocity        uk    :  0.21796E-01 0.29949E+01
   Dimensionless distance   yplus :  0.10458E+00 0.28019E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :       1000
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1717   0.42777E-02   0.39676E+00 
c  VelocityY    0.29417E+04    1717   0.42777E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1717   0.42777E-02   0.00000E+00 
c  Pressure     0.42487E+00    7056   0.29818E-01   0.20061E+00 
c  k            0.21558E+04    1358   0.65539E-04   0.97359E+00 
c  omega        0.10918E+08     189   0.97983E-04   0.78491E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0072e+05                             3
a  Local Time Step      1.1469e-05                         44371


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.578          1.3399      -0.0079601     -2.6031e-06
v  Velocity[Y]                 -15.218          32.652          6.7475          20.056
v  Velocity[Z]                 -31.385          29.322       0.0038521       0.0022946
v  ǁVelocityǁ                 0.024878          36.429          10.506          20.212
v  Pressure                    -377.76          346.98         -51.947          31.784
v  k                         2.192e-08          57.397          3.9467           1.676
v  omega                         1e-24       3.459e+07          8329.4           11.87
v  turbulent_viscosity      2.9187e-13          1.2835        0.015718         0.11129
v  CourantNb                  0.043802          2046.1          44.409          1.3772
v  FourierNb                  0.010932           15186          93.197         0.69329
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010818        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15232          137.61          2.0705


 TIME FOR THE TIME STEP              856:        0.44721E+02

===============================================================


 INSTANT    0.857000000E+02   TIME STEP NUMBER             857
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.287927886E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31682E+02 0.19882E+02
   Friction velocity        uet   :  0.25790E-02 0.31684E+01
   Friction velocity        uk    :  0.27083E-01 0.30496E+01
   Dimensionless distance   yplus :  0.12908E+00 0.28179E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1765   0.46648E-02   0.41644E+00 
c  VelocityY    0.29421E+04    1765   0.46648E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1765   0.46648E-02   0.00000E+00 
c  Pressure     0.40692E+00    7118   0.34533E-01   0.19223E+00 
c  k            0.21613E+04    1080   0.75440E-04   0.11105E+01 
c  omega        0.13508E+08     219   0.30515E-03   0.41132E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3539e+05                             1
a  Local Time Step       1.085e-05                         44341


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6698          1.6073      -0.0088252       -4.66e-07
v  Velocity[Y]                 -15.217          32.846          6.7938          20.056
v  Velocity[Z]                  -32.56          28.976       -0.024818       0.0013591
v  ǁVelocityǁ                0.0089765          35.191          10.553          20.212
v  Pressure                    -420.58          348.77         -49.872          31.996
v  k                        2.2123e-07          64.347          3.9665          1.6763
v  omega                         1e-24        9.66e+07          9268.5          11.936
v  turbulent_viscosity      1.1584e-13          1.2913        0.015748         0.11132
v  CourantNb                  0.027778          2317.8          44.422          1.3767
v  FourierNb                  0.010926           15296          92.737         0.69326
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010819        0.045713


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15348          137.16            2.07


 TIME FOR THE TIME STEP              857:        0.44042E+02

===============================================================


 INSTANT    0.858000000E+02   TIME STEP NUMBER             858
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.232657385E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30128E+02 0.17668E+02
   Friction velocity        uet   :  0.24643E-02 0.31857E+01
   Friction velocity        uk    :  0.12522E-01 0.31821E+01
   Dimensionless distance   yplus :  0.11492E+00 0.28293E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1073
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    1845   0.46955E-02   0.43578E+00 
c  VelocityY    0.29424E+04    1845   0.46955E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    1845   0.46955E-02   0.00000E+00 
c  Pressure     0.44648E+00    7039   0.37069E-01   0.21152E+00 
c  k            0.21719E+04    1318   0.74697E-04   0.11857E+01 
c  omega        0.58483E+08     122   0.59140E-04   0.34397E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1838e+05                             4
a  Local Time Step      1.1862e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8401          1.7793      -0.0097152     -1.1602e-06
v  Velocity[Y]                 -18.545          29.932          6.8304          20.056
v  Velocity[Z]                 -33.197          29.002       -0.015324      2.8647e-05
v  ǁVelocityǁ                 0.017894          35.038           10.59          20.212
v  Pressure                    -437.47          349.02         -48.646          32.112
v  k                        2.8264e-07          63.994          3.9855          1.6768
v  omega                         1e-24      8.1105e+07          9385.6          11.953
v  turbulent_viscosity      5.9911e-14          1.2976        0.015765         0.11135
v  CourantNb                  0.011669          2689.1          44.489          1.3763
v  FourierNb                   0.01092           15365          92.252         0.69314
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14894        0.010819         0.04569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15425          136.74          2.0695


 TIME FOR THE TIME STEP              858:        0.44355E+02

===============================================================


 INSTANT    0.859000000E+02   TIME STEP NUMBER             859
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.999942247E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30644E+02 0.16368E+02
   Friction velocity        uet   :  0.18301E-02 0.30173E+01
   Friction velocity        uk    :  0.18661E-01 0.27887E+01
   Dimensionless distance   yplus :  0.77776E-01 0.27827E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        459
   Nb of faces within the viscous sub-layer     :       1032
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29428E+04    1809   0.45898E-02   0.42444E+00 
c  VelocityY    0.29428E+04    1809   0.45898E-02   0.00000E+00 
c  VelocityZ    0.29428E+04    1809   0.45898E-02   0.00000E+00 
c  Pressure     0.45162E+00    7002   0.35898E-01   0.21412E+00 
c  k            0.21839E+04    1475   0.77169E-04   0.12196E+01 
c  omega        0.41396E+08     129   0.36441E-04   0.10468E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.627e+05                             4
a  Local Time Step      1.1679e-05                         44428


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9177          1.6064      -0.0096367      3.6731e-06
v  Velocity[Y]                 -23.591          29.752           6.821          20.056
v  Velocity[Z]                 -33.166          28.814       0.0079923     -0.00088513
v  ǁVelocityǁ                 0.013036          34.483          10.597          20.212
v  Pressure                    -433.61          348.15          -48.28          32.034
v  k                        1.1491e-08          53.272          4.0112          1.6772
v  omega                         1e-24      4.1214e+07          8699.3          11.902
v  turbulent_viscosity       5.863e-14          1.3056         0.01577         0.11139
v  CourantNb                  0.022232          2545.3          44.619           1.376
v  FourierNb                  0.010914           15227          92.028         0.69324
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010819        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.95916           15295          136.65          2.0693


 TIME FOR THE TIME STEP              859:        0.43559E+02

===============================================================


 INSTANT    0.860000000E+02   TIME STEP NUMBER             860
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.231094609E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31552E+02 0.14130E+02
   Friction velocity        uet   :  0.10674E-02 0.29143E+01
   Friction velocity        uk    :  0.25366E-01 0.29635E+01
   Dimensionless distance   yplus :  0.19526E+00 0.27285E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :       1066
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29430E+04    1596   0.44421E-02   0.39142E+00 
c  VelocityY    0.29430E+04    1596   0.44421E-02   0.00000E+00 
c  VelocityZ    0.29430E+04    1596   0.44421E-02   0.00000E+00 
c  Pressure     0.43120E+00    6683   0.32483E-01   0.20395E+00 
c  k            0.21936E+04    1450   0.77868E-04   0.12226E+01 
c  omega        0.15669E+08     230   0.10445E-03   0.97528E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1379e+05                             2
a  Local Time Step      1.1506e-05                         44443


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8198          1.3311      -0.0079558      2.9753e-06
v  Velocity[Y]                 -33.403          29.618          6.7477          20.057
v  Velocity[Z]                 -30.021          28.568        0.021082      -0.0020945
v  ǁVelocityǁ                 0.014013          33.638          10.598          20.213
v  Pressure                    -414.35          346.29         -48.896          31.641
v  k                        4.1797e-09          67.746          4.0838          1.6777
v  omega                         1e-24      4.9035e+07          8749.2          11.902
v  turbulent_viscosity      6.8624e-16          1.3133        0.015778         0.11144
v  CourantNb                  0.043898          2069.2          44.646          1.3758
v  FourierNb                  0.010908           14954          92.441         0.69364
v  total_pressure           1.0091e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14837         0.01082        0.045653


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15028          137.09          2.0694


 TIME FOR THE TIME STEP              860:        0.41390E+02

===============================================================


 INSTANT    0.861000000E+02   TIME STEP NUMBER             861
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.107450017E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31967E+02 0.23166E+02
   Friction velocity        uet   :  0.19423E-02 0.30451E+01
   Friction velocity        uk    :  0.16384E-01 0.30966E+01
   Dimensionless distance   yplus :  0.14142E+00 0.26810E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        425
   Nb of faces within the viscous sub-layer     :       1062
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29431E+04    1595   0.46064E-02   0.36808E+00 
c  VelocityY    0.29431E+04    1595   0.46064E-02   0.00000E+00 
c  VelocityZ    0.29431E+04    1595   0.46064E-02   0.00000E+00 
c  Pressure     0.41076E+00    7092   0.30903E-01   0.19361E+00 
c  k            0.21976E+04    1378   0.10767E-03   0.11265E+01 
c  omega        0.14189E+09     125   0.53424E-05   0.34464E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1905e+05                             3
a  Local Time Step      1.0515e-05                         44440


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5987          1.0956      -0.0058764      1.9877e-06
v  Velocity[Y]                 -23.191          29.809          6.6645          20.057
v  Velocity[Z]                  -28.68          28.722         0.02752      -0.0034791
v  ǁVelocityǁ                 0.015055          33.102          10.631          20.213
v  Pressure                    -406.59          343.39         -51.081          31.255
v  k                        2.2299e-07          113.93          4.1964          1.6784
v  omega                         1e-24      2.5738e+07          8416.6          11.888
v  turbulent_viscosity      1.2674e-14          1.3202        0.015802          0.1115
v  CourantNb                  0.034508          2060.8          44.519          1.3756
v  FourierNb                  0.010902           14871          93.965         0.69467
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891        0.010819        0.045644


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91924           14914          138.48          2.0703


 TIME FOR THE TIME STEP              861:        0.41789E+02

===============================================================


 INSTANT    0.862000000E+02   TIME STEP NUMBER             862
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.385021076E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32046E+02 0.17370E+02
   Friction velocity        uet   :  0.66065E-03 0.27200E+01
   Friction velocity        uk    :  0.22161E-01 0.38277E+01
   Dimensionless distance   yplus :  0.13480E+00 0.35671E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        420
   Nb of faces within the viscous sub-layer     :       1058
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29430E+04    1721   0.44789E-02   0.36736E+00 
c  VelocityY    0.29430E+04    1721   0.44789E-02   0.00000E+00 
c  VelocityZ    0.29430E+04    1721   0.44789E-02   0.00000E+00 
c  Pressure     0.45111E+00    7067   0.34786E-01   0.21377E+00 
c  k            0.21973E+04    1444   0.16397E-03   0.97542E+00 
c  omega        0.10993E+08     549   0.70049E-04   0.21821E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6025e+05                             1
a  Local Time Step      1.1265e-05                         44463


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3455         0.93622      -0.0046306      1.6677e-07
v  Velocity[Y]                 -34.163          30.063          6.6502          20.057
v  Velocity[Z]                 -28.735          28.462         0.04867      -0.0044373
v  ǁVelocityǁ                 0.012282          35.181          10.653          20.214
v  Pressure                    -409.86           341.8         -54.278          31.275
v  k                        7.2299e-10           99.51           4.272          1.6793
v  omega                         1e-24      1.7198e+07          8354.3          11.891
v  turbulent_viscosity      7.7958e-14          1.3259        0.015838         0.11158
v  CourantNb                  0.018573          2047.6          44.354          1.3757
v  FourierNb                  0.010897           15028           95.94         0.69611
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14812        0.010819        0.045657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15067          140.29          2.0718


 TIME FOR THE TIME STEP              862:        0.44017E+02

===============================================================


 INSTANT    0.863000000E+02   TIME STEP NUMBER             863
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.954919468E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.37501E+02 0.13253E+02
   Friction velocity        uet   :  0.26282E-03 0.32699E+01
   Friction velocity        uk    :  0.19497E-01 0.36743E+01
   Dimensionless distance   yplus :  0.12587E+00 0.35151E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29430E+04    1824   0.44586E-02   0.36726E+00 
c  VelocityY    0.29430E+04    1824   0.44586E-02   0.00000E+00 
c  VelocityZ    0.29430E+04    1824   0.44586E-02   0.00000E+00 
c  Pressure     0.42573E+00    7142   0.37358E-01   0.20162E+00 
c  k            0.21965E+04    1463   0.12030E-03   0.88471E+00 
c  omega        0.35689E+16       2   0.12035E-11   0.14535E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4327e+05                             1
a  Local Time Step      1.1103e-05                         44469


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1246          1.0177      -0.0042886       7.728e-07
v  Velocity[Y]                 -20.942          30.676          6.6741          20.056
v  Velocity[Z]                  -28.86          28.775        0.072365      -0.0055698
v  ǁVelocityǁ                 0.019944          33.476          10.659          20.213
v  Pressure                    -411.66          342.59         -57.433          31.243
v  k                        2.0243e-08          54.946          4.2787          1.6804
v  omega                         1e-24      1.1913e+07          8133.4          11.851
v  turbulent_viscosity      1.3028e-16           1.334         0.01586         0.11166
v  CourantNb                  0.044228          2954.7          44.427          1.3759
v  FourierNb                  0.010892           15046          95.831         0.69675
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14829        0.010818        0.045683


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15086          140.26          2.0726


 TIME FOR THE TIME STEP              863:        0.44187E+02

===============================================================


 INSTANT    0.864000000E+02   TIME STEP NUMBER             864
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.100844057E-15
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31082E+02 0.13447E+02
   Friction velocity        uet   :  0.13116E-02 0.25950E+01
   Friction velocity        uk    :  0.21504E-01 0.30044E+01
   Dimensionless distance   yplus :  0.14762E+00 0.28453E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        511
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29429E+04    2139   0.46187E-02   0.36247E+00 
c  VelocityY    0.29429E+04    2139   0.46187E-02   0.00000E+00 
c  VelocityZ    0.29429E+04    2139   0.46187E-02   0.00000E+00 
c  Pressure     0.43511E+00    7129   0.34976E-01   0.20561E+00 
c  k            0.21979E+04    1573   0.77554E-04   0.77252E+00 
c  omega        0.10127E+08     416   0.32920E-04   0.12253E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6626e+05                             1
a  Local Time Step       1.098e-05                         44476


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0505          1.0406      -0.0032628      4.2088e-07
v  Velocity[Y]                 -17.355          31.188          6.7061          20.056
v  Velocity[Z]                 -28.871          28.935        0.081431      -0.0061094
v  ǁVelocityǁ                  0.01562          33.762          10.641          20.213
v  Pressure                    -412.18          343.85         -59.347          31.221
v  k                        5.8744e-08            53.1          4.3327          1.6818
v  omega                         1e-24      1.1687e+07          7993.6          11.857
v  turbulent_viscosity      1.1114e-14           1.331        0.015891         0.11175
v  CourantNb                  0.055901            2587          44.294          1.3761
v  FourierNb                  0.010887           15438          97.513         0.69761
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1487        0.010816        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15483          141.81          2.0737


 TIME FOR THE TIME STEP              864:        0.48401E+02

===============================================================


 INSTANT    0.865000000E+02   TIME STEP NUMBER             865
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.195627818E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31364E+02 0.13997E+02
   Friction velocity        uet   :  0.13829E-02 0.28177E+01
   Friction velocity        uk    :  0.20108E-01 0.29411E+01
   Dimensionless distance   yplus :  0.10169E+00 0.28844E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        551
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29428E+04    1987   0.47575E-02   0.36858E+00 
c  VelocityY    0.29428E+04    1987   0.47575E-02   0.00000E+00 
c  VelocityZ    0.29428E+04    1987   0.47575E-02   0.00000E+00 
c  Pressure     0.44284E+00    6995   0.31322E-01   0.20833E+00 
c  k            0.21995E+04    1539   0.84110E-04   0.83318E+00 
c  omega        0.10143E+08     496   0.41670E-04   0.12214E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9623e+05                             2
a  Local Time Step      1.1003e-05                         44467


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98007          1.0369      -0.0016731     -1.8965e-08
v  Velocity[Y]                 -16.091          33.083           6.739          20.056
v  Velocity[Z]                 -29.001          30.372          0.0772      -0.0068742
v  ǁVelocityǁ                 0.015732          33.591          10.603          20.213
v  Pressure                    -409.73          345.16         -59.891          31.076
v  k                        7.0824e-07          48.783          4.2872          1.6833
v  omega                         1e-24      1.1682e+07          7900.2          11.842
v  turbulent_viscosity      8.3528e-15          1.3365        0.015887         0.11187
v  CourantNb                  0.044915            2021          44.142          1.3764
v  FourierNb                  0.010884           15670          99.045         0.69804
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14902        0.010815        0.045697


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15725          143.19          2.0744


 TIME FOR THE TIME STEP              865:        0.46882E+02

===============================================================


 INSTANT    0.866000000E+02   TIME STEP NUMBER             866
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.254159978E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32009E+02 0.16693E+02
   Friction velocity        uet   :  0.29595E-03 0.28361E+01
   Friction velocity        uk    :  0.27772E-01 0.32336E+01
   Dimensionless distance   yplus :  0.94847E-01 0.31376E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :        951
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29428E+04    1896   0.45212E-02   0.37972E+00 
c  VelocityY    0.29428E+04    1896   0.45212E-02   0.00000E+00 
c  VelocityZ    0.29428E+04    1896   0.45212E-02   0.00000E+00 
c  Pressure     0.47061E+00    7023   0.32361E-01   0.22499E+00 
c  k            0.21994E+04    1494   0.70091E-04   0.83955E+00 
c  omega        0.10087E+08     420   0.45204E-03   0.66869E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2668e+05                             3
a  Local Time Step      1.1412e-05                         44432


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98281         0.97955       4.811e-05     -7.0182e-07
v  Velocity[Y]                 -15.624          32.808          6.7412          20.056
v  Velocity[Z]                 -28.551          29.267        0.052354      -0.0076311
v  ǁVelocityǁ                 0.012823           33.35          10.575          20.213
v  Pressure                    -396.48          345.22         -59.979          30.821
v  k                        6.1587e-07          42.014          4.1971          1.6851
v  omega                         1e-24      2.0438e+08          8909.2          11.912
v  turbulent_viscosity      1.0261e-13          1.3409        0.015855           0.112
v  CourantNb                  0.052359            2020          44.052          1.3767
v  FourierNb                  0.010881           15877          99.757         0.69818
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010815        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15939          143.81          2.0749


 TIME FOR THE TIME STEP              866:        0.46023E+02

===============================================================


 INSTANT    0.867000000E+02   TIME STEP NUMBER             867
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.257881034E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31182E+02 0.22649E+02
   Friction velocity        uet   :  0.13229E-02 0.27034E+01
   Friction velocity        uk    :  0.19745E-01 0.31989E+01
   Dimensionless distance   yplus :  0.12428E+00 0.40207E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :        957
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29426E+04    1982   0.44574E-02   0.38708E+00 
c  VelocityY    0.29426E+04    1982   0.44574E-02   0.00000E+00 
c  VelocityZ    0.29426E+04    1982   0.44574E-02   0.00000E+00 
c  Pressure     0.42180E+00    6990   0.32272E-01   0.20034E+00 
c  k            0.22001E+04    1459   0.64803E-04   0.75457E+00 
c  omega        0.16482E+09     115   0.11815E-04   0.18756E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7563e+05                             2
a  Local Time Step      1.0907e-05                         44408


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89247         0.91554       0.0013755     -3.4608e-07
v  Velocity[Y]                 -15.188          32.768          6.7344          20.056
v  Velocity[Z]                 -28.696          29.036        0.025964      -0.0082244
v  ǁVelocityǁ                 0.010256          33.029          10.554          20.213
v  Pressure                    -378.14          345.01         -59.581          30.319
v  k                        2.5607e-08          40.678          4.1045          1.6873
v  omega                         1e-24       1.025e+08          8512.2          11.893
v  turbulent_viscosity      2.7306e-13          1.3464        0.015782         0.11216
v  CourantNb                  0.064678          2012.6          44.142          1.3772
v  FourierNb                   0.01088           15965          97.987         0.69764
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14897        0.010815        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16039          142.13          2.0749


 TIME FOR THE TIME STEP              867:        0.47601E+02

===============================================================


 INSTANT    0.868000000E+02   TIME STEP NUMBER             868
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.271494288E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30154E+02 0.20363E+02
   Friction velocity        uet   :  0.81438E-03 0.26333E+01
   Friction velocity        uk    :  0.25262E-01 0.32508E+01
   Dimensionless distance   yplus :  0.10135E+00 0.30892E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        401
   Nb of faces within the viscous sub-layer     :        949
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29425E+04    2017   0.46333E-02   0.39560E+00 
c  VelocityY    0.29425E+04    2017   0.46333E-02   0.00000E+00 
c  VelocityZ    0.29425E+04    2017   0.46333E-02   0.00000E+00 
c  Pressure     0.44129E+00    7011   0.29799E-01   0.20994E+00 
c  k            0.22023E+04    1459   0.63595E-04   0.80784E+00 
c  omega        0.43102E+08     152   0.25435E-04   0.86077E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5416e+05                             2
a  Local Time Step      1.1673e-05                         44399


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.67689         0.97939       0.0016031      1.1463e-06
v  Velocity[Y]                 -15.236          30.454          6.7567          20.056
v  Velocity[Z]                 -30.223          28.883      -0.0012255      -0.0086491
v  ǁVelocityǁ                0.0041682          35.448          10.537          20.213
v  Pressure                    -358.34          347.87         -57.373          30.736
v  k                        3.1972e-08          40.401          4.0089          1.6897
v  omega                         1e-24      5.1842e+07          8190.4          11.879
v  turbulent_viscosity      2.1481e-13          1.3515        0.015714         0.11233
v  CourantNb                  0.074301          2021.1          44.391          1.3777
v  FourierNb                  0.010879           15918          96.631         0.69734
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010814         0.04564


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15964          141.02          2.0751


 TIME FOR THE TIME STEP              868:        0.46167E+02

===============================================================


 INSTANT    0.869000000E+02   TIME STEP NUMBER             869
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.175371753E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31528E+02 0.20281E+02
   Friction velocity        uet   :  0.43529E-03 0.28860E+01
   Friction velocity        uk    :  0.21528E-01 0.31412E+01
   Dimensionless distance   yplus :  0.10561E+00 0.29149E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        364
   Nb of faces within the viscous sub-layer     :        952
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29424E+04    2013   0.44205E-02   0.39874E+00 
c  VelocityY    0.29424E+04    2013   0.44205E-02   0.00000E+00 
c  VelocityZ    0.29424E+04    2013   0.44205E-02   0.00000E+00 
c  Pressure     0.42878E+00    7073   0.29366E-01   0.20330E+00 
c  k            0.22072E+04    1491   0.62136E-04   0.94904E+00 
c  omega        0.16348E+08     201   0.14291E-03   0.29916E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9583e+05                             2
a  Local Time Step      1.1133e-05                         44383


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.56064          1.2074       0.0014196       1.771e-06
v  Velocity[Y]                 -15.137          30.387          6.8022          20.057
v  Velocity[Z]                 -31.064          28.982       -0.018898      -0.0087822
v  ǁVelocityǁ                 0.028149          36.997          10.545          20.214
v  Pressure                    -364.42          350.96         -54.685          31.151
v  k                        1.5646e-08          51.428          3.9509          1.6926
v  omega                         1e-24      7.5467e+07            8608          11.884
v  turbulent_viscosity       5.169e-14          1.3527        0.015673         0.11252
v  CourantNb                  0.039732          2035.4          44.592          1.3777
v  FourierNb                   0.01088           16044          94.663         0.69726
v  total_pressure           1.0096e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14806        0.010813        0.045612


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16098          139.26           2.075


 TIME FOR THE TIME STEP              869:        0.46456E+02

===============================================================


 INSTANT    0.870000000E+02   TIME STEP NUMBER             870
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.122220899E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30735E+02 0.15011E+02
   Friction velocity        uet   :  0.10659E-02 0.31227E+01
   Friction velocity        uk    :  0.17223E-01 0.30487E+01
   Dimensionless distance   yplus :  0.19741E+00 0.29108E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :        958
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2074   0.43280E-02   0.39726E+00 
c  VelocityY    0.29422E+04    2074   0.43280E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2074   0.43280E-02   0.00000E+00 
c  Pressure     0.44453E+00    7132   0.33109E-01   0.21111E+00 
c  k            0.22166E+04    1631   0.66431E-04   0.11097E+01 
c  omega        0.54978E+08     117   0.21573E-04   0.10008E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6777e+05                             2
a  Local Time Step      1.1919e-05                         44401


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.61793          1.4614       0.0011294      1.8325e-06
v  Velocity[Y]                 -15.285            32.7          6.8591          20.057
v  Velocity[Z]                     -33          28.567         -0.0164      -0.0084984
v  ǁVelocityǁ                0.0073064          35.779          10.582          20.214
v  Pressure                    -417.11          352.62         -51.955          31.567
v  k                        9.0496e-08          63.443          3.9373          1.6957
v  omega                         1e-24      3.7751e+07          8323.4          11.862
v  turbulent_viscosity      4.1616e-14          1.3536         0.01568         0.11272
v  CourantNb                  0.035125          2192.9          44.654          1.3774
v  FourierNb                  0.010881           16050          93.567         0.69795
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14876        0.010813        0.045638


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16113          138.22          2.0754


 TIME FOR THE TIME STEP              870:        0.48492E+02

===============================================================


 INSTANT    0.871000000E+02   TIME STEP NUMBER             871
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.295578235E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30849E+02 0.13903E+02
   Friction velocity        uet   :  0.35872E-02 0.32316E+01
   Friction velocity        uk    :  0.21676E-01 0.29095E+01
   Dimensionless distance   yplus :  0.13431E+00 0.28500E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1995   0.43903E-02   0.39740E+00 
c  VelocityY    0.29421E+04    1995   0.43903E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1995   0.43903E-02   0.00000E+00 
c  Pressure     0.42305E+00    7110   0.36628E-01   0.20015E+00 
c  k            0.22321E+04    1704   0.68051E-04   0.11877E+01 
c  omega        0.17396E+08     226   0.99820E-04   0.13356E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -61176                             1
a  Local Time Step       1.153e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.68181          1.6632      0.00061837       3.453e-06
v  Velocity[Y]                 -15.811          31.491          6.9045          20.056
v  Velocity[Z]                 -32.503          28.622        0.010691      -0.0084024
v  ǁVelocityǁ                0.0063653          34.414           10.62          20.214
v  Pressure                    -439.23          352.25         -50.359          31.651
v  k                        7.1662e-08          66.604          3.9469          1.6989
v  omega                         1e-24       6.281e+07          8598.2          11.894
v  turbulent_viscosity      3.1005e-14          1.3548        0.015721         0.11295
v  CourantNb                  0.045345          2823.6            44.8           1.377
v  FourierNb                  0.010883           15763          92.465         0.69911
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14844        0.010811        0.045625


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94896           15835          137.26          2.0762


 TIME FOR THE TIME STEP              871:        0.48898E+02

===============================================================


 INSTANT    0.872000000E+02   TIME STEP NUMBER             872
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.193400055E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30441E+02 0.13927E+02
   Friction velocity        uet   :  0.84299E-03 0.31135E+01
   Friction velocity        uk    :  0.15901E-01 0.31736E+01
   Dimensionless distance   yplus :  0.99011E-01 0.27720E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :       1001
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29420E+04    1884   0.43507E-02   0.38069E+00 
c  VelocityY    0.29420E+04    1884   0.43507E-02   0.00000E+00 
c  VelocityZ    0.29420E+04    1884   0.43507E-02   0.00000E+00 
c  Pressure     0.43625E+00    7062   0.36266E-01   0.20795E+00 
c  k            0.22504E+04    1643   0.68728E-04   0.12426E+01 
c  omega        0.20451E+08     168   0.14106E-03   0.25107E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0811e+05                             4
a  Local Time Step      1.1424e-05                         44489


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.74934           1.647      7.3341e-05      3.1561e-06
v  Velocity[Y]                  -22.87          29.971          6.8932          20.056
v  Velocity[Z]                 -32.241          28.747        0.044889      -0.0079866
v  ǁVelocityǁ                0.0038905          33.279          10.606          20.214
v  Pressure                    -439.17          350.87         -49.582          31.831
v  k                        6.1554e-07          58.428          3.9597           1.702
v  omega                         1e-24      7.1928e+07            9312          11.945
v  turbulent_viscosity      1.4882e-14          1.3539        0.015754         0.11318
v  CourantNb                  0.032791          2773.3          44.882          1.3768
v  FourierNb                  0.010885           15397          91.775         0.70026
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14763         0.01081        0.045618


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15475          136.66           2.077


 TIME FOR THE TIME STEP              872:        0.46793E+02

===============================================================


 INSTANT    0.873000000E+02   TIME STEP NUMBER             873
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.142598278E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31976E+02 0.13824E+02
   Friction velocity        uet   :  0.23569E-02 0.28312E+01
   Friction velocity        uk    :  0.12920E-01 0.30459E+01
   Dimensionless distance   yplus :  0.11086E+00 0.27050E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :        981
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1764   0.44942E-02   0.34841E+00 
c  VelocityY    0.29419E+04    1764   0.44942E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1764   0.44942E-02   0.00000E+00 
c  Pressure     0.41567E+00    7003   0.32418E-01   0.19777E+00 
c  k            0.22667E+04    1495   0.71952E-04   0.12872E+01 
c  omega        0.31677E+08     135   0.50575E-04   0.11074E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -53776                             1
a  Local Time Step       1.085e-05                         44534


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.80442          1.4253      0.00046561      2.6577e-06
v  Velocity[Y]                 -26.564          29.812          6.8068          20.057
v  Velocity[Z]                 -31.328          28.542        0.072931      -0.0072321
v  ǁVelocityǁ                0.0049525           32.76          10.582          20.215
v  Pressure                    -423.26          348.88         -49.908          31.599
v  k                        2.9097e-07           58.16          3.9991          1.7049
v  omega                         1e-24      4.0898e+07          8835.7           11.91
v  turbulent_viscosity      1.1075e-13          1.3528        0.015769         0.11342
v  CourantNb                  0.019691          2080.3          44.669          1.3767
v  FourierNb                  0.010888           15011           91.65         0.70161
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14825        0.010809        0.045632


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15058          136.32          2.0783


 TIME FOR THE TIME STEP              873:        0.43749E+02

===============================================================


 INSTANT    0.874000000E+02   TIME STEP NUMBER             874
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.769217023E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32173E+02 0.18945E+02
   Friction velocity        uet   :  0.78203E-03 0.27458E+01
   Friction velocity        uk    :  0.14994E-01 0.32076E+01
   Dimensionless distance   yplus :  0.12247E+00 0.27377E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        381
   Nb of faces within the viscous sub-layer     :        984
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29417E+04    1823   0.44162E-02   0.33062E+00 
c  VelocityY    0.29417E+04    1823   0.44162E-02   0.00000E+00 
c  VelocityZ    0.29417E+04    1823   0.44162E-02   0.00000E+00 
c  Pressure     0.42495E+00    7102   0.30377E-01   0.20175E+00 
c  k            0.22759E+04    1278   0.90703E-04   0.12419E+01 
c  omega        0.15203E+08     253   0.51089E-04   0.46088E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6557e+05                             1
a  Local Time Step      1.1624e-05                         44547


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.82988           1.416       0.0016731      4.5785e-06
v  Velocity[Y]                 -22.525          29.698          6.6964          20.056
v  Velocity[Z]                  -30.11           28.69        0.077294       -0.006636
v  ǁVelocityǁ                  0.01259           33.04          10.607          20.214
v  Pressure                    -402.89          348.07         -51.435          31.293
v  k                        6.5958e-10          87.737          4.0967          1.7077
v  omega                         1e-24      2.1684e+07          8471.8          11.886
v  turbulent_viscosity      5.2528e-14          1.3544        0.015792         0.11367
v  CourantNb                  0.020611          2006.5            44.3          1.3764
v  FourierNb                  0.010891           14925          92.718         0.70336
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14816        0.010809        0.045639


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14968          137.02          2.0798


 TIME FOR THE TIME STEP              874:        0.44804E+02

===============================================================


 INSTANT    0.875000000E+02   TIME STEP NUMBER             875
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.204214879E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30860E+02 0.16313E+02
   Friction velocity        uet   :  0.27274E-02 0.25808E+01
   Friction velocity        uk    :  0.19793E-01 0.31611E+01
   Dimensionless distance   yplus :  0.11889E+00 0.28718E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        384
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1838   0.45914E-02   0.32949E+00 
c  VelocityY    0.29415E+04    1838   0.45914E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1838   0.45914E-02   0.00000E+00 
c  Pressure     0.42656E+00    6981   0.32627E-01   0.20202E+00 
c  k            0.22770E+04    1171   0.10336E-03   0.11254E+01 
c  omega        0.11025E+08     476   0.44145E-04   0.17802E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80254                             1
a  Local Time Step      1.0747e-05                         44524


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.81446          1.3951       0.0027007      2.9079e-06
v  Velocity[Y]                 -36.332          30.156          6.6471          20.055
v  Velocity[Z]                 -29.066          28.678        0.094894        -0.00575
v  ǁVelocityǁ                 0.009634          36.788          10.642          20.214
v  Pressure                    -407.15           348.5         -53.771          31.458
v  k                        5.7831e-10          87.777          4.1897          1.7104
v  omega                         1e-24       1.326e+07          8383.9          11.905
v  turbulent_viscosity      2.7912e-15          1.3548        0.015831         0.11392
v  CourantNb                  0.025773          2023.8          44.125          1.3765
v  FourierNb                  0.010893           14864          94.613         0.70586
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869         0.01081        0.045647


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14909          138.74          2.0824


 TIME FOR THE TIME STEP              875:        0.44681E+02

===============================================================


 INSTANT    0.876000000E+02   TIME STEP NUMBER             876
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.210461085E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.41794E+02 0.14142E+02
   Friction velocity        uet   :  0.11124E-02 0.33733E+01
   Friction velocity        uk    :  0.31446E-01 0.34096E+01
   Dimensionless distance   yplus :  0.16524E+00 0.34012E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        410
   Nb of faces within the viscous sub-layer     :        993
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1767   0.46023E-02   0.33040E+00 
c  VelocityY    0.29416E+04    1767   0.46023E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1767   0.46023E-02   0.00000E+00 
c  Pressure     0.43816E+00    7138   0.35805E-01   0.20820E+00 
c  k            0.22743E+04    1342   0.10630E-03   0.10577E+01 
c  omega        0.10254E+08     410   0.38363E-04   0.11705E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7122e+05                             1
a  Local Time Step      1.1175e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79407          1.2198       0.0027086      1.7724e-06
v  Velocity[Y]                 -25.175          30.582          6.6354          20.056
v  Velocity[Z]                 -28.809          28.808         0.11211      -0.0049566
v  ǁVelocityǁ                 0.011423          33.554           10.65          20.215
v  Pressure                    -409.58          348.77         -56.364          31.652
v  k                        1.1908e-09           41.96          4.2107          1.7129
v  omega                         1e-24      1.1692e+07          8233.6          11.905
v  turbulent_viscosity       9.693e-16          1.3523        0.015885         0.11417
v  CourantNb                  0.058778          3051.1          44.475          1.3768
v  FourierNb                  0.010895           14856          95.358         0.70805
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14835        0.010808         0.04561


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14905          139.83          2.0849


 TIME FOR THE TIME STEP              876:        0.44614E+02

===============================================================


 INSTANT    0.877000000E+02   TIME STEP NUMBER             877
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.610835825E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30758E+02 0.14110E+02
   Friction velocity        uet   :  0.14147E-02 0.28242E+01
   Friction velocity        uk    :  0.30563E-01 0.28875E+01
   Dimensionless distance   yplus :  0.15510E+00 0.27770E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        444
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1736   0.44947E-02   0.33180E+00 
c  VelocityY    0.29416E+04    1736   0.44947E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1736   0.44947E-02   0.00000E+00 
c  Pressure     0.45053E+00    7112   0.34884E-01   0.21483E+00 
c  k            0.22703E+04    1440   0.70117E-04   0.91777E+00 
c  omega        0.10219E+08     311   0.35828E-04   0.11412E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -78165                             2
a  Local Time Step      1.1175e-05                         44470


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.76702          1.0218       0.0017497      1.4424e-06
v  Velocity[Y]                 -17.711          32.758          6.6494          20.057
v  Velocity[Z]                 -28.577           28.79         0.12342      -0.0043634
v  ǁVelocityǁ                 0.016235          33.627          10.631          20.216
v  Pressure                    -409.69             349         -57.876          31.802
v  k                        3.2459e-09          59.463          4.2306          1.7151
v  omega                         1e-24      1.1753e+07          8135.3          11.876
v  turbulent_viscosity      1.5306e-15          1.3491        0.015909         0.11441
v  CourantNb                  0.020318          2894.9          44.472          1.3771
v  FourierNb                  0.010897           14947          95.655         0.70959
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14855        0.010807        0.045606


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15004          140.13          2.0867


 TIME FOR THE TIME STEP              877:        0.43734E+02

===============================================================


 INSTANT    0.878000000E+02   TIME STEP NUMBER             878
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.200348521E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31412E+02 0.14158E+02
   Friction velocity        uet   :  0.26496E-02 0.29712E+01
   Friction velocity        uk    :  0.32678E-01 0.29641E+01
   Dimensionless distance   yplus :  0.23169E+00 0.28919E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :        966
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1804   0.43482E-02   0.34527E+00 
c  VelocityY    0.29415E+04    1804   0.43482E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1804   0.43482E-02   0.00000E+00 
c  Pressure     0.43059E+00    6961   0.32618E-01   0.20452E+00 
c  k            0.22658E+04    1473   0.71904E-04   0.93320E+00 
c  omega        0.10206E+08     335   0.36965E-04   0.13075E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8785e+05                             2
a  Local Time Step      1.1378e-05                         44486


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -0.8153         0.88671      0.00061938      1.1198e-06
v  Velocity[Y]                 -17.114          33.821          6.6778          20.057
v  Velocity[Z]                 -28.583          29.069         0.11582      -0.0032444
v  ǁVelocityǁ                 0.014604          33.966          10.596          20.217
v  Pressure                    -407.58          348.58         -58.266          31.711
v  k                         3.533e-08           80.13          4.2194          1.7169
v  omega                         1e-24      1.1748e+07            8025          11.857
v  turbulent_viscosity      3.2056e-15          1.3437        0.015938         0.11465
v  CourantNb                  0.051285          2069.8          44.257          1.3774
v  FourierNb                  0.010899           15051          97.195         0.71138
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14918        0.010806        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15116          141.45          2.0887


 TIME FOR THE TIME STEP              878:        0.44735E+02

===============================================================


 INSTANT    0.879000000E+02   TIME STEP NUMBER             879
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.454113951E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31398E+02 0.14401E+02
   Friction velocity        uet   :  0.23131E-02 0.29644E+01
   Friction velocity        uk    :  0.36754E-01 0.32286E+01
   Dimensionless distance   yplus :  0.13866E+00 0.31978E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        373
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1773   0.44578E-02   0.36844E+00 
c  VelocityY    0.29413E+04    1773   0.44578E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1773   0.44578E-02   0.00000E+00 
c  Pressure     0.44940E+00    7049   0.31319E-01   0.21334E+00 
c  k            0.22597E+04    1456   0.76397E-04   0.10334E+01 
c  omega        0.10211E+08     442   0.74038E-04   0.23567E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4934e+05                             3
a  Local Time Step      1.0884e-05                         44545


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88658         0.98533     -0.00049876      2.4606e-06
v  Velocity[Y]                 -15.701          33.464          6.7009          20.057
v  Velocity[Z]                 -28.703          29.075        0.082772      -0.0023883
v  ǁVelocityǁ                 0.013691          34.207          10.563          20.216
v  Pressure                    -396.92          347.22         -58.143          31.384
v  k                        3.6781e-07          87.089          4.1314          1.7185
v  omega                         1e-24      1.5606e+07          8204.4          11.886
v  turbulent_viscosity       5.296e-14          1.3378        0.015941         0.11487
v  CourantNb                  0.042207            2063          43.949          1.3775
v  FourierNb                  0.010899           15099          98.724         0.71307
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010807        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15172          142.67          2.0906


 TIME FOR THE TIME STEP              879:        0.44882E+02

===============================================================


 INSTANT    0.880000000E+02   TIME STEP NUMBER             880
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.407329542E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31604E+02 0.16766E+02
   Friction velocity        uet   :  0.12780E-02 0.27858E+01
   Friction velocity        uk    :  0.26207E-01 0.31839E+01
   Dimensionless distance   yplus :  0.14079E+00 0.36399E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        416
   Nb of faces within the viscous sub-layer     :        919
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1823   0.45291E-02   0.38598E+00 
c  VelocityY    0.29411E+04    1823   0.45291E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1823   0.45291E-02   0.00000E+00 
c  Pressure     0.39675E+00    6842   0.30328E-01   0.18776E+00 
c  k            0.22512E+04    1338   0.68447E-04   0.96662E+00 
c  omega        0.15915E+08     327   0.98771E-04   0.55307E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0647e+05                             3
a  Local Time Step      1.1776e-05                         44553


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92038           1.036      -0.0022077      1.2614e-06
v  Velocity[Y]                 -16.011          32.944          6.6836          20.056
v  Velocity[Z]                 -29.433           29.22        0.025495      -0.0014761
v  ǁVelocityǁ                  0.01583          33.354          10.527          20.216
v  Pressure                    -381.45          346.77         -57.138          31.063
v  k                         2.304e-07          45.109          4.0415          1.7197
v  omega                         1e-24      1.3269e+08          8631.1          11.917
v  turbulent_viscosity      3.9268e-14          1.3314        0.015892         0.11507
v  CourantNb                  0.043305          2047.9           43.92          1.3779
v  FourierNb                  0.010899           15075          98.033         0.71375
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14849        0.010806          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15143          141.95          2.0917


 TIME FOR THE TIME STEP              880:        0.44430E+02

===============================================================


 INSTANT    0.881000000E+02   TIME STEP NUMBER             881
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.973455923E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30584E+02 0.20277E+02
   Friction velocity        uet   :  0.26364E-02 0.27138E+01
   Friction velocity        uk    :  0.14857E-01 0.30287E+01
   Dimensionless distance   yplus :  0.71286E-01 0.34145E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        452
   Nb of faces within the viscous sub-layer     :        956
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    1996   0.45751E-02   0.40456E+00 
c  VelocityY    0.29410E+04    1996   0.45751E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    1996   0.45751E-02   0.00000E+00 
c  Pressure     0.42350E+00    7034   0.27798E-01   0.20100E+00 
c  k            0.22426E+04    1103   0.65183E-04   0.10260E+01 
c  omega        0.15407E+09     153   0.52159E-05   0.14156E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -90720                             1
a  Local Time Step      1.1834e-05                         44496


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0631          1.1454      -0.0033318      2.7012e-06
v  Velocity[Y]                 -15.306          30.713          6.6771          20.056
v  Velocity[Z]                 -30.133          29.113       -0.020748      -0.0004826
v  ǁVelocityǁ                 0.013739          34.458          10.502          20.216
v  Pressure                    -365.68          348.46         -55.416          31.044
v  k                        3.8932e-08          40.982          3.9755          1.7208
v  omega                         1e-24      6.6355e+07          8264.1          11.863
v  turbulent_viscosity      2.4386e-14          1.3236        0.015832         0.11525
v  CourantNb                  0.053656          2026.5          44.049          1.3783
v  FourierNb                  0.010897           15233          96.419         0.71392
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14793        0.010806        0.045682


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.7654           15286          140.47          2.0922


 TIME FOR THE TIME STEP              881:        0.46189E+02

===============================================================


 INSTANT    0.882000000E+02   TIME STEP NUMBER             882
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.413836078E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31059E+02 0.20313E+02
   Friction velocity        uet   :  0.53251E-03 0.28128E+01
   Friction velocity        uk    :  0.15853E-01 0.31296E+01
   Dimensionless distance   yplus :  0.16600E+00 0.28826E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    2047   0.46081E-02   0.42600E+00 
c  VelocityY    0.29409E+04    2047   0.46081E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    2047   0.46081E-02   0.00000E+00 
c  Pressure     0.44767E+00    7036   0.27554E-01   0.21239E+00 
c  k            0.22350E+04    1364   0.64259E-04   0.11759E+01 
c  omega        0.39798E+08     146   0.13061E-04   0.62723E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9434e+05                             2
a  Local Time Step      1.1373e-05                         44521


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3302           1.269      -0.0038961      3.3306e-06
v  Velocity[Y]                  -15.34          31.021          6.6968          20.056
v  Velocity[Z]                  -31.84          29.312       -0.074887      0.00047725
v  ǁVelocityǁ                 0.018851          36.587          10.491          20.216
v  Pressure                    -351.95          350.32         -52.772          31.246
v  k                          3.59e-09          53.306           3.958          1.7216
v  omega                         1e-24      3.3173e+07          8119.7           11.84
v  turbulent_viscosity      2.0409e-14          1.3158        0.015805          0.1154
v  CourantNb                  0.045774          2006.2          44.375          1.3784
v  FourierNb                  0.010895           15315          95.298         0.71424
v  total_pressure           1.0097e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14786        0.010808        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.85589           15378          139.67          2.0926


 TIME FOR THE TIME STEP              882:        0.47030E+02

===============================================================


 INSTANT    0.883000000E+02   TIME STEP NUMBER             883
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.445948288E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31924E+02 0.17807E+02
   Friction velocity        uet   :  0.15076E-02 0.30783E+01
   Friction velocity        uk    :  0.85667E-02 0.31777E+01
   Dimensionless distance   yplus :  0.96351E-01 0.28370E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        410
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    2034   0.44824E-02   0.44181E+00 
c  VelocityY    0.29409E+04    2034   0.44824E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    2034   0.44824E-02   0.00000E+00 
c  Pressure     0.44192E+00    7092   0.32376E-01   0.21103E+00 
c  k            0.22301E+04    1506   0.70526E-04   0.13598E+01 
c  omega        0.15500E+08     211   0.24408E-04   0.27693E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1997e+05                             2
a  Local Time Step      1.0612e-05                         44567


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.582          1.4935      -0.0035451      5.9854e-06
v  Velocity[Y]                 -15.279          34.062          6.7385          20.056
v  Velocity[Z]                 -33.491           28.99        -0.11096       0.0010739
v  ǁVelocityǁ                0.0071362          36.454          10.524          20.216
v  Pressure                    -409.38          350.92         -50.706          31.545
v  k                        4.9362e-08          64.566          3.9667          1.7221
v  omega                         1e-24      1.6563e+07          8084.5          11.867
v  turbulent_viscosity       4.728e-15          1.3077        0.015797         0.11553
v  CourantNb                  0.064636          2243.7          44.453          1.3781
v  FourierNb                  0.010893           15244          93.454         0.71433
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14799        0.010808        0.045665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15316          137.91          2.0924


 TIME FOR THE TIME STEP              883:        0.48793E+02

===============================================================


 INSTANT    0.884000000E+02   TIME STEP NUMBER             884
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.156209833E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32214E+02 0.16860E+02
   Friction velocity        uet   :  0.59989E-03 0.32971E+01
   Friction velocity        uk    :  0.19252E-01 0.31235E+01
   Dimensionless distance   yplus :  0.16579E+00 0.27563E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        436
   Nb of faces within the viscous sub-layer     :       1009
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29409E+04    2011   0.45752E-02   0.46010E+00 
c  VelocityY    0.29409E+04    2011   0.45752E-02   0.00000E+00 
c  VelocityZ    0.29409E+04    2011   0.45752E-02   0.00000E+00 
c  Pressure     0.41894E+00    7048   0.37056E-01   0.19937E+00 
c  k            0.22305E+04    1533   0.75183E-04   0.14843E+01 
c  omega        0.10591E+08     289   0.24279E-03   0.19881E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7379e+05                             2
a  Local Time Step      1.1664e-05                         44585


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6811          1.7143       -0.002327       6.401e-06
v  Velocity[Y]                 -15.191          33.133          6.7856          20.056
v  Velocity[Z]                 -33.553          28.895        -0.11265       0.0018338
v  ǁVelocityǁ                0.0041711          35.829          10.569          20.216
v  Pressure                    -440.01          350.17         -49.224           31.69
v  k                        1.0009e-07          68.856          3.9912          1.7221
v  omega                         1e-24      6.6647e+07          8879.1          11.941
v  turbulent_viscosity      1.2198e-13          1.2996        0.015801         0.11564
v  CourantNb                  0.032698            2778          44.457          1.3778
v  FourierNb                   0.01089           15135          92.019         0.71463
v  total_pressure           1.0088e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1482         0.01081        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15212          136.48          2.0924


 TIME FOR THE TIME STEP              884:        0.47140E+02

===============================================================


 INSTANT    0.885000000E+02   TIME STEP NUMBER             885
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.250338007E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31496E+02 0.17091E+02
   Friction velocity        uet   :  0.99619E-03 0.32849E+01
   Friction velocity        uk    :  0.18371E-01 0.28564E+01
   Dimensionless distance   yplus :  0.11554E+00 0.26994E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        497
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1944   0.47098E-02   0.46080E+00 
c  VelocityY    0.29408E+04    1944   0.47098E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1944   0.47098E-02   0.00000E+00 
c  Pressure     0.44615E+00    7031   0.37130E-01   0.21172E+00 
c  k            0.22346E+04    1463   0.75978E-04   0.15513E+01 
c  omega        0.28651E+08     153   0.43841E-04   0.93010E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3471e+05                             2
a  Local Time Step      1.1461e-05                         44598


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5933          1.8453     -0.00058684      7.7718e-06
v  Velocity[Y]                 -23.831          30.174          6.8015          20.056
v  Velocity[Z]                 -32.286          28.856       -0.085928       0.0026622
v  ǁVelocityǁ                0.0064668          33.486          10.594          20.217
v  Pressure                    -446.34          348.13         -48.968          31.618
v  k                        1.8902e-07           62.78          4.0147          1.7217
v  omega                         1e-24      3.4101e+07          8714.1          11.953
v  turbulent_viscosity      1.0092e-14          1.2916        0.015815         0.11571
v  CourantNb                  0.032593          2884.5          44.508          1.3775
v  FourierNb                  0.010887           15038          91.072         0.71519
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14818        0.010812         0.04569


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0024           15084          135.58          2.0927


 TIME FOR THE TIME STEP              885:        0.45801E+02

===============================================================


 INSTANT    0.886000000E+02   TIME STEP NUMBER             886
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.645672271E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30684E+02 0.14915E+02
   Friction velocity        uet   :  0.18900E-03 0.28414E+01
   Friction velocity        uk    :  0.65949E-02 0.28931E+01
   Dimensionless distance   yplus :  0.86925E-01 0.27677E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :       1063
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1870   0.45070E-02   0.43437E+00 
c  VelocityY    0.29408E+04    1870   0.45070E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1870   0.45070E-02   0.00000E+00 
c  Pressure     0.44421E+00    7062   0.33569E-01   0.21141E+00 
c  k            0.22382E+04    1285   0.76456E-04   0.15998E+01 
c  omega        0.13115E+08     226   0.87302E-04   0.12786E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8474e+05                             2
a  Local Time Step      1.1469e-05                         44601


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3177          1.8216      6.8531e-05      6.2872e-06
v  Velocity[Y]                 -28.003          30.033          6.7509          20.057
v  Velocity[Z]                 -32.144           28.82       -0.056177       0.0033168
v  ǁVelocityǁ                0.0059058          33.219          10.594          20.217
v  Pressure                    -433.43          348.22         -49.284           31.49
v  k                        1.7033e-08          48.291          4.0584          1.7207
v  omega                         1e-24      4.8695e+07          8671.7           11.94
v  turbulent_viscosity      8.5026e-14          1.2835         0.01583         0.11576
v  CourantNb                  0.012972            2399          44.545          1.3773
v  FourierNb                  0.010885           14980          91.324         0.71601
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010815        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9713           15023          135.87          2.0934


 TIME FOR THE TIME STEP              886:        0.46376E+02

===============================================================


 INSTANT    0.887000000E+02   TIME STEP NUMBER             887
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.949591969E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31466E+02 0.17894E+02
   Friction velocity        uet   :  0.42977E-03 0.27991E+01
   Friction velocity        uk    :  0.13814E-01 0.29268E+01
   Dimensionless distance   yplus :  0.16325E+00 0.28092E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1039
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1913   0.44033E-02   0.41146E+00 
c  VelocityY    0.29407E+04    1913   0.44033E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1913   0.44033E-02   0.00000E+00 
c  Pressure     0.42788E+00    7093   0.31322E-01   0.20391E+00 
c  k            0.22372E+04    1087   0.92323E-04   0.15745E+01 
c  omega        0.22275E+08     211   0.72443E-04   0.10684E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8449e+05                             2
a  Local Time Step       1.132e-05                         44603


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0708          1.6196      3.1148e-05      4.8251e-06
v  Velocity[Y]                 -35.601          29.915          6.6543          20.055
v  Velocity[Z]                  -30.13          28.642       -0.035975       0.0038095
v  ǁVelocityǁ                0.0085452          35.892          10.628          20.216
v  Pressure                    -408.73          348.46         -50.684          31.082
v  k                        7.3422e-09           87.18          4.1583          1.7193
v  omega                         1e-24      6.9201e+07          8544.7          11.916
v  turbulent_viscosity      8.4448e-14          1.2752         0.01587         0.11578
v  CourantNb                  0.021231          2033.3          44.344          1.3772
v  FourierNb                  0.010882           14915          93.235         0.71758
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010817        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.75641           14961          137.58          2.0947


 TIME FOR THE TIME STEP              887:        0.45991E+02

===============================================================


 INSTANT    0.888000000E+02   TIME STEP NUMBER             888
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.474252267E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31041E+02 0.24387E+02
   Friction velocity        uet   :  0.11082E-02 0.29708E+01
   Friction velocity        uk    :  0.16261E-01 0.32037E+01
   Dimensionless distance   yplus :  0.17537E+00 0.32387E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :       1061
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    2006   0.46024E-02   0.41155E+00 
c  VelocityY    0.29406E+04    2006   0.46024E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    2006   0.46024E-02   0.00000E+00 
c  Pressure     0.41400E+00    7033   0.34150E-01   0.19602E+00 
c  k            0.22285E+04    1353   0.12960E-03   0.14706E+01 
c  omega        0.22255E+08     381   0.46891E-04   0.41428E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6562e+05                             2
a  Local Time Step      1.0916e-05                         44557


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93538           1.356      0.00024301      1.6924e-06
v  Velocity[Y]                 -37.087          30.136          6.6079          20.055
v  Velocity[Z]                 -28.555          28.685       0.0053585       0.0043317
v  ǁVelocityǁ                0.0048593          38.923          10.668          20.216
v  Pressure                     -411.7          347.81         -53.269          31.076
v  k                        6.3679e-09          109.62           4.273          1.7177
v  omega                         1e-24      3.5452e+07          8398.9          11.933
v  turbulent_viscosity      3.0768e-14          1.2671        0.015929         0.11577
v  CourantNb                  0.021544          2038.5          44.169          1.3772
v  FourierNb                  0.010879           14949          95.634         0.71978
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14831        0.010818        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.76943           15001           139.8           2.097


 TIME FOR THE TIME STEP              888:        0.46731E+02

===============================================================


 INSTANT    0.889000000E+02   TIME STEP NUMBER             889
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.651154552E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.52155E+02 0.14306E+02
   Friction velocity        uet   :  0.22901E-02 0.34394E+01
   Friction velocity        uk    :  0.21810E-01 0.51335E+01
   Dimensionless distance   yplus :  0.15546E+00 0.42416E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :       1008
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1945   0.44613E-02   0.41991E+00 
c  VelocityY    0.29406E+04    1945   0.44613E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1945   0.44613E-02   0.00000E+00 
c  Pressure     0.43266E+00    7129   0.37969E-01   0.20434E+00 
c  k            0.22153E+04    1441   0.13346E-03   0.13697E+01 
c  omega        0.17191E+08     436   0.38849E-04   0.19351E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6232e+05                             2
a  Local Time Step      1.1634e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86335          1.1283      0.00087511     -2.4631e-06
v  Velocity[Y]                 -28.472          30.551          6.6269          20.056
v  Velocity[Z]                 -28.537          28.663        0.056753       0.0046961
v  ǁVelocityǁ                0.0076692          33.578          10.688          20.217
v  Pressure                    -410.71          347.01         -56.073           31.47
v  k                        1.0443e-08          53.218          4.2761          1.7157
v  omega                         1e-24      1.9465e+07          8171.1          11.907
v  turbulent_viscosity      4.3624e-15          1.2592        0.015944         0.11573
v  CourantNb                  0.040832          2247.6          44.144          1.3774
v  FourierNb                  0.010876           18979          96.352         0.72078
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14764        0.010816        0.045658


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89314           19131           140.5          2.0982


 TIME FOR THE TIME STEP              889:        0.46876E+02

===============================================================


 INSTANT    0.890000000E+02   TIME STEP NUMBER             890
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.103939876E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31028E+02 0.14259E+02
   Friction velocity        uet   :  0.40948E-03 0.27932E+01
   Friction velocity        uk    :  0.31422E-01 0.29777E+01
   Dimensionless distance   yplus :  0.83787E-01 0.27764E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        453
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29405E+04    1992   0.44737E-02   0.41677E+00 
c  VelocityY    0.29405E+04    1992   0.44737E-02   0.00000E+00 
c  VelocityZ    0.29405E+04    1992   0.44737E-02   0.00000E+00 
c  Pressure     0.42111E+00    7105   0.37419E-01   0.19850E+00 
c  k            0.22024E+04    1480   0.80023E-04   0.12606E+01 
c  omega        0.11921E+08     315   0.36291E-04   0.18656E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0677e+05                             2
a  Local Time Step      1.1556e-05                         44530


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95743          1.0096      0.00053046     -5.3486e-06
v  Velocity[Y]                 -17.959          30.746          6.6694          20.056
v  Velocity[Z]                 -28.651          29.026         0.10004       0.0047257
v  ǁVelocityǁ                 0.018708          33.497          10.674          20.217
v  Pressure                    -408.76          346.01         -57.762          31.674
v  k                        1.2408e-08          50.681           4.269          1.7136
v  omega                         1e-24      1.4158e+07            8035           11.89
v  turbulent_viscosity      1.1582e-14          1.2513        0.015944         0.11567
v  CourantNb                   0.04279          2933.5          44.433          1.3777
v  FourierNb                  0.010873           15106          96.828         0.72101
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14724        0.010817        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15173          141.26          2.0987


 TIME FOR THE TIME STEP              890:        0.47954E+02

===============================================================


 INSTANT    0.891000000E+02   TIME STEP NUMBER             891
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.114064269E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30020E+02 0.14111E+02
   Friction velocity        uet   :  0.16995E-02 0.27666E+01
   Friction velocity        uk    :  0.31548E-01 0.29176E+01
   Dimensionless distance   yplus :  0.17851E+00 0.27953E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1035
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    2098   0.43180E-02   0.42061E+00 
c  VelocityY    0.29404E+04    2098   0.43180E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    2098   0.43180E-02   0.00000E+00 
c  Pressure     0.42981E+00    7092   0.34295E-01   0.20406E+00 
c  k            0.21917E+04    1468   0.80189E-04   0.12478E+01 
c  omega        0.10631E+08     402   0.29933E-04   0.13271E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3251e+05                             2
a  Local Time Step      1.1522e-05                         44515


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92842         0.93471      -0.0016378     -6.8904e-06
v  Velocity[Y]                 -17.072           32.08          6.7131          20.056
v  Velocity[Z]                 -28.928          28.829         0.12643       0.0048937
v  ǁVelocityǁ                 0.015335          33.577          10.634          20.217
v  Pressure                    -406.39          345.12         -57.692          31.912
v  k                        4.4829e-09          56.069          4.2427          1.7113
v  omega                         1e-24      1.1736e+07          7936.9           11.88
v  turbulent_viscosity       3.102e-15          1.2434        0.015927         0.11558
v  CourantNb                  0.038919          2082.8          44.462          1.3779
v  FourierNb                   0.01087           15136          98.195         0.72093
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14842        0.010817        0.045704


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15211          142.66          2.0989


 TIME FOR THE TIME STEP              891:        0.48183E+02

===============================================================


 INSTANT    0.892000000E+02   TIME STEP NUMBER             892
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240346261E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31760E+02 0.13782E+02
   Friction velocity        uet   :  0.91416E-03 0.28425E+01
   Friction velocity        uk    :  0.25889E-01 0.30655E+01
   Dimensionless distance   yplus :  0.13976E+00 0.31662E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2048   0.44411E-02   0.43357E+00 
c  VelocityY    0.29402E+04    2048   0.44411E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2048   0.44411E-02   0.00000E+00 
c  Pressure     0.42078E+00    7061   0.31688E-01   0.19968E+00 
c  k            0.21817E+04    1346   0.77507E-04   0.13521E+01 
c  omega        0.10233E+08     470   0.24751E-03   0.20949E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9548e+05                             2
a  Local Time Step      1.1124e-05                         44468


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92552         0.87503      -0.0043655     -7.7666e-06
v  Velocity[Y]                 -15.223          32.534          6.7371          20.057
v  Velocity[Z]                 -29.352          29.188         0.12401       0.0047576
v  ǁVelocityǁ                 0.010862          33.608          10.581          20.217
v  Pressure                    -397.61           345.4         -56.942           31.88
v  k                        1.5443e-08          51.563          4.1404          1.7089
v  omega                         1e-24      8.9606e+07          8472.7          11.883
v  turbulent_viscosity      9.4826e-15          1.2358        0.015878         0.11547
v  CourantNb                  0.039525          2025.4          44.382          1.3781
v  FourierNb                  0.010868           15172          99.256         0.72049
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14768        0.010818        0.045741


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15212          143.64          2.0986


 TIME FOR THE TIME STEP              892:        0.47287E+02

===============================================================


 INSTANT    0.893000000E+02   TIME STEP NUMBER             893
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.145735162E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31689E+02 0.15093E+02
   Friction velocity        uet   :  0.24975E-02 0.27504E+01
   Friction velocity        uk    :  0.18962E-01 0.32794E+01
   Dimensionless distance   yplus :  0.41392E-01 0.33651E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    2080   0.45038E-02   0.44255E+00 
c  VelocityY    0.29400E+04    2080   0.45038E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    2080   0.45038E-02   0.00000E+00 
c  Pressure     0.44049E+00    7084   0.31739E-01   0.20958E+00 
c  k            0.21705E+04     942   0.73872E-04   0.12909E+01 
c  omega        0.41848E+08     208   0.29464E-04   0.96188E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.5842e+05                             1
a  Local Time Step       1.164e-05                         44462


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97902         0.82562      -0.0072883     -7.8161e-06
v  Velocity[Y]                 -16.304          33.139          6.7251          20.057
v  Velocity[Z]                 -29.071          29.161        0.099023       0.0045825
v  ǁVelocityǁ                 0.008226          33.445          10.552          20.217
v  Pressure                     -377.3          346.82         -55.748          31.552
v  k                        1.2506e-07          44.711          4.0351          1.7065
v  omega                         1e-24      4.5526e+07          8379.7          11.871
v  turbulent_viscosity      2.4374e-14          1.2282        0.015796         0.11534
v  CourantNb                  0.032782          2049.9          44.379          1.3782
v  FourierNb                  0.010866           15329          97.838         0.71885
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010819        0.045745


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15377          142.22          2.0971


 TIME FOR THE TIME STEP              893:        0.45808E+02

===============================================================


 INSTANT    0.894000000E+02   TIME STEP NUMBER             894
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.351336726E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31425E+02 0.22316E+02
   Friction velocity        uet   :  0.17010E-02 0.26895E+01
   Friction velocity        uk    :  0.11110E-01 0.35029E+01
   Dimensionless distance   yplus :  0.13899E+00 0.37572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        439
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    2005   0.44224E-02   0.45456E+00 
c  VelocityY    0.29398E+04    2005   0.44224E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    2005   0.44224E-02   0.00000E+00 
c  Pressure     0.43299E+00    7030   0.29061E-01   0.20592E+00 
c  k            0.21613E+04    1331   0.70316E-04   0.13020E+01 
c  omega        0.16607E+08     241   0.82795E-03   0.35258E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3299e+05                             1
a  Local Time Step      1.1851e-05                         44471


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0427         0.83143      -0.0092721     -6.3839e-06
v  Velocity[Y]                 -15.312          30.854          6.7222          20.056
v  Velocity[Z]                 -29.414          29.264        0.075965        0.003928
v  ǁVelocityǁ                 0.012423          32.883          10.526          20.216
v  Pressure                    -360.39          348.82         -53.428          31.656
v  k                        6.8603e-08          45.278          3.9515          1.7043
v  omega                         1e-24      4.3065e+08           11316            12.1
v  turbulent_viscosity      2.7556e-13          1.2219        0.015722          0.1152
v  CourantNb                  0.044098          2068.3          44.598          1.3786
v  FourierNb                  0.010865           15403          95.892         0.71701
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14891         0.01082        0.045766


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15463          140.49          2.0956


 TIME FOR THE TIME STEP              894:        0.45381E+02

===============================================================


 INSTANT    0.895000000E+02   TIME STEP NUMBER             895
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.416941811E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31796E+02 0.20570E+02
   Friction velocity        uet   :  0.96918E-03 0.26192E+01
   Friction velocity        uk    :  0.15948E-01 0.30178E+01
   Dimensionless distance   yplus :  0.10460E+00 0.30519E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :        995
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2023   0.45201E-02   0.45860E+00 
c  VelocityY    0.29397E+04    2023   0.45201E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2023   0.45201E-02   0.00000E+00 
c  Pressure     0.43678E+00    7042   0.27405E-01   0.20690E+00 
c  k            0.21548E+04    1487   0.67456E-04   0.14035E+01 
c  omega        0.12426E+15       2   0.37769E-10   0.97214E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1435e+05                             1
a  Local Time Step      1.1407e-05                         44510


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0803         0.89719      -0.0099255     -4.6854e-06
v  Velocity[Y]                 -15.244          30.308          6.7397          20.056
v  Velocity[Z]                 -31.247          29.077        0.053337       0.0034994
v  ǁVelocityǁ                0.0090466          36.328           10.52          20.216
v  Pressure                    -351.14          350.67         -50.568          31.963
v  k                        9.1987e-08            46.6          3.9067          1.7021
v  omega                         1e-24      2.1545e+08          9646.4          11.984
v  turbulent_viscosity      1.7501e-13          1.2201        0.015684         0.11504
v  CourantNb                 0.0025579          2076.5          44.957          1.3788
v  FourierNb                  0.010863           15404          94.246         0.71547
v  total_pressure           1.0097e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14884         0.01082        0.045763


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15475           139.2          2.0942


 TIME FOR THE TIME STEP              895:        0.45688E+02

===============================================================


 INSTANT    0.896000000E+02   TIME STEP NUMBER             896
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.314389017E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31783E+02 0.18536E+02
   Friction velocity        uet   :  0.16268E-02 0.30402E+01
   Friction velocity        uk    :  0.14706E-01 0.32144E+01
   Dimensionless distance   yplus :  0.17649E+00 0.27763E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        475
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1993   0.45351E-02   0.45487E+00 
c  VelocityY    0.29397E+04    1993   0.45351E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1993   0.45351E-02   0.00000E+00 
c  Pressure     0.46112E+00    6988   0.31168E-01   0.21934E+00 
c  k            0.21551E+04    1566   0.72203E-04   0.15946E+01 
c  omega        0.18847E+09      98   0.21226E-04   0.67796E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1381e+05                             2
a  Local Time Step      1.2151e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1071         0.92498      -0.0095407     -6.1778e-06
v  Velocity[Y]                 -15.387          30.215          6.7749          20.056
v  Velocity[Z]                 -31.654          29.369        0.042137       0.0028263
v  ǁVelocityǁ                0.0092745          36.219          10.551          20.217
v  Pressure                    -385.36          351.34         -47.685          32.533
v  k                        4.0493e-09          56.474          3.9098          1.7003
v  omega                         1e-24      1.3064e+08          9502.5          11.998
v  turbulent_viscosity      2.2941e-14          1.2198         0.01569         0.11485
v  CourantNb                 0.0057349          2075.3          45.009          1.3785
v  FourierNb                   0.01086           15231          91.831         0.71368
v  total_pressure           1.0094e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14825         0.01082        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15285          136.84          2.0922


 TIME FOR THE TIME STEP              896:        0.46915E+02

===============================================================


 INSTANT    0.897000000E+02   TIME STEP NUMBER             897
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.155153093E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32231E+02 0.14263E+02
   Friction velocity        uet   :  0.14632E-02 0.30854E+01
   Friction velocity        uk    :  0.12475E-01 0.30003E+01
   Dimensionless distance   yplus :  0.10252E+00 0.27011E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        519
   Nb of faces within the viscous sub-layer     :       1047
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1971   0.43994E-02   0.45714E+00 
c  VelocityY    0.29398E+04    1971   0.43994E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1971   0.43994E-02   0.00000E+00 
c  Pressure     0.44477E+00    7072   0.35930E-01   0.21084E+00 
c  k            0.21626E+04    1469   0.74790E-04   0.16663E+01 
c  omega        0.12250E+09     108   0.14608E-04   0.18607E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k                   -0.00046304                             2
a  omega                -1.007e+05                             1
a  Local Time Step      1.1931e-05                         44502


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0619         0.91144      -0.0087624     -8.2808e-06
v  Velocity[Y]                 -15.305          32.155           6.821          20.056
v  Velocity[Z]                 -32.273          28.982        0.058514       0.0017751
v  ǁVelocityǁ                 0.015161          34.958          10.602          20.217
v  Pressure                    -418.61          350.53         -45.697          32.704
v  k                        5.4534e-08          64.995          3.9249          1.6985
v  omega                         1e-24      6.5305e+07          8682.1          11.909
v  turbulent_viscosity      1.8998e-15          1.2191        0.015743         0.11468
v  CourantNb                  0.046293          2530.4           44.93          1.3782
v  FourierNb                  0.010859           15418          90.166         0.71268
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010819        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15465           135.1          2.0909


 TIME FOR THE TIME STEP              897:        0.46551E+02

===============================================================


 INSTANT    0.898000000E+02   TIME STEP NUMBER             898
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.111142899E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30368E+02 0.13882E+02
   Friction velocity        uet   :  0.11552E-02 0.31544E+01
   Friction velocity        uk    :  0.17352E-01 0.29118E+01
   Dimensionless distance   yplus :  0.11525E+00 0.27597E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        492
   Nb of faces within the viscous sub-layer     :       1090
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1932   0.44940E-02   0.45867E+00 
c  VelocityY    0.29399E+04    1932   0.44940E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1932   0.44940E-02   0.00000E+00 
c  Pressure     0.42303E+00    7133   0.38464E-01   0.20113E+00 
c  k            0.21753E+04    1303   0.76830E-04   0.17080E+01 
c  omega        0.32606E+08     151   0.84028E-04   0.23673E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8327e+05                             2
a  Local Time Step      1.2033e-05                         44495


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0249         0.85571      -0.0078183     -6.0756e-06
v  Velocity[Y]                 -20.879          29.893          6.8512          20.056
v  Velocity[Z]                 -32.682          28.935        0.093284      0.00091165
v  ǁVelocityǁ                0.0060754          34.095          10.632          20.218
v  Pressure                    -428.33          349.82         -44.984          32.703
v  k                          1.96e-07           62.49          3.9496          1.6967
v  omega                         1e-24       7.951e+07          8948.5          11.939
v  turbulent_viscosity      1.1785e-15          1.2398         0.01579         0.11449
v  CourantNb                  0.031835            2767          44.812          1.3779
v  FourierNb                  0.010857           15463          89.705         0.71189
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14929         0.01082        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15508          134.52          2.0898


 TIME FOR THE TIME STEP              898:        0.45097E+02

===============================================================


 INSTANT    0.899000000E+02   TIME STEP NUMBER             899
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.114128855E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29573E+02 0.13640E+02
   Friction velocity        uet   :  0.16995E-03 0.29097E+01
   Friction velocity        uk    :  0.20894E-01 0.29184E+01
   Dimensionless distance   yplus :  0.10727E+00 0.27783E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1918   0.44881E-02   0.42290E+00 
c  VelocityY    0.29399E+04    1918   0.44881E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1918   0.44881E-02   0.00000E+00 
c  Pressure     0.45532E+00    7116   0.37138E-01   0.21538E+00 
c  k            0.21877E+04    1020   0.77417E-04   0.17473E+01 
c  omega        0.36750E+08     128   0.93708E-04   0.32243E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -48907                             2
a  Local Time Step      1.1253e-05                         44475


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97159         0.76106      -0.0063362     -3.2523e-06
v  Velocity[Y]                 -24.168          29.712          6.8117          20.056
v  Velocity[Z]                 -32.746          28.689           0.146      0.00021449
v  ǁVelocityǁ                0.0094381          33.409          10.605          20.218
v  Pressure                    -419.78          350.69         -45.095          32.679
v  k                        3.4909e-08          50.202          3.9753          1.6946
v  omega                         1e-24      8.4125e+07          9281.4          11.943
v  turbulent_viscosity       8.139e-15          1.2596        0.015821         0.11431
v  CourantNb                  0.031533          2426.5          44.759          1.3779
v  FourierNb                  0.010856           15365          90.173         0.71089
v  total_pressure           1.0091e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14896         0.01082        0.045665


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15413          134.93          2.0888


 TIME FOR THE TIME STEP              899:        0.44672E+02

===============================================================


 INSTANT    0.900000000E+02   TIME STEP NUMBER             900
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.113415139E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31237E+02 0.14788E+02
   Friction velocity        uet   :  0.70760E-03 0.28561E+01
   Friction velocity        uk    :  0.24565E-01 0.31284E+01
   Dimensionless distance   yplus :  0.11884E+00 0.27821E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2018   0.45611E-02   0.37856E+00 
c  VelocityY    0.29399E+04    2018   0.45611E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2018   0.45611E-02   0.00000E+00 
c  Pressure     0.43477E+00    7012   0.33740E-01   0.20663E+00 
c  k            0.21956E+04    1243   0.86240E-04   0.17259E+01 
c  omega        0.44850E+08     132   0.38287E-04   0.11564E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3051e+05                             2
a  Local Time Step      1.1454e-05                         44447


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98416          0.6386      -0.0053741     -1.9237e-06
v  Velocity[Y]                 -32.139          29.539          6.7077          20.056
v  Velocity[Z]                 -29.565          28.494         0.16453     -0.00063787
v  ǁVelocityǁ                 0.010195           32.88            10.6          20.218
v  Pressure                    -397.15          350.55         -45.954          32.483
v  k                        1.3819e-07          70.539          4.0339          1.6925
v  omega                         1e-24      4.2633e+07          8832.1          11.926
v  turbulent_viscosity      9.2232e-14          1.2749        0.015849         0.11412
v  CourantNb                 0.0079678          2032.1          44.387          1.3777
v  FourierNb                  0.010855           15248           91.27         0.71014
v  total_pressure           1.0093e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14855        0.010821        0.045685


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15303          135.66          2.0878


 TIME FOR THE TIME STEP              900:        0.46320E+02

===============================================================


 INSTANT    0.901000000E+02   TIME STEP NUMBER             901
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.216205325E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31179E+02 0.21968E+02
   Friction velocity        uet   :  0.13361E-02 0.28645E+01
   Friction velocity        uk    :  0.30277E-01 0.28073E+01
   Dimensionless distance   yplus :  0.10134E+00 0.27746E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        392
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2023   0.47032E-02   0.35191E+00 
c  VelocityY    0.29399E+04    2023   0.47032E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2023   0.47032E-02   0.00000E+00 
c  Pressure     0.42343E+00    7037   0.33240E-01   0.20145E+00 
c  k            0.21954E+04    1418   0.10685E-03   0.16246E+01 
c  omega        0.16063E+08     356   0.51743E-04   0.45186E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -51058                             1
a  Local Time Step      1.1212e-05                         44432


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0692         0.70949      -0.0046176     -3.7161e-06
v  Velocity[Y]                 -31.357           29.73          6.6277          20.056
v  Velocity[Z]                 -28.684          28.562         0.18159      -0.0015564
v  ǁVelocityǁ                  0.01463          38.249          10.612          20.218
v  Pressure                    -396.64          349.14         -47.832          32.352
v  k                        2.2257e-08          95.035          4.1235          1.6904
v  omega                         1e-24      2.2474e+07          8523.6          11.928
v  turbulent_viscosity      3.4632e-14           1.286        0.015875         0.11394
v  CourantNb                   0.05331          2024.3          44.222          1.3776
v  FourierNb                  0.010854           15167          92.651         0.70983
v  total_pressure           1.0093e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14822         0.01082        0.045696


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9172           15231          136.87          2.0875


 TIME FOR THE TIME STEP              901:        0.47410E+02

===============================================================


 INSTANT    0.902000000E+02   TIME STEP NUMBER             902
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.782974426E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.57141E+02 0.13955E+02
   Friction velocity        uet   :  0.20937E-02 0.33075E+01
   Friction velocity        uk    :  0.26663E-01 0.41786E+01
   Dimensionless distance   yplus :  0.16523E+00 0.34086E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        457
   Nb of faces within the viscous sub-layer     :       1023
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2038   0.44205E-02   0.33934E+00 
c  VelocityY    0.29399E+04    2038   0.44205E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2038   0.44205E-02   0.00000E+00 
c  Pressure     0.45194E+00    6999   0.36149E-01   0.21428E+00 
c  k            0.21899E+04    1464   0.11541E-03   0.14791E+01 
c  omega        0.10846E+08     463   0.47655E-04   0.18716E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0404e+05                             2
a  Local Time Step      1.1015e-05                         44427


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2875         0.62966      -0.0035907     -1.8415e-07
v  Velocity[Y]                 -32.488          30.045           6.603          20.057
v  Velocity[Z]                 -28.769          28.512         0.19182      -0.0025285
v  ǁVelocityǁ                 0.012447          33.691          10.614          20.219
v  Pressure                    -399.91          346.95         -50.269          32.394
v  k                        3.4917e-10          58.445          4.1627          1.6884
v  omega                         1e-24      1.3528e+07          8256.8          11.898
v  turbulent_viscosity      8.8115e-15           1.299        0.015913         0.11376
v  CourantNb                  0.020638          2020.4          44.195          1.3777
v  FourierNb                  0.010853           15159           94.31         0.70975
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010819        0.045702


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15230          138.51          2.0875


 TIME FOR THE TIME STEP              902:        0.47254E+02

===============================================================


 INSTANT    0.903000000E+02   TIME STEP NUMBER             903
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.566487380E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31046E+02 0.13575E+02
   Friction velocity        uet   :  0.20157E-02 0.31507E+01
   Friction velocity        uk    :  0.20582E-01 0.31896E+01
   Dimensionless distance   yplus :  0.16094E+00 0.27267E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1976   0.45061E-02   0.32378E+00 
c  VelocityY    0.29398E+04    1976   0.45061E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1976   0.45061E-02   0.00000E+00 
c  Pressure     0.42279E+00    7130   0.37365E-01   0.20111E+00 
c  k            0.21841E+04    1487   0.81366E-04   0.13648E+01 
c  omega        0.10141E+08     384   0.60848E-04   0.58825E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5855e+05                             1
a  Local Time Step       1.137e-05                         44376


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5276         0.72355      -0.0022501     -1.3825e-06
v  Velocity[Y]                 -18.204          30.865          6.6105          20.057
v  Velocity[Z]                 -28.927          28.386         0.19257      -0.0035705
v  ǁVelocityǁ                 0.021827          33.269          10.593           20.22
v  Pressure                    -402.07          344.73         -52.323          32.306
v  k                        1.2682e-11          49.894           4.179          1.6865
v  omega                         1e-24      3.4064e+07          8229.5          11.892
v  turbulent_viscosity      4.0757e-16          1.3086        0.015944         0.11359
v  CourantNb                  0.045069          3141.5          44.428          1.3778
v  FourierNb                  0.010852           15192          95.081         0.70899
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14774        0.010819        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15268          139.51          2.0868


 TIME FOR THE TIME STEP              903:        0.46645E+02

===============================================================


 INSTANT    0.904000000E+02   TIME STEP NUMBER             904
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.408537986E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30256E+02 0.13167E+02
   Friction velocity        uet   :  0.19894E-02 0.28946E+01
   Friction velocity        uk    :  0.34208E-01 0.29528E+01
   Dimensionless distance   yplus :  0.15594E+00 0.27992E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        430
   Nb of faces within the viscous sub-layer     :       1041
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29398E+04    1995   0.43341E-02   0.31950E+00 
c  VelocityY    0.29398E+04    1995   0.43341E-02   0.00000E+00 
c  VelocityZ    0.29398E+04    1995   0.43341E-02   0.00000E+00 
c  Pressure     0.42679E+00    7104   0.34561E-01   0.20208E+00 
c  k            0.21799E+04    1461   0.73668E-04   0.12679E+01 
c  omega        0.19578E+08     210   0.25221E-04   0.38716E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step       1.115e-05                         44328


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7652         0.79021     -0.00089659     -2.9614e-06
v  Velocity[Y]                 -17.376           33.01          6.6471          20.057
v  Velocity[Z]                 -29.219          28.712         0.17021      -0.0048661
v  ǁVelocityǁ                 0.021917          33.773           10.55           20.22
v  Pressure                    -401.87          344.83         -53.309          32.349
v  k                        3.0544e-09          51.158           4.185          1.6848
v  omega                         1e-24      1.7027e+07          8138.9          11.892
v  turbulent_viscosity      1.2677e-17           1.319         0.01595         0.11342
v  CourantNb                  0.054546          2343.7           44.24          1.3778
v  FourierNb                  0.010852           15197          95.526         0.70778
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14868        0.010819         0.04574


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15276          139.77          2.0856


 TIME FOR THE TIME STEP              904:        0.46713E+02

===============================================================


 INSTANT    0.905000000E+02   TIME STEP NUMBER             905
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.654264130E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31255E+02 0.12836E+02
   Friction velocity        uet   :  0.18283E-02 0.29352E+01
   Friction velocity        uk    :  0.24142E-01 0.29696E+01
   Dimensionless distance   yplus :  0.10154E+00 0.29734E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        433
   Nb of faces within the viscous sub-layer     :       1028
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2044   0.46000E-02   0.32976E+00 
c  VelocityY    0.29397E+04    2044   0.46000E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2044   0.46000E-02   0.00000E+00 
c  Pressure     0.42970E+00    7033   0.33479E-01   0.20238E+00 
c  k            0.21767E+04    1394   0.77536E-04   0.13595E+01 
c  omega        0.11805E+08     362   0.35408E-04   0.58451E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -58716                             1
a  Local Time Step      1.1342e-05                         44354


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7031           0.827      0.00010785     -3.7481e-06
v  Velocity[Y]                 -16.166          33.776           6.697          20.056
v  Velocity[Z]                 -29.565          28.892          0.1278      -0.0057214
v  ǁVelocityǁ                  0.01262          33.788          10.511          20.219
v  Pressure                    -396.57          345.49         -53.734          31.959
v  k                        1.7351e-07          52.499          4.1384          1.6832
v  omega                         1e-24      1.8392e+07          8004.3          11.886
v  turbulent_viscosity      5.8816e-15          1.3267        0.015954         0.11326
v  CourantNb                  0.015154          2019.9          43.898          1.3778
v  FourierNb                  0.010851           15370           96.14         0.70672
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14865        0.010818        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15415          140.04          2.0845


 TIME FOR THE TIME STEP              905:        0.46688E+02

===============================================================


 INSTANT    0.906000000E+02   TIME STEP NUMBER             906
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.215183757E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31518E+02 0.14215E+02
   Friction velocity        uet   :  0.21973E-02 0.28788E+01
   Friction velocity        uk    :  0.17353E-01 0.29158E+01
   Dimensionless distance   yplus :  0.10658E+00 0.34461E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        406
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2036   0.46134E-02   0.35198E+00 
c  VelocityY    0.29396E+04    2036   0.46134E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2036   0.46134E-02   0.00000E+00 
c  Pressure     0.42323E+00    7046   0.31358E-01   0.19965E+00 
c  k            0.21739E+04    1351   0.76455E-04   0.13455E+01 
c  omega        0.13590E+08     378   0.30613E-03   0.45568E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3089e+05                             2
a  Local Time Step      1.1047e-05                         44393


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6492         0.83746       0.0009822      -2.508e-06
v  Velocity[Y]                 -15.351           33.39          6.7263          20.056
v  Velocity[Z]                 -28.839          28.874        0.064557      -0.0064891
v  ǁVelocityǁ                 0.021794          33.893          10.492          20.219
v  Pressure                    -379.29          345.57         -53.798          31.693
v  k                        6.6662e-08          42.844          4.0585          1.6819
v  omega                         1e-24      1.3944e+08          9071.2          11.979
v  turbulent_viscosity      9.6202e-14          1.3305        0.015945         0.11311
v  CourantNb                  0.043538          2027.9          43.824          1.3777
v  FourierNb                  0.010851           15609          96.947         0.70564
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14877        0.010817        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15664          140.77          2.0834


 TIME FOR THE TIME STEP              906:        0.47238E+02

===============================================================


 INSTANT    0.907000000E+02   TIME STEP NUMBER             907
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.193006085E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31381E+02 0.23158E+02
   Friction velocity        uet   :  0.55382E-03 0.27577E+01
   Friction velocity        uk    :  0.20216E-01 0.31644E+01
   Dimensionless distance   yplus :  0.17596E+00 0.36419E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :       1015
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2057   0.46048E-02   0.35812E+00 
c  VelocityY    0.29396E+04    2057   0.46048E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2057   0.46048E-02   0.00000E+00 
c  Pressure     0.44852E+00    7020   0.29089E-01   0.21168E+00 
c  k            0.21715E+04    1414   0.67057E-04   0.13208E+01 
c  omega        0.85161E+08     168   0.19897E-04   0.13597E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9921e+05                             3
a  Local Time Step       1.122e-05                         44433


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7756          0.9062       0.0018299     -1.6485e-06
v  Velocity[Y]                  -15.21          32.184           6.719          20.056
v  Velocity[Z]                 -28.578          29.011        0.011663      -0.0072036
v  ǁVelocityǁ                  0.01158          32.794          10.472          20.219
v  Pressure                     -365.8          345.56         -53.071          31.404
v  k                        1.2412e-09          42.049          4.0011           1.681
v  omega                         1e-24      7.0145e+07          8597.4          11.946
v  turbulent_viscosity      3.1903e-13           1.333        0.015915         0.11297
v  CourantNb                  0.020154          2025.9           43.93           1.378
v  FourierNb                  0.010851           15809          96.107         0.70394
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14919        0.010816        0.045675


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.96352           15875          140.04          2.0819


 TIME FOR THE TIME STEP              907:        0.47177E+02

===============================================================


 INSTANT    0.908000000E+02   TIME STEP NUMBER             908
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.207110971E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31126E+02 0.20808E+02
   Friction velocity        uet   :  0.94939E-03 0.25642E+01
   Friction velocity        uk    :  0.18934E-01 0.31851E+01
   Dimensionless distance   yplus :  0.11380E+00 0.28448E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        443
   Nb of faces within the viscous sub-layer     :       1064
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2003   0.45694E-02   0.37210E+00 
c  VelocityY    0.29394E+04    2003   0.45694E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2003   0.45694E-02   0.00000E+00 
c  Pressure     0.43566E+00    7045   0.26859E-01   0.20651E+00 
c  k            0.21709E+04    1487   0.66913E-04   0.14001E+01 
c  omega        0.24009E+08     163   0.78971E-04   0.76989E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.579e+05                             1
a  Local Time Step      1.1923e-05                         44445


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.851          1.1215       0.0022202     -2.5838e-06
v  Velocity[Y]                 -15.274          30.231          6.7293          20.056
v  Velocity[Z]                 -29.715          29.043       -0.040161      -0.0076828
v  ǁVelocityǁ                 0.011656          35.716          10.462          20.219
v  Pressure                    -349.33           345.8          -51.26          31.295
v  k                        1.6464e-08          45.853          3.9844          1.6805
v  omega                         1e-24      3.3899e+08          9584.9           12.19
v  turbulent_viscosity       2.906e-14          1.3353        0.015908         0.11284
v  CourantNb                  0.026534          2014.2          44.071           1.378
v  FourierNb                  0.010852           15783          94.893         0.70232
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14907        0.010816        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15859          138.96          2.0803


 TIME FOR THE TIME STEP              908:        0.46399E+02

===============================================================


 INSTANT    0.909000000E+02   TIME STEP NUMBER             909
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.747150160E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32035E+02 0.20060E+02
   Friction velocity        uet   :  0.20049E-02 0.29728E+01
   Friction velocity        uk    :  0.21504E-01 0.29153E+01
   Dimensionless distance   yplus :  0.19220E+00 0.28032E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        451
   Nb of faces within the viscous sub-layer     :       1024
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1993   0.45896E-02   0.37930E+00 
c  VelocityY    0.29393E+04    1993   0.45896E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1993   0.45896E-02   0.00000E+00 
c  Pressure     0.45014E+00    7089   0.28944E-01   0.21320E+00 
c  k            0.21728E+04    1475   0.71199E-04   0.15446E+01 
c  omega        0.21979E+10      24   0.41708E-06   0.19439E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1154e+05                             1
a  Local Time Step       1.164e-05                         44446


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8827          1.4252       0.0025777     -6.6461e-08
v  Velocity[Y]                 -15.283          31.723          6.7558          20.056
v  Velocity[Z]                 -31.013          28.911        -0.09442      -0.0079968
v  ǁVelocityǁ                0.0052423          36.336          10.481          20.219
v  Pressure                    -376.33          345.95         -49.172          31.532
v  k                        6.1205e-11          56.524          4.0035          1.6804
v  omega                         1e-24      1.6949e+08          8749.1          12.013
v  turbulent_viscosity      7.9985e-15          1.3333        0.015949         0.11271
v  CourantNb                    0.0371          1995.3          44.245          1.3779
v  FourierNb                  0.010852           15823          93.569         0.70128
v  total_pressure           1.0095e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14861        0.010815        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15868          137.81          2.0792


 TIME FOR THE TIME STEP              909:        0.46368E+02

===============================================================


 INSTANT    0.910000000E+02   TIME STEP NUMBER             910
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.126702563E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31571E+02 0.17499E+02
   Friction velocity        uet   :  0.83584E-03 0.31260E+01
   Friction velocity        uk    :  0.17036E-01 0.30444E+01
   Dimensionless distance   yplus :  0.12961E+00 0.28775E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :       1050
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1955   0.45263E-02   0.39302E+00 
c  VelocityY    0.29392E+04    1955   0.45263E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1955   0.45263E-02   0.00000E+00 
c  Pressure     0.43222E+00    7050   0.33613E-01   0.20414E+00 
c  k            0.21801E+04    1392   0.77435E-04   0.16864E+01 
c  omega        0.54942E+09     112   0.12840E-05   0.60257E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8279e+05                             1
a  Local Time Step      1.0965e-05                         44455


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8927          1.6887       0.0023148      7.0222e-09
v  Velocity[Y]                 -15.292           33.39          6.7946          20.056
v  Velocity[Z]                 -33.435          28.966        -0.12329      -0.0082554
v  ǁVelocityǁ                0.0085294          35.792          10.534           20.22
v  Pressure                    -422.33          347.87         -47.939          31.766
v  k                         2.535e-09          65.938          4.0422          1.6806
v  omega                         1e-24      8.4746e+07          8662.6          11.974
v  turbulent_viscosity      5.9001e-17          1.3347        0.016022         0.11259
v  CourantNb                  0.010561          2395.9          44.237          1.3775
v  FourierNb                  0.010853           16076          92.692         0.70065
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14893        0.010815        0.045705


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16121          136.93          2.0782


 TIME FOR THE TIME STEP              910:        0.46190E+02

===============================================================


 INSTANT    0.911000000E+02   TIME STEP NUMBER             911
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.937407392E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30118E+02 0.15790E+02
   Friction velocity        uet   :  0.30033E-02 0.32413E+01
   Friction velocity        uk    :  0.17286E-01 0.31371E+01
   Dimensionless distance   yplus :  0.11495E+00 0.28838E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1077
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1905   0.44578E-02   0.41145E+00 
c  VelocityY    0.29390E+04    1905   0.44578E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1905   0.44578E-02   0.00000E+00 
c  Pressure     0.43023E+00    7043   0.36276E-01   0.20148E+00 
c  k            0.21930E+04    1363   0.81393E-04   0.17484E+01 
c  omega        0.13867E+09     103   0.19079E-04   0.35369E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5278e+05                             1
a  Local Time Step      1.1449e-05                         44456


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7795          1.7918       0.0013301      2.3368e-07
v  Velocity[Y]                 -18.773          29.976          6.8323          20.056
v  Velocity[Z]                 -33.169          28.948        -0.10489      -0.0081375
v  ǁVelocityǁ                0.0061271           34.94          10.587          20.219
v  Pressure                    -441.41          348.84         -47.807          31.644
v  k                        1.9142e-07          67.694          4.0786          1.6809
v  omega                         1e-24      6.6104e+07          9014.5          11.958
v  turbulent_viscosity       2.624e-15           1.334         0.01606         0.11247
v  CourantNb                  0.029936          2813.5           44.15          1.3771
v  FourierNb                  0.010853           16135          92.273         0.69989
v  total_pressure           1.0088e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01          0.1485        0.010815        0.045738


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.87478           16186          136.42           2.077


 TIME FOR THE TIME STEP              911:        0.45382E+02

===============================================================


 INSTANT    0.912000000E+02   TIME STEP NUMBER             912
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.330995263E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29549E+02 0.15696E+02
   Friction velocity        uet   :  0.33721E-02 0.29960E+01
   Friction velocity        uk    :  0.24690E-01 0.29078E+01
   Dimensionless distance   yplus :  0.15902E+00 0.28801E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1994   0.44028E-02   0.41049E+00 
c  VelocityY    0.29391E+04    1994   0.44028E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1994   0.44028E-02   0.00000E+00 
c  Pressure     0.41426E+00    7022   0.35425E-01   0.19442E+00 
c  k            0.22074E+04    1517   0.80857E-04   0.17767E+01 
c  omega        0.45600E+08     122   0.40422E-03   0.89565E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0965e+05                             3
a  Local Time Step      1.0844e-05                         44486


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7325          1.6108       0.0007142     -4.0363e-07
v  Velocity[Y]                 -23.918          29.813          6.8279          20.055
v  Velocity[Z]                 -32.421          28.645       -0.067141      -0.0078741
v  ǁVelocityǁ                0.0023657          33.365          10.602          20.219
v  Pressure                    -438.84          348.38          -48.72          31.563
v  k                        1.4954e-08          81.489          4.1031          1.6812
v  omega                         1e-24      5.6964e+08           12703          12.161
v  turbulent_viscosity      9.6888e-14          1.3298        0.016085         0.11237
v  CourantNb                  0.022661          2719.4          44.168          1.3768
v  FourierNb                  0.010854           15983          92.555         0.69908
v  total_pressure           1.0089e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14765        0.010816        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.91927           16042          136.72          2.0759


 TIME FOR THE TIME STEP              912:        0.46608E+02

===============================================================


 INSTANT    0.913000000E+02   TIME STEP NUMBER             913
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.459481625E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30800E+02 0.14076E+02
   Friction velocity        uet   :  0.18846E-02 0.28281E+01
   Friction velocity        uk    :  0.12941E-01 0.28903E+01
   Dimensionless distance   yplus :  0.81690E-01 0.28189E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        427
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1949   0.46312E-02   0.39430E+00 
c  VelocityY    0.29391E+04    1949   0.46312E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1949   0.46312E-02   0.00000E+00 
c  Pressure     0.44906E+00    7029   0.31953E-01   0.21067E+00 
c  k            0.22186E+04    1552   0.82052E-04   0.17728E+01 
c  omega        0.16770E+10      60   0.11146E-04   0.11281E+11 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6639e+05                             1
a  Local Time Step      1.0991e-05                         44539


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7284          1.3776       0.0014781     -2.2929e-07
v  Velocity[Y]                 -32.874          29.699          6.7591          20.056
v  Velocity[Z]                 -30.841          28.584       -0.022423      -0.0070662
v  ǁVelocityǁ                 0.015954          33.475          10.605          20.219
v  Pressure                    -419.92          347.39         -50.086          31.402
v  k                        1.6462e-08          75.114          4.1465          1.6813
v  omega                         1e-24      7.9848e+08           13381          12.187
v  turbulent_viscosity      8.8169e-14          1.3236        0.016093         0.11227
v  CourantNb                  0.041837            2067          44.166          1.3767
v  FourierNb                  0.010856           15715          93.378         0.69867
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010816        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15782          137.54          2.0754


 TIME FOR THE TIME STEP              913:        0.45985E+02

===============================================================


 INSTANT    0.914000000E+02   TIME STEP NUMBER             914
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.270169099E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31511E+02 0.22852E+02
   Friction velocity        uet   :  0.12979E-02 0.30124E+01
   Friction velocity        uk    :  0.39014E-01 0.31082E+01
   Dimensionless distance   yplus :  0.15252E+00 0.32886E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1903   0.45563E-02   0.38798E+00 
c  VelocityY    0.29391E+04    1903   0.45563E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1903   0.45563E-02   0.00000E+00 
c  Pressure     0.41871E+00    7053   0.30821E-01   0.19634E+00 
c  k            0.22219E+04    1534   0.10644E-03   0.16709E+01 
c  omega        0.25227E+10      42   0.35869E-05   0.28357E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.759e+05                             2
a  Local Time Step       1.126e-05                         44561


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5545          1.2557       0.0022965      1.7915e-06
v  Velocity[Y]                 -23.572          29.704          6.6703          20.055
v  Velocity[Z]                 -28.736          28.844         0.00974      -0.0063342
v  ǁVelocityǁ                 0.013164          33.038           10.64          20.218
v  Pressure                    -407.37          345.23         -52.317          31.179
v  k                        2.0702e-08          100.87          4.2168          1.6814
v  omega                         1e-24      3.9935e+08           10685          12.021
v  turbulent_viscosity      1.1586e-14          1.3161        0.016091         0.11218
v  CourantNb                  0.044415          2062.2          43.967          1.3766
v  FourierNb                  0.010859           15340          94.083         0.69866
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14828        0.010814        0.045671


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15414          138.05          2.0753


 TIME FOR THE TIME STEP              914:        0.45875E+02

===============================================================


 INSTANT    0.915000000E+02   TIME STEP NUMBER             915
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.363554416E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31883E+02 0.18348E+02
   Friction velocity        uet   :  0.19757E-02 0.25648E+01
   Friction velocity        uk    :  0.20687E-01 0.36048E+01
   Dimensionless distance   yplus :  0.90363E-01 0.34388E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        412
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    2002   0.46110E-02   0.39469E+00 
c  VelocityY    0.29392E+04    2002   0.46110E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    2002   0.46110E-02   0.00000E+00 
c  Pressure     0.43365E+00    7048   0.35071E-01   0.20422E+00 
c  k            0.22179E+04    1494   0.14906E-03   0.15396E+01 
c  omega        0.63154E+09     118   0.71330E-05   0.71055E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0468e+05                             1
a  Local Time Step       1.141e-05                         44541


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.3139          1.0577       0.0023866      2.5887e-06
v  Velocity[Y]                 -35.563          30.067          6.6513          20.055
v  Velocity[Z]                 -28.615          28.456        0.055966      -0.0054967
v  ǁVelocityǁ                 0.014747          35.972          10.667          20.218
v  Pressure                     -409.1           343.2         -54.965          31.359
v  k                        4.6931e-08          97.239          4.2631          1.6814
v  omega                         1e-24      1.9988e+08          9208.8          11.931
v  turbulent_viscosity      3.7303e-15          1.3104        0.016073         0.11209
v  CourantNb                  0.040259          2045.6          43.973          1.3768
v  FourierNb                  0.010861           15614           95.42         0.69868
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14843        0.010811        0.045668


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15654          139.39          2.0755


 TIME FOR THE TIME STEP              915:        0.47176E+02

===============================================================


 INSTANT    0.916000000E+02   TIME STEP NUMBER             916
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.492058893E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.39321E+02 0.13515E+02
   Friction velocity        uet   :  0.93829E-03 0.33463E+01
   Friction velocity        uk    :  0.31013E-01 0.39996E+01
   Dimensionless distance   yplus :  0.14419E+00 0.38415E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        440
   Nb of faces within the viscous sub-layer     :        938
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29394E+04    2038   0.46466E-02   0.39839E+00 
c  VelocityY    0.29394E+04    2038   0.46466E-02   0.00000E+00 
c  VelocityZ    0.29394E+04    2038   0.46466E-02   0.00000E+00 
c  Pressure     0.41077E+00    7091   0.38463E-01   0.19356E+00 
c  k            0.22103E+04    1341   0.12854E-03   0.14550E+01 
c  omega        0.15897E+09     239   0.14206E-04   0.18038E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1503e-05                         44551


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1079         0.85183       0.0015596      4.1671e-06
v  Velocity[Y]                 -22.213          30.592          6.6746          20.056
v  Velocity[Z]                 -28.918           29.06        0.093635      -0.0044282
v  ǁVelocityǁ                0.0056319          33.449          10.665          20.219
v  Pressure                    -409.13          343.75         -57.281          31.625
v  k                        1.2031e-09          57.541          4.2205          1.6814
v  omega                         1e-24      1.0029e+08          8435.7          11.872
v  turbulent_viscosity      7.7106e-16          1.3052        0.016031         0.11201
v  CourantNb                 0.0081525          3006.5          44.314          1.3772
v  FourierNb                  0.010863           15830          95.711         0.69856
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14745         0.01081        0.045616


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15871          140.02          2.0758


 TIME FOR THE TIME STEP              916:        0.47262E+02

===============================================================


 INSTANT    0.917000000E+02   TIME STEP NUMBER             917
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.367111445E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30896E+02 0.13356E+02
   Friction velocity        uet   :  0.15728E-02 0.26179E+01
   Friction velocity        uk    :  0.18768E-01 0.32391E+01
   Dimensionless distance   yplus :  0.11896E+00 0.28647E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        403
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    2130   0.45297E-02   0.40495E+00 
c  VelocityY    0.29395E+04    2130   0.45297E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    2130   0.45297E-02   0.00000E+00 
c  Pressure     0.40128E+00    7029   0.36684E-01   0.18928E+00 
c  k            0.22020E+04    1088   0.84786E-04   0.12627E+01 
c  omega        0.41602E+08     211   0.33676E-04   0.69822E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7505e+05                             3
a  Local Time Step      1.0541e-05                         44542


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.98171         0.78087       0.0013291       5.461e-06
v  Velocity[Y]                 -17.599          30.937          6.7142          20.056
v  Velocity[Z]                 -29.567          28.874         0.10191      -0.0031879
v  ǁVelocityǁ                 0.015009          33.681          10.634          20.219
v  Pressure                    -408.95          346.36         -58.009           31.74
v  k                        9.9101e-09          52.521          4.1943          1.6812
v  omega                         1e-24      5.0767e+07          8281.4          11.865
v  turbulent_viscosity      3.8689e-17           1.301        0.015952         0.11194
v  CourantNb                  0.045387            2656          44.395          1.3775
v  FourierNb                  0.010865           15833          95.479         0.69776
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14847        0.010809        0.045609


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15877          139.87          2.0753


 TIME FOR THE TIME STEP              917:        0.48081E+02

===============================================================


 INSTANT    0.918000000E+02   TIME STEP NUMBER             918
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.504738992E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31535E+02 0.14045E+02
   Friction velocity        uet   :  0.16194E-02 0.28302E+01
   Friction velocity        uk    :  0.15965E-01 0.34201E+01
   Dimensionless distance   yplus :  0.13508E+00 0.29237E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    2191   0.45754E-02   0.41683E+00 
c  VelocityY    0.29396E+04    2191   0.45754E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    2191   0.45754E-02   0.00000E+00 
c  Pressure     0.40757E+00    7090   0.32987E-01   0.19086E+00 
c  k            0.21936E+04    1402   0.88159E-04   0.12790E+01 
c  omega        0.19826E+08     419   0.14578E-03   0.21198E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -27974                             1
a  Local Time Step      1.1617e-05                         44537


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89691         0.77074       0.0022617      3.5046e-06
v  Velocity[Y]                 -16.335          32.519           6.755          20.056
v  Velocity[Z]                 -29.317          29.672        0.080746      -0.0020147
v  ǁVelocityǁ                0.0087636          33.436          10.583          20.219
v  Pressure                    -406.48          348.53         -57.524          31.748
v  k                        1.9741e-08          50.707          4.1363           1.681
v  omega                         1e-24      6.2244e+07          9002.6          11.918
v  turbulent_viscosity      5.9047e-16          1.2944        0.015872         0.11188
v  CourantNb                  0.020679          2030.1          44.354          1.3778
v  FourierNb                  0.010867           15797          96.283         0.69705
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14737        0.010809        0.045605


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.98851           15850          140.64          2.0748


 TIME FOR THE TIME STEP              918:        0.49506E+02

===============================================================


 INSTANT    0.919000000E+02   TIME STEP NUMBER             919
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.104658051E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32167E+02 0.16696E+02
   Friction velocity        uet   :  0.80995E-03 0.28454E+01
   Friction velocity        uk    :  0.67760E-02 0.27533E+01
   Dimensionless distance   yplus :  0.78118E-01 0.30066E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        402
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2101   0.45299E-02   0.43600E+00 
c  VelocityY    0.29397E+04    2101   0.45299E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2101   0.45299E-02   0.00000E+00 
c  Pressure     0.44727E+00    7050   0.30693E-01   0.21016E+00 
c  k            0.21829E+04    1500   0.80053E-04   0.12850E+01 
c  omega        0.28020E+08     360   0.50615E-04   0.91778E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1606e+05                             1
a  Local Time Step      1.1464e-05                         44514


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.83556         0.84342       0.0039858      3.3485e-06
v  Velocity[Y]                 -15.213          32.615          6.7623          20.057
v  Velocity[Z]                 -28.641          29.347          0.0432     -0.00075306
v  ǁVelocityǁ                 0.020182          33.279          10.545          20.219
v  Pressure                    -394.36          348.67         -57.169          31.379
v  k                        4.6202e-08          46.269          4.0491          1.6807
v  omega                         1e-24       3.211e+07          8623.1          11.896
v  turbulent_viscosity      8.7096e-15          1.2848         0.01578         0.11182
v  CourantNb                  0.016468          2044.1           44.32          1.3779
v  FourierNb                  0.010869           15781          96.586         0.69643
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14718         0.01081        0.045616


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90898           15844          140.91          2.0744


 TIME FOR THE TIME STEP              919:        0.48114E+02

===============================================================


 INSTANT    0.920000000E+02   TIME STEP NUMBER             920
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.312292677E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31857E+02 0.19552E+02
   Friction velocity        uet   :  0.71257E-03 0.27595E+01
   Friction velocity        uk    :  0.27465E-01 0.29134E+01
   Dimensionless distance   yplus :  0.16277E+00 0.36617E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        418
   Nb of faces within the viscous sub-layer     :        944
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    1941   0.46510E-02   0.44266E+00 
c  VelocityY    0.29396E+04    1941   0.46510E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    1941   0.46510E-02   0.00000E+00 
c  Pressure     0.43910E+00    6969   0.29395E-01   0.20706E+00 
c  k            0.21721E+04    1533   0.68045E-04   0.11922E+01 
c  omega        0.14528E+08     293   0.44769E-04   0.33184E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.259e+05                             2
a  Local Time Step      1.1629e-05                         44491


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85721          1.0413       0.0063639      1.4245e-06
v  Velocity[Y]                  -15.08          33.303          6.7441          20.057
v  Velocity[Z]                 -28.638           29.17       0.0053249      0.00065711
v  ǁVelocityǁ                 0.014163          33.547          10.526          20.218
v  Pressure                     -375.6          347.84         -56.543          31.094
v  k                        8.3385e-08          39.553          3.9873          1.6805
v  omega                         1e-24      1.7975e+07          8353.3          11.859
v  turbulent_viscosity      3.6736e-14          1.2746         0.01568         0.11177
v  CourantNb                   0.04987          2042.6          44.332          1.3781
v  FourierNb                  0.010871           15699           95.39         0.69548
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14704         0.01081        0.045655


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15773          139.72          2.0736


 TIME FOR THE TIME STEP              920:        0.47951E+02

===============================================================


 INSTANT    0.921000000E+02   TIME STEP NUMBER             921
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240239290E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31330E+02 0.20223E+02
   Friction velocity        uet   :  0.22932E-02 0.26806E+01
   Friction velocity        uk    :  0.18246E-01 0.33650E+01
   Dimensionless distance   yplus :  0.10423E+00 0.28837E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        464
   Nb of faces within the viscous sub-layer     :        943
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1933   0.45307E-02   0.45230E+00 
c  VelocityY    0.29393E+04    1933   0.45307E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1933   0.45307E-02   0.00000E+00 
c  Pressure     0.45377E+00    6788   0.27615E-01   0.21413E+00 
c  k            0.21634E+04    1498   0.64747E-04   0.12121E+01 
c  omega        0.10782E+08     234   0.34386E-04   0.19017E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -54650                             2
a  Local Time Step      1.0921e-05                         44464


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.87562          1.2967       0.0080179      2.9033e-07
v  Velocity[Y]                 -15.248          30.416          6.7476          20.056
v  Velocity[Z]                  -29.52          29.151       -0.022564       0.0018631
v  ǁVelocityǁ                 0.010669          34.931          10.525          20.217
v  Pressure                    -357.77          347.64         -55.046          31.019
v  k                        1.4808e-07          38.993          3.9427          1.6803
v  omega                         1e-24      1.2399e+07          8152.1          11.838
v  turbulent_viscosity      1.2882e-14          1.2652        0.015596         0.11172
v  CourantNb                  0.038988          2035.3          44.588          1.3784
v  FourierNb                  0.010872           15480          93.732         0.69445
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14771        0.010811        0.045709


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15563          138.32          2.0729


 TIME FOR THE TIME STEP              921:        0.45746E+02

===============================================================


 INSTANT    0.922000000E+02   TIME STEP NUMBER             922
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.115662062E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30541E+02 0.19855E+02
   Friction velocity        uet   :  0.84975E-03 0.28824E+01
   Friction velocity        uk    :  0.16982E-01 0.31393E+01
   Dimensionless distance   yplus :  0.15687E+00 0.28566E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        505
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1959   0.46573E-02   0.44955E+00 
c  VelocityY    0.29391E+04    1959   0.46573E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1959   0.46573E-02   0.00000E+00 
c  Pressure     0.43904E+00    6970   0.28571E-01   0.20684E+00 
c  k            0.21572E+04    1421   0.64136E-04   0.13038E+01 
c  omega        0.10266E+08     212   0.28914E-04   0.26750E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0017e+05                             2
a  Local Time Step      1.1081e-05                         44449


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.88154           1.498       0.0085064     -1.5916e-06
v  Velocity[Y]                 -15.264          30.324          6.7677          20.056
v  Velocity[Z]                 -31.439          29.136       -0.047554       0.0030272
v  ǁVelocityǁ                 0.015471          36.626          10.544          20.217
v  Pressure                    -353.26          349.35         -53.066          31.367
v  k                        2.0931e-08          49.993          3.9332          1.6802
v  omega                         1e-24      1.1764e+07          8165.9          11.849
v  turbulent_viscosity      1.2168e-13          1.2547        0.015545         0.11168
v  CourantNb                 0.0055048          2024.8          44.802          1.3784
v  FourierNb                  0.010874           15390          91.583         0.69322
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14858        0.010812        0.045743


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15439          136.39          2.0716


 TIME FOR THE TIME STEP              922:        0.45738E+02

===============================================================


 INSTANT    0.923000000E+02   TIME STEP NUMBER             923
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.168172105E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31585E+02 0.15711E+02
   Friction velocity        uet   :  0.13077E-02 0.30816E+01
   Friction velocity        uk    :  0.14460E-01 0.31526E+01
   Dimensionless distance   yplus :  0.10004E+00 0.28599E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :        965
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1902   0.44477E-02   0.44361E+00 
c  VelocityY    0.29391E+04    1902   0.44477E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1902   0.44477E-02   0.00000E+00 
c  Pressure     0.44917E+00    7104   0.33392E-01   0.21294E+00 
c  k            0.21559E+04    1373   0.69809E-04   0.14256E+01 
c  omega        0.10561E+08     298   0.65072E-04   0.14217E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -62654                             2
a  Local Time Step      1.1562e-05                         44394


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85415          1.6267       0.0082495     -3.0986e-08
v  Velocity[Y]                 -15.163          31.394          6.8001          20.057
v  Velocity[Z]                 -32.863          28.876       -0.047825         0.00388
v  ǁVelocityǁ                0.0096448            36.9          10.605          20.217
v  Pressure                    -410.92          351.11         -51.273          31.665
v  k                        9.9479e-08          61.882          3.9601          1.6799
v  omega                         1e-24      4.4393e+07          8206.3          11.858
v  turbulent_viscosity      9.4561e-14          1.2456         0.01554         0.11163
v  CourantNb                  0.032046          2153.6          44.705           1.378
v  FourierNb                  0.010875           15404          90.316         0.69251
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14915        0.010813        0.045752


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.99356           15459          135.02          2.0705


 TIME FOR THE TIME STEP              923:        0.46373E+02

===============================================================


 INSTANT    0.924000000E+02   TIME STEP NUMBER             924
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.506080018E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30867E+02 0.14183E+02
   Friction velocity        uet   :  0.19310E-02 0.31688E+01
   Friction velocity        uk    :  0.12843E-01 0.29206E+01
   Dimensionless distance   yplus :  0.14285E+00 0.28270E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :        970
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1918   0.45240E-02   0.43903E+00 
c  VelocityY    0.29390E+04    1918   0.45240E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1918   0.45240E-02   0.00000E+00 
c  Pressure     0.42439E+00    7130   0.37354E-01   0.20100E+00 
c  k            0.21611E+04    1489   0.72440E-04   0.14869E+01 
c  omega        0.34001E+08     160   0.13233E-04   0.40474E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.838e+05                             2
a  Local Time Step       1.142e-05                         44356


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79953          1.6508       0.0075805      3.4844e-06
v  Velocity[Y]                 -16.046          30.837          6.8348          20.056
v  Velocity[Z]                 -32.408           28.68       -0.010595       0.0047489
v  ǁVelocityǁ                0.0090967          34.952          10.675          20.216
v  Pressure                    -436.91          351.13         -50.223          31.822
v  k                        2.5355e-09          65.794           4.001          1.6795
v  omega                         1e-24      2.2204e+07          8044.2          11.838
v  turbulent_viscosity      5.5249e-14          1.2372        0.015566         0.11159
v  CourantNb                 0.0094092          2722.1           44.66          1.3776
v  FourierNb                  0.010877           15383          89.984         0.69196
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14839        0.010814        0.045731


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.88537           15446          134.64          2.0696


 TIME FOR THE TIME STEP              924:        0.45747E+02

===============================================================


 INSTANT    0.925000000E+02   TIME STEP NUMBER             925
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.601948530E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31665E+02 0.14607E+02
   Friction velocity        uet   :  0.13151E-02 0.30887E+01
   Friction velocity        uk    :  0.19511E-01 0.30242E+01
   Dimensionless distance   yplus :  0.17570E+00 0.27556E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        481
   Nb of faces within the viscous sub-layer     :        967
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29390E+04    1905   0.45360E-02   0.41877E+00 
c  VelocityY    0.29390E+04    1905   0.45360E-02   0.00000E+00 
c  VelocityZ    0.29390E+04    1905   0.45360E-02   0.00000E+00 
c  Pressure     0.41187E+00    7106   0.37846E-01   0.19487E+00 
c  k            0.21698E+04    1531   0.74982E-04   0.15176E+01 
c  omega        0.12982E+08     202   0.15609E-03   0.12125E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0804e+05                             2
a  Local Time Step      1.1207e-05                         44384


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.72356          1.6022       0.0063637      4.5934e-06
v  Velocity[Y]                 -22.924          29.949          6.8318          20.056
v  Velocity[Z]                 -32.073          28.719        0.054879       0.0052755
v  ǁVelocityǁ                0.0075107          33.408          10.696          20.216
v  Pressure                    -438.97          350.34         -49.714          32.119
v  k                        1.2621e-08          58.558           4.032          1.6787
v  omega                         1e-24      6.6775e+07          8368.8          11.868
v  turbulent_viscosity      1.5497e-14            1.23        0.015612         0.11154
v  CourantNb                  0.020364          2749.1          44.697          1.3774
v  FourierNb                  0.010879           15146          90.901         0.69183
v  total_pressure           1.0089e+05      1.0168e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14765        0.010816        0.045688


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.70054           15216           135.6          2.0692


 TIME FOR THE TIME STEP              925:        0.45738E+02

===============================================================


 INSTANT    0.926000000E+02   TIME STEP NUMBER             926
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.622341576E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32207E+02 0.14059E+02
   Friction velocity        uet   :  0.94425E-03 0.28335E+01
   Friction velocity        uk    :  0.24678E-01 0.32147E+01
   Dimensionless distance   yplus :  0.13388E+00 0.26822E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        438
   Nb of faces within the viscous sub-layer     :        945
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1870   0.45807E-02   0.37324E+00 
c  VelocityY    0.29392E+04    1870   0.45807E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1870   0.45807E-02   0.00000E+00 
c  Pressure     0.43694E+00    6969   0.34170E-01   0.20636E+00 
c  k            0.21776E+04    1457   0.79908E-04   0.15410E+01 
c  omega        0.24480E+08     164   0.54080E-04   0.66730E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1892e+05                             3
a  Local Time Step      1.1514e-05                         44411


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.62662          1.4933       0.0050541      6.2102e-06
v  Velocity[Y]                 -26.852           29.78          6.7544          20.056
v  Velocity[Z]                 -29.607           28.48         0.12668       0.0060508
v  ǁVelocityǁ                  0.01255          32.577          10.665          20.216
v  Pressure                    -423.14          348.75         -49.888          32.212
v  k                        7.9481e-09          54.565          4.0612          1.6777
v  omega                         1e-24      3.4208e+07          8438.4          11.881
v  turbulent_viscosity      4.5151e-14          1.2263        0.015645         0.11148
v  CourantNb                  0.020089          2124.5          44.633          1.3774
v  FourierNb                   0.01088           14873          91.626         0.69158
v  total_pressure            1.009e+05      1.0167e+05      1.0128e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010817        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.69875           14949          136.26          2.0689


 TIME FOR THE TIME STEP              926:        0.44114E+02

===============================================================


 INSTANT    0.927000000E+02   TIME STEP NUMBER             927
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.795870238E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31614E+02 0.19140E+02
   Friction velocity        uet   :  0.70752E-03 0.26104E+01
   Friction velocity        uk    :  0.34445E-01 0.27606E+01
   Dimensionless distance   yplus :  0.16460E+00 0.26687E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        380
   Nb of faces within the viscous sub-layer     :        964
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1956   0.44350E-02   0.33574E+00 
c  VelocityY    0.29393E+04    1956   0.44350E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1956   0.44350E-02   0.00000E+00 
c  Pressure     0.44159E+00    7054   0.30729E-01   0.20918E+00 
c  k            0.21791E+04    1355   0.10220E-03   0.14681E+01 
c  omega        0.12411E+08     250   0.53013E-04   0.37442E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -60342                             1
a  Local Time Step      1.1509e-05                         44415


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.52901          1.3841       0.0042979      5.8401e-06
v  Velocity[Y]                 -24.304          29.595          6.6456          20.057
v  Velocity[Z]                  -29.71          28.696         0.16867       0.0063966
v  ǁVelocityǁ                0.0080632          32.975          10.662          20.216
v  Pressure                    -398.24          346.31         -50.747          32.249
v  k                        4.8774e-09          84.982          4.1161          1.6764
v  omega                         1e-24       1.864e+07          8224.1          11.886
v  turbulent_viscosity      4.2175e-14          1.2248        0.015677         0.11142
v  CourantNb                  0.025834          2031.9          44.341          1.3772
v  FourierNb                   0.01088           14644          92.599         0.69166
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14893        0.010818        0.045626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92986           14687          136.94          2.0689


 TIME FOR THE TIME STEP              927:        0.45849E+02

===============================================================


 INSTANT    0.928000000E+02   TIME STEP NUMBER             928
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.786377695E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30769E+02 0.18066E+02
   Friction velocity        uet   :  0.59191E-03 0.26066E+01
   Friction velocity        uk    :  0.23642E-01 0.30047E+01
   Dimensionless distance   yplus :  0.75024E-01 0.30437E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        393
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1989   0.45770E-02   0.31732E+00 
c  VelocityY    0.29393E+04    1989   0.45770E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1989   0.45770E-02   0.00000E+00 
c  Pressure     0.44318E+00    7051   0.32321E-01   0.20963E+00 
c  k            0.21728E+04    1298   0.12020E-03   0.13250E+01 
c  omega        0.10425E+08     474   0.39020E-04   0.39289E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -2.704e+05                             2
a  Local Time Step      1.1548e-05                         44393


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.44506          1.2601       0.0036866      6.5481e-06
v  Velocity[Y]                 -38.303          30.055          6.5986          20.056
v  Velocity[Z]                 -28.905          28.553         0.20145       0.0064254
v  ǁVelocityǁ                 0.014332          38.827           10.65          20.215
v  Pressure                    -401.22          346.04         -52.191           32.27
v  k                        1.5279e-08          93.821          4.1604           1.675
v  omega                         1e-24      1.2047e+07          8193.4          11.924
v  turbulent_viscosity      3.0243e-15          1.2243        0.015676         0.11135
v  CourantNb                  0.025199          2049.2          44.287          1.3772
v  FourierNb                  0.010879           14644          94.113           0.692
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14881        0.010819        0.045664


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14685           138.4          2.0692


 TIME FOR THE TIME STEP              928:        0.46247E+02

===============================================================


 INSTANT    0.929000000E+02   TIME STEP NUMBER             929
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.229459902E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46858E+02 0.13363E+02
   Friction velocity        uet   :  0.27635E-02 0.34807E+01
   Friction velocity        uk    :  0.11386E-01 0.38581E+01
   Dimensionless distance   yplus :  0.15017E+00 0.38484E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        376
   Nb of faces within the viscous sub-layer     :       1021
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    2021   0.45523E-02   0.30594E+00 
c  VelocityY    0.29393E+04    2021   0.45523E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    2021   0.45523E-02   0.00000E+00 
c  Pressure     0.43747E+00    6991   0.36108E-01   0.20681E+00 
c  k            0.21640E+04    1341   0.12362E-03   0.12010E+01 
c  omega        0.10503E+08     410   0.53512E-04   0.19937E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.4728e+05                             2
a  Local Time Step      1.0913e-05                         44385


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.48762          1.1359       0.0032397      6.8467e-06
v  Velocity[Y]                 -27.845          30.463           6.601          20.056
v  Velocity[Z]                 -29.373          28.743         0.21687       0.0064116
v  ǁVelocityǁ                0.0078556          33.485          10.623          20.214
v  Pressure                    -402.25           346.4         -54.058          32.458
v  k                        9.2816e-09          42.669          4.1254          1.6735
v  omega                         1e-24      1.1704e+07          8043.3          11.904
v  turbulent_viscosity      3.4146e-14          1.2272        0.015653         0.11127
v  CourantNb                  0.017164          2856.7          44.577          1.3773
v  FourierNb                  0.010878           14622          94.243         0.69151
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1486        0.010819        0.045684


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14668          138.82          2.0689


 TIME FOR THE TIME STEP              929:        0.45854E+02

===============================================================


 INSTANT    0.930000000E+02   TIME STEP NUMBER             930
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.176749331E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31187E+02 0.13662E+02
   Friction velocity        uet   :  0.18554E-02 0.29543E+01
   Friction velocity        uk    :  0.19082E-01 0.31826E+01
   Dimensionless distance   yplus :  0.10813E+00 0.27964E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        432
   Nb of faces within the viscous sub-layer     :       1058
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    2081   0.44808E-02   0.29913E+00 
c  VelocityY    0.29395E+04    2081   0.44808E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    2081   0.44808E-02   0.00000E+00 
c  Pressure     0.45651E+00    7092   0.35575E-01   0.21553E+00 
c  k            0.21563E+04    1413   0.75738E-04   0.10227E+01 
c  omega        0.99662E+07     336   0.71320E-04   0.25386E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3371e+05                             1
a  Local Time Step      1.1299e-05                         44404


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.58773          1.1565       0.0027952      7.2111e-06
v  Velocity[Y]                 -17.585           32.06          6.6295          20.056
v  Velocity[Z]                 -29.063          29.222         0.20697       0.0058183
v  ǁVelocityǁ                 0.012033          33.437          10.582          20.214
v  Pressure                    -402.61          346.54         -55.203          32.594
v  k                        1.6901e-09           53.59          4.1179          1.6719
v  omega                         1e-24      1.6631e+07          7977.4          11.884
v  turbulent_viscosity      5.0698e-15          1.2335        0.015607         0.11119
v  CourantNb                  0.016207          2955.8          44.724          1.3773
v  FourierNb                  0.010876           14750          93.098         0.69032
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14773         0.01082          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          0.9359           14803          137.82          2.0676


 TIME FOR THE TIME STEP              930:        0.48210E+02

===============================================================


 INSTANT    0.931000000E+02   TIME STEP NUMBER             931
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.222527798E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30136E+02 0.14271E+02
   Friction velocity        uet   :  0.20712E-02 0.29276E+01
   Friction velocity        uk    :  0.24153E-01 0.29428E+01
   Dimensionless distance   yplus :  0.16873E+00 0.27888E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        496
   Nb of faces within the viscous sub-layer     :       1074
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    2054   0.43989E-02   0.30723E+00 
c  VelocityY    0.29397E+04    2054   0.43989E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    2054   0.43989E-02   0.00000E+00 
c  Pressure     0.42817E+00    7005   0.33411E-01   0.20230E+00 
c  k            0.21505E+04    1447   0.74006E-04   0.98482E+00 
c  omega        0.13409E+16       2   0.72489E-11   0.23022E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6444e+05                             2
a  Local Time Step      1.0935e-05                         44416


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.70063           1.377       0.0025432      5.3038e-06
v  Velocity[Y]                 -16.989          33.114          6.6764          20.057
v  Velocity[Z]                 -28.926          28.993           0.175       0.0051881
v  ǁVelocityǁ                0.0044998          33.682          10.542          20.214
v  Pressure                     -401.6          346.19          -55.47          32.548
v  k                        1.9052e-10          61.261          4.1148          1.6704
v  omega                         1e-24      5.5508e+07          8921.4          11.909
v  turbulent_viscosity      2.0972e-15          1.2453        0.015578          0.1111
v  CourantNb                  0.019711          2085.9          44.575          1.3771
v  FourierNb                  0.010875           14876          93.405         0.68969
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14801        0.010821        0.045729


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           14938          137.98          2.0668


 TIME FOR THE TIME STEP              931:        0.45290E+02

===============================================================


 INSTANT    0.932000000E+02   TIME STEP NUMBER             932
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.788604482E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31990E+02 0.14424E+02
   Friction velocity        uet   :  0.68879E-03 0.29221E+01
   Friction velocity        uk    :  0.14590E-01 0.31808E+01
   Dimensionless distance   yplus :  0.11906E+00 0.31295E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1087
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    2019   0.45028E-02   0.32703E+00 
c  VelocityY    0.29399E+04    2019   0.45028E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    2019   0.45028E-02   0.00000E+00 
c  Pressure     0.42177E+00    6781   0.31488E-01   0.19858E+00 
c  k            0.21457E+04    1527   0.82659E-04   0.11420E+01 
c  omega        0.26090E+08     327   0.46288E-04   0.10351E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1114e+05                             3
a  Local Time Step      1.1757e-05                         44450


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.79575          1.6582       0.0026745      3.6185e-06
v  Velocity[Y]                 -15.311          32.905          6.7152          20.057
v  Velocity[Z]                 -28.678           29.26         0.12242       0.0045098
v  ǁVelocityǁ                0.0031097          33.707          10.506          20.213
v  Pressure                    -392.39           344.5         -55.625          32.242
v  k                        2.5541e-09          50.131          4.0755          1.6688
v  omega                         1e-24      2.8842e+07          8656.6          11.933
v  turbulent_viscosity      2.4383e-16          1.2494        0.015559         0.11096
v  CourantNb                  0.030952          2078.4          44.324          1.3769
v  FourierNb                  0.010872           15037          94.633         0.68922
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14777         0.01082        0.045742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15079          138.96          2.0661


 TIME FOR THE TIME STEP              932:        0.44855E+02

===============================================================


 INSTANT    0.933000000E+02   TIME STEP NUMBER             933
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.159971503E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31500E+02 0.15104E+02
   Friction velocity        uet   :  0.27604E-03 0.28227E+01
   Friction velocity        uk    :  0.21718E-01 0.29555E+01
   Dimensionless distance   yplus :  0.16023E+00 0.35778E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1081
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29402E+04    2054   0.45870E-02   0.34504E+00 
c  VelocityY    0.29402E+04    2054   0.45870E-02   0.00000E+00 
c  VelocityZ    0.29402E+04    2054   0.45870E-02   0.00000E+00 
c  Pressure     0.44521E+00    7014   0.30092E-01   0.20914E+00 
c  k            0.21416E+04    1413   0.74379E-04   0.10369E+01 
c  omega        0.14512E+08     321   0.14202E-03   0.14493E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0077e+05                             1
a  Local Time Step      1.1261e-05                         44467


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86105          1.8604       0.0029333      7.1972e-07
v  Velocity[Y]                 -15.965          32.767          6.7069          20.057
v  Velocity[Z]                 -28.642          29.218        0.056638       0.0031779
v  ǁVelocityǁ                 0.014806          33.342          10.483          20.213
v  Pressure                    -374.96          342.37         -55.509          31.779
v  k                        2.6542e-08          44.685          4.0096          1.6672
v  omega                         1e-24      5.7195e+07          8993.7          11.956
v  turbulent_viscosity      1.2001e-14          1.2659        0.015547         0.11088
v  CourantNb                  0.023645          2060.2          44.299          1.3767
v  FourierNb                  0.010869           15157          94.458         0.68832
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14829        0.010819        0.045727


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15199          138.76          2.0651


 TIME FOR THE TIME STEP              933:        0.45863E+02

===============================================================


 INSTANT    0.934000000E+02   TIME STEP NUMBER             934
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.109934289E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31838E+02 0.19981E+02
   Friction velocity        uet   :  0.72484E-03 0.27401E+01
   Friction velocity        uk    :  0.21329E-01 0.28562E+01
   Dimensionless distance   yplus :  0.92682E-01 0.32169E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1085
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    2068   0.45132E-02   0.35305E+00 
c  VelocityY    0.29404E+04    2068   0.45132E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    2068   0.45132E-02   0.00000E+00 
c  Pressure     0.42814E+00    6982   0.28503E-01   0.20325E+00 
c  k            0.21394E+04    1235   0.70256E-04   0.10331E+01 
c  omega        0.19793E+08     199   0.13272E-03   0.20604E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80101                             1
a  Local Time Step      1.1751e-05                         44461


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.97721          1.9777       0.0038412     -2.8894e-06
v  Velocity[Y]                 -15.302           30.75          6.6982          20.057
v  Velocity[Z]                 -29.066          29.437       0.0016224       0.0018264
v  ǁVelocityǁ                 0.016327          33.915          10.468          20.213
v  Pressure                     -359.8          342.93         -54.765          31.642
v  k                        1.6106e-08          44.932          3.9824          1.6659
v  omega                         1e-24      1.0808e+08          8745.6          11.925
v  turbulent_viscosity      7.8848e-14          1.2791        0.015554         0.11079
v  CourantNb                  0.035916          2033.5          44.169          1.3768
v  FourierNb                  0.010865           15187          93.916         0.68774
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14788        0.010819        0.045723


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15233          138.08          2.0646


 TIME FOR THE TIME STEP              934:        0.45321E+02

===============================================================


 INSTANT    0.935000000E+02   TIME STEP NUMBER             935
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.610165302E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30648E+02 0.19818E+02
   Friction velocity        uet   :  0.88887E-03 0.27744E+01
   Friction velocity        uk    :  0.57601E-02 0.29764E+01
   Dimensionless distance   yplus :  0.68338E-01 0.28703E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :       1094
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    2008   0.46570E-02   0.36970E+00 
c  VelocityY    0.29407E+04    2008   0.46570E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    2008   0.46570E-02   0.00000E+00 
c  Pressure     0.44356E+00    7012   0.27748E-01   0.20879E+00 
c  k            0.21401E+04    1051   0.70432E-04   0.11363E+01 
c  omega        0.47415E+08     158   0.29076E-04   0.60941E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8988e+05                             2
a  Local Time Step       1.132e-05                         44466


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2098          2.1071       0.0043295     -5.0075e-06
v  Velocity[Y]                  -15.32          30.361          6.7104          20.057
v  Velocity[Z]                  -31.08          29.152        -0.05472      0.00039958
v  ǁVelocityǁ                0.0092333          36.544          10.469          20.213
v  Pressure                    -348.99           344.7         -52.954          31.545
v  k                        1.0936e-07           50.64          4.0023          1.6649
v  omega                         1e-24      5.4546e+07          8320.9          11.886
v  turbulent_viscosity      1.1142e-14           1.295        0.015582         0.11071
v  CourantNb                   0.03331          2032.5           44.28          1.3768
v  FourierNb                  0.010861           15288          93.075         0.68752
v  total_pressure           1.0098e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14735         0.01082        0.045715


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15343          137.35          2.0643


 TIME FOR THE TIME STEP              935:        0.44025E+02

===============================================================


 INSTANT    0.936000000E+02   TIME STEP NUMBER             936
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.880107599E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31267E+02 0.17529E+02
   Friction velocity        uet   :  0.19946E-03 0.30836E+01
   Friction velocity        uk    :  0.12793E-01 0.29437E+01
   Dimensionless distance   yplus :  0.10398E+00 0.28704E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        474
   Nb of faces within the viscous sub-layer     :       1094
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29410E+04    2019   0.44935E-02   0.37850E+00 
c  VelocityY    0.29410E+04    2019   0.44935E-02   0.00000E+00 
c  VelocityZ    0.29410E+04    2019   0.44935E-02   0.00000E+00 
c  Pressure     0.42958E+00    7117   0.31766E-01   0.20324E+00 
c  k            0.21452E+04    1357   0.75171E-04   0.12736E+01 
c  omega        0.15859E+08     201   0.42197E-04   0.19043E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -80871                             2
a  Local Time Step      1.1474e-05                         44458


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4623          1.8872       0.0046147     -3.5628e-06
v  Velocity[Y]                 -15.359          32.419          6.7433          20.057
v  Velocity[Z]                   -32.5          29.256       -0.095666     -0.00096242
v  ǁVelocityǁ                0.0080097          37.114          10.514          20.213
v  Pressure                    -397.35           345.4         -51.624           31.74
v  k                        1.2216e-10          61.885          4.0441          1.6643
v  omega                         1e-24      2.8321e+07          8060.2           11.85
v  turbulent_viscosity      6.0225e-14          1.3113        0.015633         0.11063
v  CourantNb                  0.032612          2108.4          44.157          1.3764
v  FourierNb                  0.010857           15361          91.965         0.68714
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14708         0.01082        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89977           15425          136.12          2.0636


 TIME FOR THE TIME STEP              936:        0.45110E+02

===============================================================


 INSTANT    0.937000000E+02   TIME STEP NUMBER             937
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.456375628E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31227E+02 0.16309E+02
   Friction velocity        uet   :  0.77170E-03 0.32035E+01
   Friction velocity        uk    :  0.68930E-02 0.30659E+01
   Dimensionless distance   yplus :  0.60688E-01 0.27917E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :       1044
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29412E+04    2028   0.46226E-02   0.39779E+00 
c  VelocityY    0.29412E+04    2028   0.46226E-02   0.00000E+00 
c  VelocityZ    0.29412E+04    2028   0.46226E-02   0.00000E+00 
c  Pressure     0.43464E+00    6967   0.35541E-01   0.20420E+00 
c  k            0.21562E+04    1479   0.78554E-04   0.13654E+01 
c  omega        0.24121E+27       2   0.23932E-21   0.33317E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2388e+05                             2
a  Local Time Step      1.1152e-05                         44438


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7106          1.7443       0.0050304     -1.7605e-06
v  Velocity[Y]                 -15.285           32.44          6.7924          20.057
v  Velocity[Z]                 -33.367          28.874       -0.091958      -0.0026824
v  ǁVelocityǁ                0.0063223          35.451          10.583          20.212
v  Pressure                    -430.58          345.24          -50.91          31.767
v  k                        5.8621e-09          67.317          4.0892          1.6638
v  omega                         1e-24       9.668e+07          8935.3          11.873
v  turbulent_viscosity      4.1564e-16          1.3243        0.015685         0.11057
v  CourantNb                  0.037114          2644.9          44.079          1.3761
v  FourierNb                  0.010854           15364          91.503         0.68682
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14827         0.01082        0.045712


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84318           15436          135.58          2.0629


 TIME FOR THE TIME STEP              937:        0.44559E+02

===============================================================


 INSTANT    0.938000000E+02   TIME STEP NUMBER             938
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.168958522E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30641E+02 0.16795E+02
   Friction velocity        uet   :  0.70276E-03 0.32228E+01
   Friction velocity        uk    :  0.24130E-01 0.31551E+01
   Dimensionless distance   yplus :  0.14664E+00 0.27031E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        445
   Nb of faces within the viscous sub-layer     :       1026
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    1959   0.46218E-02   0.40711E+00 
c  VelocityY    0.29416E+04    1959   0.46218E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    1959   0.46218E-02   0.00000E+00 
c  Pressure     0.43731E+00    7141   0.37323E-01   0.20633E+00 
c  k            0.21717E+04    1525   0.79787E-04   0.14605E+01 
c  omega        0.48115E+08     148   0.40290E-04   0.10897E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6787e+05                             4
a  Local Time Step      1.1798e-05                         44407


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.771          1.6657       0.0058503       9.626e-07
v  Velocity[Y]                 -19.884          30.014          6.8298          20.057
v  Velocity[Z]                 -33.526          28.771       -0.053831      -0.0041908
v  ǁVelocityǁ                0.0075079          34.982          10.624          20.212
v  Pressure                    -441.42          343.98         -51.066          31.742
v  k                        3.4748e-10          61.181          4.1261          1.6636
v  omega                         1e-24      4.8929e+07          8642.4           11.88
v  turbulent_viscosity      1.2437e-14          1.3284        0.015738         0.11048
v  CourantNb                  0.012882          2831.6          44.078          1.3758
v  FourierNb                   0.01085           15291          91.835         0.68666
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010821        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.94643           15338          135.91          2.0625


 TIME FOR THE TIME STEP              938:        0.46164E+02

===============================================================


 INSTANT    0.939000000E+02   TIME STEP NUMBER             939
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.773612380E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31656E+02 0.15616E+02
   Friction velocity        uet   :  0.18633E-02 0.29701E+01
   Friction velocity        uk    :  0.19063E-01 0.27724E+01
   Dimensionless distance   yplus :  0.11024E+00 0.27171E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :       1048
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29418E+04    1900   0.44780E-02   0.38805E+00 
c  VelocityY    0.29418E+04    1900   0.44780E-02   0.00000E+00 
c  VelocityZ    0.29418E+04    1900   0.44780E-02   0.00000E+00 
c  Pressure     0.44596E+00    7068   0.35140E-01   0.21104E+00 
c  k            0.21900E+04    1401   0.78435E-04   0.14154E+01 
c  omega        0.20553E+08     196   0.49932E-04   0.54218E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3391e+05                             2
a  Local Time Step      1.1744e-05                         44459


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4933           1.734        0.005529      1.8573e-06
v  Velocity[Y]                 -25.234          29.885           6.812          20.057
v  Velocity[Z]                 -31.308          28.616      0.00033748      -0.0056663
v  ǁVelocityǁ                0.0095654          32.319           10.63          20.212
v  Pressure                    -432.25          343.15         -51.871          31.708
v  k                        4.6028e-09          48.615          4.1198          1.6634
v  omega                         1e-24      2.5683e+07          8473.6          11.893
v  turbulent_viscosity      2.7205e-15          1.3441        0.015752         0.11044
v  CourantNb                  0.062067          2482.4          44.175          1.3758
v  FourierNb                  0.010847           15516          92.261         0.68663
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14841        0.010822        0.045689


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15558          136.44          2.0625


 TIME FOR THE TIME STEP              939:        0.44665E+02

===============================================================


 INSTANT    0.940000000E+02   TIME STEP NUMBER             940
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.833751735E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31668E+02 0.15551E+02
   Friction velocity        uet   :  0.11707E-02 0.26996E+01
   Friction velocity        uk    :  0.15221E-01 0.28606E+01
   Dimensionless distance   yplus :  0.13401E+00 0.27884E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        407
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    1931   0.45191E-02   0.36286E+00 
c  VelocityY    0.29419E+04    1931   0.45191E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    1931   0.45191E-02   0.00000E+00 
c  Pressure     0.43997E+00    7097   0.31210E-01   0.20936E+00 
c  k            0.22019E+04    1352   0.81217E-04   0.13791E+01 
c  omega        0.12528E+08     226   0.21017E-03   0.17866E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5633e+05                             2
a  Local Time Step      1.1645e-05                         44477


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2599          1.6214       0.0036233     -1.5848e-06
v  Velocity[Y]                  -36.75          29.743          6.7307          20.056
v  Velocity[Z]                 -30.493          28.771        0.035293      -0.0070735
v  ǁVelocityǁ                 0.010389          36.944          10.643          20.212
v  Pressure                    -407.75          344.67         -53.264          31.464
v  k                         1.263e-08          67.242          4.1487          1.6635
v  omega                         1e-24      2.4498e+08          8983.4          11.971
v  turbulent_viscosity      4.5667e-14          1.3567        0.015748         0.11042
v  CourantNb                  0.026716          2053.6          44.219          1.3758
v  FourierNb                  0.010844           15577          92.872         0.68651
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14837        0.010821        0.045696


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15618          137.09          2.0624


 TIME FOR THE TIME STEP              940:        0.46839E+02

===============================================================


 INSTANT    0.941000000E+02   TIME STEP NUMBER             941
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.564183790E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30751E+02 0.25034E+02
   Friction velocity        uet   :  0.11566E-02 0.31728E+01
   Friction velocity        uk    :  0.21634E-01 0.30172E+01
   Dimensionless distance   yplus :  0.13432E+00 0.28229E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        450
   Nb of faces within the viscous sub-layer     :       1005
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29420E+04    1977   0.47056E-02   0.35405E+00 
c  VelocityY    0.29420E+04    1977   0.47056E-02   0.00000E+00 
c  VelocityZ    0.29420E+04    1977   0.47056E-02   0.00000E+00 
c  Pressure     0.42585E+00    7055   0.31678E-01   0.20141E+00 
c  k            0.22066E+04    1365   0.10383E-03   0.12636E+01 
c  omega        0.52328E+09      82   0.24511E-05   0.46004E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -47569                             1
a  Local Time Step      1.0688e-05                         44485


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1616          1.3972       0.0017719     -2.3983e-06
v  Velocity[Y]                 -35.281          29.941          6.6785          20.056
v  Velocity[Z]                 -29.353          28.822        0.058631      -0.0080411
v  ǁVelocityǁ                 0.010403          39.355          10.664          20.211
v  Pressure                    -411.24          346.03         -55.145          31.453
v  k                        2.9556e-08          100.97          4.2003          1.6639
v  omega                         1e-24      1.2248e+08          8399.4           11.91
v  turbulent_viscosity      2.2767e-15          1.3663        0.015737         0.11043
v  CourantNb                  0.023779          2067.2          44.272          1.3759
v  FourierNb                  0.010842           15649          94.331         0.68676
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14881        0.010821        0.045678


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15696           138.6          2.0627


 TIME FOR THE TIME STEP              941:        0.45993E+02

===============================================================


 INSTANT    0.942000000E+02   TIME STEP NUMBER             942
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.799446173E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.49244E+02 0.14414E+02
   Friction velocity        uet   :  0.57693E-03 0.34603E+01
   Friction velocity        uk    :  0.15604E-01 0.46599E+01
   Dimensionless distance   yplus :  0.13831E+00 0.37249E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        399
   Nb of faces within the viscous sub-layer     :        998
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    1940   0.45669E-02   0.35597E+00 
c  VelocityY    0.29421E+04    1940   0.45669E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    1940   0.45669E-02   0.00000E+00 
c  Pressure     0.45703E+00    7067   0.35926E-01   0.21603E+00 
c  k            0.22071E+04    1459   0.12349E-03   0.11369E+01 
c  omega        0.13116E+09     295   0.53252E-05   0.12156E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.3273e+05                             2
a  Local Time Step      1.1436e-05                         44493


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.1238          1.1731      0.00077328     -3.5611e-06
v  Velocity[Y]                 -30.996          30.376          6.6941          20.056
v  Velocity[Z]                 -28.621          28.824        0.069046      -0.0085927
v  ǁVelocityǁ                 0.006341          33.455          10.662          20.212
v  Pressure                    -412.78          346.99         -57.401          31.666
v  k                        1.1767e-09           66.01          4.2045          1.6649
v  omega                         1e-24      6.1234e+07          8010.9          11.862
v  turbulent_viscosity       1.111e-14          1.3754        0.015717         0.11046
v  CourantNb                  0.047796          2017.2          44.426          1.3762
v  FourierNb                  0.010841           15832          94.762         0.68679
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14927        0.010819         0.04565


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15887          139.19           2.063


 TIME FOR THE TIME STEP              942:        0.45709E+02

===============================================================


 INSTANT    0.943000000E+02   TIME STEP NUMBER             943
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.324279549E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31370E+02 0.14391E+02
   Friction velocity        uet   :  0.15172E-02 0.30194E+01
   Friction velocity        uk    :  0.15734E-01 0.31213E+01
   Dimensionless distance   yplus :  0.11598E+00 0.28245E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        374
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    1964   0.45237E-02   0.35245E+00 
c  VelocityY    0.29422E+04    1964   0.45237E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    1964   0.45237E-02   0.00000E+00 
c  Pressure     0.42094E+00    7043   0.36756E-01   0.19906E+00 
c  k            0.22079E+04    1503   0.84218E-04   0.10214E+01 
c  omega        0.34196E+08     326   0.17992E-04   0.65076E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1392e-05                         44526


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0533          1.0429      0.00030307     -4.0572e-06
v  Velocity[Y]                 -17.737          30.736          6.7286          20.056
v  Velocity[Z]                 -28.578          28.757         0.06437      -0.0095491
v  ǁVelocityǁ                  0.01785          33.355          10.636          20.212
v  Pressure                    -414.06          347.45         -58.897          31.677
v  k                         2.169e-08          49.058          4.1973          1.6662
v  omega                         1e-24      3.0649e+07          7991.3          11.857
v  turbulent_viscosity       2.216e-15           1.383        0.015699         0.11052
v  CourantNb                  0.022898          2981.9          44.741          1.3765
v  FourierNb                   0.01084           15910          94.626         0.68641
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14942        0.010818        0.045647


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15974          139.37          2.0629


 TIME FOR THE TIME STEP              943:        0.46076E+02

===============================================================


 INSTANT    0.944000000E+02   TIME STEP NUMBER             944
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.292594642E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31145E+02 0.14018E+02
   Friction velocity        uet   :  0.92676E-03 0.27738E+01
   Friction velocity        uk    :  0.13611E-01 0.28723E+01
   Dimensionless distance   yplus :  0.12478E+00 0.28001E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        416
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2089   0.46303E-02   0.35759E+00 
c  VelocityY    0.29422E+04    2089   0.46303E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2089   0.46303E-02   0.00000E+00 
c  Pressure     0.44808E+00    7056   0.33446E-01   0.21196E+00 
c  k            0.22107E+04    1509   0.71884E-04   0.94852E+00 
c  omega        0.14163E+08     350   0.18925E-03   0.21976E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.9295e+05                             1
a  Local Time Step      1.1447e-05                         44552


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.99208         0.95313     -0.00053448     -4.5923e-06
v  Velocity[Y]                 -17.218          32.356          6.7629          20.057
v  Velocity[Z]                 -28.651          28.743        0.033146       -0.010178
v  ǁVelocityǁ                 0.017477          33.912          10.589          20.213
v  Pressure                    -414.04          347.43         -58.946          31.766
v  k                        6.4837e-08          58.397          4.2067          1.6681
v  omega                         1e-24      6.5642e+07          8748.3          11.909
v  turbulent_viscosity      1.0698e-14          1.3919        0.015692          0.1106
v  CourantNb                  0.058992          2169.8          44.692          1.3765
v  FourierNb                  0.010839           15992          95.513         0.68622
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14879        0.010817        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16064           140.2          2.0627


 TIME FOR THE TIME STEP              944:        0.47699E+02

===============================================================


 INSTANT    0.945000000E+02   TIME STEP NUMBER             945
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.245643376E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30413E+02 0.13744E+02
   Friction velocity        uet   :  0.88082E-03 0.29138E+01
   Friction velocity        uk    :  0.14078E-01 0.30352E+01
   Dimensionless distance   yplus :  0.11120E+00 0.29768E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        447
   Nb of faces within the viscous sub-layer     :       1030
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29422E+04    2147   0.44928E-02   0.36937E+00 
c  VelocityY    0.29422E+04    2147   0.44928E-02   0.00000E+00 
c  VelocityZ    0.29422E+04    2147   0.44928E-02   0.00000E+00 
c  Pressure     0.43458E+00    6961   0.30563E-01   0.20575E+00 
c  k            0.22150E+04    1479   0.72017E-04   0.10291E+01 
c  omega        0.27994E+08     386   0.44292E-04   0.72999E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0989e-05                         44557


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.91273         0.86916      -0.0013528      -3.625e-06
v  Velocity[Y]                 -15.308          33.189          6.7865          20.057
v  Velocity[Z]                  -28.82          28.854       -0.012856       -0.010771
v  ǁVelocityǁ                 0.020799          33.833          10.541          20.213
v  Pressure                    -409.14          346.86          -58.53          31.513
v  k                        4.3834e-07          54.115          4.1704          1.6703
v  omega                         1e-24      3.3734e+07          8341.2           11.89
v  turbulent_viscosity      9.3566e-15          1.3968        0.015703         0.11071
v  CourantNb                  0.033029          2020.4          44.533          1.3765
v  FourierNb                   0.01084           15983          97.571         0.68697
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14876        0.010815        0.045626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16062           142.1          2.0635


 TIME FOR THE TIME STEP              945:        0.47773E+02

===============================================================


 INSTANT    0.946000000E+02   TIME STEP NUMBER             946
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.848837442E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31539E+02 0.14394E+02
   Friction velocity        uet   :  0.14760E-02 0.28620E+01
   Friction velocity        uk    :  0.15367E-01 0.32136E+01
   Dimensionless distance   yplus :  0.15446E+00 0.34121E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        455
   Nb of faces within the viscous sub-layer     :        974
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29421E+04    2254   0.42751E-02   0.38068E+00 
c  VelocityY    0.29421E+04    2254   0.42751E-02   0.00000E+00 
c  VelocityZ    0.29421E+04    2254   0.42751E-02   0.00000E+00 
c  Pressure     0.44958E+00    7061   0.30514E-01   0.21150E+00 
c  k            0.22178E+04    1398   0.65423E-04   0.98511E+00 
c  omega        0.12349E+08     325   0.76241E-04   0.51730E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.6049e+05                             4
a  Local Time Step      1.1889e-05                         44488


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86296         0.82657      -0.0018179      -3.156e-06
v  Velocity[Y]                 -15.246          33.176          6.7617          20.056
v  Velocity[Z]                 -28.902           28.95       -0.074012       -0.010882
v  ǁVelocityǁ                 0.017213            33.9          10.512          20.212
v  Pressure                    -391.65          348.03          -58.24          30.912
v  k                        3.4629e-08          40.942          4.1275          1.6729
v  omega                         1e-24      1.8665e+07          8214.1           11.87
v  turbulent_viscosity      8.3709e-14          1.4002        0.015698         0.11085
v  CourantNb                  0.030256          2034.6          44.386          1.3765
v  FourierNb                  0.010841           15942          98.045         0.68767
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14869        0.010815        0.045634


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15987          142.43          2.0642


 TIME FOR THE TIME STEP              946:        0.49030E+02

===============================================================


 INSTANT    0.947000000E+02   TIME STEP NUMBER             947
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.279567079E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31264E+02 0.23053E+02
   Friction velocity        uet   :  0.15089E-02 0.27463E+01
   Friction velocity        uk    :  0.67192E-02 0.33093E+01
   Dimensionless distance   yplus :  0.73982E-01 0.36558E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        500
   Nb of faces within the viscous sub-layer     :        941
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    2184   0.45387E-02   0.38733E+00 
c  VelocityY    0.29419E+04    2184   0.45387E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    2184   0.45387E-02   0.00000E+00 
c  Pressure     0.42480E+00    6991   0.28995E-01   0.19925E+00 
c  k            0.22215E+04    1415   0.56750E-04   0.97006E+00 
c  omega        0.16319E+08     226   0.34267E-03   0.11543E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7337e+05                             2
a  Local Time Step      1.1985e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.86556         0.86529      -0.0021377     -1.4307e-06
v  Velocity[Y]                 -15.317          31.733          6.7452          20.056
v  Velocity[Z]                 -29.368           28.77        -0.12002       -0.011247
v  ǁVelocityǁ                 0.016526          33.213          10.504          20.212
v  Pressure                    -378.49          349.74         -57.375          30.711
v  k                        4.3993e-10          40.231          4.0953          1.6761
v  omega                         1e-24      2.6245e+08            9358          11.912
v  turbulent_viscosity      3.5222e-15          1.4004        0.015694         0.11102
v  CourantNb                  0.029069          2047.7          44.193          1.3766
v  FourierNb                  0.010843           16034          96.319         0.68787
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01           0.149        0.010814        0.045626


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16088          140.51          2.0645


 TIME FOR THE TIME STEP              947:        0.47878E+02

===============================================================


 INSTANT    0.948000000E+02   TIME STEP NUMBER             948
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.534030715E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31554E+02 0.20990E+02
   Friction velocity        uet   :  0.16343E-02 0.25468E+01
   Friction velocity        uk    :  0.22788E-01 0.32119E+01
   Dimensionless distance   yplus :  0.12483E+00 0.29510E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        512
   Nb of faces within the viscous sub-layer     :        978
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29419E+04    2117   0.46024E-02   0.39243E+00 
c  VelocityY    0.29419E+04    2117   0.46024E-02   0.00000E+00 
c  VelocityZ    0.29419E+04    2117   0.46024E-02   0.00000E+00 
c  Pressure     0.43463E+00    6994   0.27309E-01   0.20414E+00 
c  k            0.22270E+04    1570   0.56729E-04   0.10690E+01 
c  omega        0.27040E+09      93   0.15892E-04   0.72065E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.934e+05                             2
a  Local Time Step       1.192e-05                         44390


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.89064          0.7818      -0.0025501      -1.689e-06
v  Velocity[Y]                 -15.338          30.596          6.7635          20.057
v  Velocity[Z]                 -30.797            28.8        -0.16479       -0.010737
v  ǁVelocityǁ                0.0071553           36.71          10.512          20.213
v  Pressure                    -354.15          351.62         -55.958          30.887
v  k                         4.965e-08          46.591          4.0834          1.6796
v  omega                         1e-24      1.3142e+08            9905          11.953
v  turbulent_viscosity      9.8318e-16          1.4021        0.015701         0.11122
v  CourantNb                  0.036883          2056.1          44.327          1.3767
v  FourierNb                  0.010845           16032          95.323         0.68868
v  total_pressure           1.0097e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14933        0.010814         0.04563


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16095          139.65          2.0654


 TIME FOR THE TIME STEP              948:        0.47215E+02

===============================================================


 INSTANT    0.949000000E+02   TIME STEP NUMBER             949
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.453899479E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31808E+02 0.19180E+02
   Friction velocity        uet   :  0.62103E-03 0.30133E+01
   Friction velocity        uk    :  0.19862E-01 0.28735E+01
   Dimensionless distance   yplus :  0.11386E+00 0.28364E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        429
   Nb of faces within the viscous sub-layer     :       1013
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29416E+04    2054   0.44405E-02   0.38949E+00 
c  VelocityY    0.29416E+04    2054   0.44405E-02   0.00000E+00 
c  VelocityZ    0.29416E+04    2054   0.44405E-02   0.00000E+00 
c  Pressure     0.44161E+00    6993   0.29488E-01   0.20859E+00 
c  k            0.22359E+04    1622   0.62344E-04   0.12164E+01 
c  omega        0.86200E+08     134   0.22021E-04   0.20199E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                 -1.99e+05                             2
a  Local Time Step      1.1452e-05                         44393


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.92862         0.77487      -0.0029513     -1.1216e-06
v  Velocity[Y]                 -15.226          31.654          6.8054          20.057
v  Velocity[Z]                 -31.422          28.556        -0.18461       -0.010308
v  ǁVelocityǁ                0.0074895          36.552          10.559          20.213
v  Pressure                    -400.44          352.57         -54.686          31.122
v  k                        1.7979e-08          58.976          4.0971          1.6835
v  omega                         1e-24      6.6151e+07          8919.2          11.892
v  turbulent_viscosity      2.9646e-14          1.4009        0.015723         0.11145
v  CourantNb                  0.032119          2053.5          44.326          1.3766
v  FourierNb                  0.010847           15749          93.626         0.68963
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14936        0.010814         0.04567


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.92497           15821          137.95          2.0662


 TIME FOR THE TIME STEP              949:        0.46866E+02

===============================================================


 INSTANT    0.950000000E+02   TIME STEP NUMBER             950
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.175562440E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32277E+02 0.14148E+02
   Friction velocity        uet   :  0.15630E-03 0.30836E+01
   Friction velocity        uk    :  0.16643E-01 0.29820E+01
   Dimensionless distance   yplus :  0.13276E+00 0.27599E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        452
   Nb of faces within the viscous sub-layer     :        991
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29415E+04    1969   0.44049E-02   0.39217E+00 
c  VelocityY    0.29415E+04    1969   0.44049E-02   0.00000E+00 
c  VelocityZ    0.29415E+04    1969   0.44049E-02   0.00000E+00 
c  Pressure     0.47145E+00    7017   0.33872E-01   0.22318E+00 
c  k            0.22504E+04    1585   0.68301E-04   0.13464E+01 
c  omega        0.24448E+08     179   0.48148E-04   0.86608E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4809e+05                             2
a  Local Time Step      1.1346e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.95653         0.79328      -0.0035395     -6.4749e-07
v  Velocity[Y]                 -15.037          32.944          6.8593          20.056
v  Velocity[Z]                 -32.607           28.75        -0.16001      -0.0097265
v  ǁVelocityǁ                0.0070016          35.846           10.63          20.212
v  Pressure                    -437.51          352.34         -53.759          31.317
v  k                        9.5171e-09          66.757          4.1168          1.6876
v  omega                         1e-24      4.1068e+07          8356.2          11.852
v  turbulent_viscosity      5.6182e-15          1.3967        0.015748          0.1117
v  CourantNb                  0.036002          2571.2          44.209          1.3764
v  FourierNb                  0.010848           15713          92.665         0.69075
v  total_pressure           1.0089e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14906        0.010814          0.0457


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15760          136.87          2.0671


 TIME FOR THE TIME STEP              950:        0.46688E+02

===============================================================


 INSTANT    0.951000000E+02   TIME STEP NUMBER             951
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.441234418E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30864E+02 0.14116E+02
   Friction velocity        uet   :  0.18137E-02 0.32331E+01
   Friction velocity        uk    :  0.19654E-01 0.30561E+01
   Dimensionless distance   yplus :  0.10140E+00 0.27670E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        421
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1869   0.46903E-02   0.39108E+00 
c  VelocityY    0.29413E+04    1869   0.46903E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1869   0.46903E-02   0.00000E+00 
c  Pressure     0.43824E+00    7021   0.36678E-01   0.20669E+00 
c  k            0.22693E+04    1485   0.70082E-04   0.14065E+01 
c  omega        0.15300E+08     226   0.25412E-03   0.12842E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7074e+05                             2
a  Local Time Step      1.0924e-05                         44405


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.96675         0.76645      -0.0040455     -3.0423e-06
v  Velocity[Y]                 -21.019          30.288          6.8972          20.055
v  Velocity[Z]                 -32.457          28.463       -0.093251      -0.0090116
v  ǁVelocityǁ                 0.014026          33.982          10.679          20.211
v  Pressure                    -450.35          350.97         -53.822          31.341
v  k                        3.3901e-08          64.363          4.1213          1.6918
v  omega                         1e-24      1.8431e+08          9451.6          11.951
v  turbulent_viscosity      3.2999e-16          1.3946        0.015771         0.11198
v  CourantNb                  0.027137          2787.7           44.27          1.3764
v  FourierNb                  0.010851           15691          92.907          0.6921
v  total_pressure           1.0087e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14923        0.010814        0.045699


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15732          137.18          2.0685


 TIME FOR THE TIME STEP              951:        0.45079E+02

===============================================================


 INSTANT    0.952000000E+02   TIME STEP NUMBER             952
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.354543623E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30474E+02 0.13875E+02
   Friction velocity        uet   :  0.20302E-02 0.29202E+01
   Friction velocity        uk    :  0.17763E-01 0.31567E+01
   Dimensionless distance   yplus :  0.13760E+00 0.28459E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        415
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1895   0.45045E-02   0.36197E+00 
c  VelocityY    0.29413E+04    1895   0.45045E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1895   0.45045E-02   0.00000E+00 
c  Pressure     0.43731E+00    7046   0.35549E-01   0.20715E+00 
c  k            0.22879E+04    1350   0.68973E-04   0.14539E+01 
c  omega        0.29898E+09      93   0.62608E-05   0.36682E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7925e+05                             4
a  Local Time Step      1.1516e-05                         44413


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.94948         0.75464      -0.0039713     -2.5485e-06
v  Velocity[Y]                  -23.02          30.097          6.8711          20.056
v  Velocity[Z]                 -31.983          28.669       -0.010231      -0.0079168
v  ǁVelocityǁ                 0.013879          32.813          10.662          20.213
v  Pressure                    -442.21          352.36         -54.089           31.49
v  k                        3.6258e-08          52.752          4.1105          1.6957
v  omega                         1e-24      9.2166e+07          9062.8          11.926
v  turbulent_viscosity      2.1249e-15           1.392        0.015765         0.11228
v  CourantNb                  0.044403          2500.4          44.464          1.3766
v  FourierNb                  0.010854           15526          93.557         0.69352
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14852        0.010813        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15569          138.02          2.0702


 TIME FOR THE TIME STEP              952:        0.44876E+02

===============================================================


 INSTANT    0.953000000E+02   TIME STEP NUMBER             953
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.329763951E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31028E+02 0.14409E+02
   Friction velocity        uet   :  0.21523E-02 0.27830E+01
   Friction velocity        uk    :  0.12802E-01 0.28114E+01
   Dimensionless distance   yplus :  0.11670E+00 0.28536E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        403
   Nb of faces within the viscous sub-layer     :       1016
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1941   0.44569E-02   0.33474E+00 
c  VelocityY    0.29413E+04    1941   0.44569E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1941   0.44569E-02   0.00000E+00 
c  Pressure     0.43268E+00    7053   0.32413E-01   0.20503E+00 
c  k            0.23011E+04    1291   0.77268E-04   0.14373E+01 
c  omega        0.76246E+08     119   0.12596E-04   0.11780E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1473e+05                             1
a  Local Time Step      1.1325e-05                         44409


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.90558         0.73981      -0.0031371     -5.3203e-07
v  Velocity[Y]                 -33.541          29.912          6.7841          20.056
v  Velocity[Z]                 -29.543          28.547         0.05694      -0.0066548
v  ǁVelocityǁ                 0.011546          33.662          10.652          20.212
v  Pressure                    -419.25           353.3         -54.564          31.284
v  k                        1.0014e-09          68.101           4.103          1.6995
v  omega                         1e-24      4.6127e+07          8668.5          11.918
v  turbulent_viscosity      6.5293e-15           1.389        0.015729          0.1126
v  CourantNb                  0.058346          2030.9          44.451          1.3768
v  FourierNb                  0.010858           15366          94.183         0.69514
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14763        0.010813        0.045649


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.93733           15416          138.63           2.072


 TIME FOR THE TIME STEP              953:        0.45004E+02

===============================================================


 INSTANT    0.954000000E+02   TIME STEP NUMBER             954
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.476877233E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31507E+02 0.23148E+02
   Friction velocity        uet   :  0.27701E-03 0.29960E+01
   Friction velocity        uk    :  0.28641E-01 0.28426E+01
   Dimensionless distance   yplus :  0.15952E+00 0.28294E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        383
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1837   0.44874E-02   0.32405E+00 
c  VelocityY    0.29413E+04    1837   0.44874E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1837   0.44874E-02   0.00000E+00 
c  Pressure     0.44118E+00    7059   0.32807E-01   0.20953E+00 
c  k            0.23052E+04    1421   0.99083E-04   0.13155E+01 
c  omega        0.22001E+08     309   0.23403E-04   0.48612E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -17746                             1
a  Local Time Step      1.1383e-05                         44406


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.85093         0.76396      -0.0018411      1.9288e-06
v  Velocity[Y]                 -29.482          29.932          6.7118          20.055
v  Velocity[Z]                 -28.741          28.779         0.10104      -0.0055562
v  ǁVelocityǁ                 0.014256           38.25          10.665          20.212
v  Pressure                    -410.13          353.48         -55.324          31.445
v  k                        3.9606e-07          92.458          4.1159          1.7031
v  omega                         1e-24      2.3131e+07          8395.8          11.914
v  turbulent_viscosity      1.8034e-16          1.3872        0.015655         0.11294
v  CourantNb                  0.083403          2045.7          44.495          1.3771
v  FourierNb                  0.010861           15171          94.202         0.69677
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14822        0.010812        0.045646


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15229           138.7          2.0738


 TIME FOR THE TIME STEP              954:        0.45675E+02

===============================================================


 INSTANT    0.955000000E+02   TIME STEP NUMBER             955
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.377315661E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.53883E+02 0.14398E+02
   Friction velocity        uet   :  0.12247E-02 0.32725E+01
   Friction velocity        uk    :  0.31249E-01 0.42024E+01
   Dimensionless distance   yplus :  0.15584E+00 0.31680E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        402
   Nb of faces within the viscous sub-layer     :       1033
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1756   0.45860E-02   0.32480E+00 
c  VelocityY    0.29413E+04    1756   0.45860E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1756   0.45860E-02   0.00000E+00 
c  Pressure     0.43048E+00    6975   0.36555E-01   0.20410E+00 
c  k            0.23022E+04    1459   0.10035E-03   0.11513E+01 
c  omega        0.11471E+08     502   0.32512E-04   0.28957E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5448e+05                             1
a  Local Time Step      1.0997e-05                         44433


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.78755         0.77088     -4.2172e-05      2.0097e-06
v  Velocity[Y]                 -33.679          30.199          6.7071          20.056
v  Velocity[Z]                 -29.025          28.707          0.1316       -0.003891
v  ǁVelocityǁ                 0.014011          34.634          10.666          20.213
v  Pressure                    -410.55             353         -56.362          31.825
v  k                        4.5011e-09          66.333           4.101          1.7066
v  omega                         1e-24      1.1752e+07          8227.8          11.907
v  turbulent_viscosity      7.1362e-14          1.3834        0.015574         0.11328
v  CourantNb                 0.0062699          2051.4          44.752          1.3775
v  FourierNb                  0.010864           15020          94.075         0.69837
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14785        0.010812        0.045618


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15087          138.83          2.0758


 TIME FOR THE TIME STEP              955:        0.45001E+02

===============================================================


 INSTANT    0.956000000E+02   TIME STEP NUMBER             956
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.210019420E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32327E+02 0.14914E+02
   Friction velocity        uet   :  0.24711E-02 0.32495E+01
   Friction velocity        uk    :  0.20320E-01 0.32138E+01
   Dimensionless distance   yplus :  0.11063E+00 0.30164E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        423
   Nb of faces within the viscous sub-layer     :       1052
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1623   0.44985E-02   0.32287E+00 
c  VelocityY    0.29414E+04    1623   0.44985E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1623   0.44985E-02   0.00000E+00 
c  Pressure     0.39974E+00    7089   0.38047E-01   0.18923E+00 
c  k            0.22965E+04    1434   0.75156E-04   0.10275E+01 
c  omega        0.10501E+08     384   0.35636E-04   0.14420E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -68306                             2
a  Local Time Step       1.148e-05                         44450


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.75914         0.79617       0.0022748      2.6378e-06
v  Velocity[Y]                 -18.771          30.753          6.7256          20.056
v  Velocity[Z]                 -28.842          29.054         0.13604       -0.002496
v  ǁVelocityǁ                0.0097442           33.55           10.64          20.214
v  Pressure                    -410.24          351.78          -57.07          32.199
v  k                        9.8921e-09          47.023          4.0766          1.7099
v  omega                         1e-24      1.1724e+07          8118.9            11.9
v  turbulent_viscosity      1.9757e-15          1.3763         0.01551         0.11362
v  CourantNb                   0.04164          3151.1          45.245          1.3778
v  FourierNb                  0.010866           14948          92.883         0.69973
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14867        0.010812        0.045611


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15022          138.13          2.0775


 TIME FOR THE TIME STEP              956:        0.43485E+02

===============================================================


 INSTANT    0.957000000E+02   TIME STEP NUMBER             957
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.386979873E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30947E+02 0.14206E+02
   Friction velocity        uet   :  0.58122E-03 0.28352E+01
   Friction velocity        uk    :  0.26132E-01 0.28700E+01
   Dimensionless distance   yplus :  0.15855E+00 0.27572E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :       1014
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29414E+04    1757   0.46759E-02   0.33862E+00 
c  VelocityY    0.29414E+04    1757   0.46759E-02   0.00000E+00 
c  VelocityZ    0.29414E+04    1757   0.46759E-02   0.00000E+00 
c  Pressure     0.43364E+00    7038   0.34259E-01   0.20475E+00 
c  k            0.22900E+04    1346   0.60967E-04   0.90517E+00 
c  omega        0.10164E+08     274   0.23530E-03   0.24076E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2263e+05                             3
a  Local Time Step      1.1479e-05                         44441


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.69184         0.91695       0.0048205      3.6618e-06
v  Velocity[Y]                 -17.584           33.01          6.7455          20.057
v  Velocity[Z]                 -28.833          28.829         0.10847      -0.0012208
v  ǁVelocityǁ                0.0093777          33.987          10.607          20.214
v  Pressure                    -408.98          350.26         -56.951          32.395
v  k                        1.3392e-10          52.331          4.0865           1.713
v  omega                         1e-24      5.5557e+07          9202.2          11.933
v  turbulent_viscosity      5.5234e-15          1.3676        0.015464         0.11396
v  CourantNb                  0.040635          2423.2          45.207          1.3779
v  FourierNb                  0.010868           14750           92.94          0.7014
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14932        0.010811        0.045644


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14830          138.15          2.0793


 TIME FOR THE TIME STEP              957:        0.44012E+02

===============================================================


 INSTANT    0.958000000E+02   TIME STEP NUMBER             958
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.533959776E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32147E+02 0.13961E+02
   Friction velocity        uet   :  0.77783E-03 0.29721E+01
   Friction velocity        uk    :  0.17583E-01 0.28877E+01
   Dimensionless distance   yplus :  0.12120E+00 0.29084E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        525
   Nb of faces within the viscous sub-layer     :       1025
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29413E+04    1909   0.45983E-02   0.35976E+00 
c  VelocityY    0.29413E+04    1909   0.45983E-02   0.00000E+00 
c  VelocityZ    0.29413E+04    1909   0.45983E-02   0.00000E+00 
c  Pressure     0.44929E+00    7038   0.33238E-01   0.21332E+00 
c  k            0.22835E+04    1097   0.64057E-04   0.97436E+00 
c  omega        0.24891E+08     331   0.45711E-04   0.93426E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -50404                             2
a  Local Time Step       1.142e-05                         44453


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.65031          1.1534        0.006963      3.5848e-06
v  Velocity[Y]                 -16.151           34.25          6.7611          20.056
v  Velocity[Z]                 -29.331          29.155        0.059722      0.00024572
v  ǁVelocityǁ                0.0088787          34.431          10.572          20.214
v  Pressure                    -405.11          350.33         -56.708          32.105
v  k                        1.1655e-09          52.617          4.0674          1.7157
v  omega                         1e-24      2.8872e+07          8716.8          11.901
v  turbulent_viscosity      1.8296e-16          1.3592         0.01544          0.1143
v  CourantNb                  0.029972          2029.4          44.873          1.3778
v  FourierNb                  0.010869           14736          94.083         0.70344
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14815        0.010812        0.045672


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.90512           14779          138.96          2.0812


 TIME FOR THE TIME STEP              958:        0.45775E+02

===============================================================


 INSTANT    0.959000000E+02   TIME STEP NUMBER             959
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.231843506E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31651E+02 0.16332E+02
   Friction velocity        uet   :  0.11698E-02 0.29550E+01
   Friction velocity        uk    :  0.12298E-01 0.30513E+01
   Dimensionless distance   yplus :  0.87966E-01 0.31492E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        482
   Nb of faces within the viscous sub-layer     :       1043
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1865   0.46004E-02   0.38986E+00 
c  VelocityY    0.29411E+04    1865   0.46004E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1865   0.46004E-02   0.00000E+00 
c  Pressure     0.42493E+00    6927   0.31639E-01   0.19995E+00 
c  k            0.22750E+04    1176   0.63156E-04   0.98360E+00 
c  omega        0.12490E+08     376   0.46295E-04   0.36500E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -3.7976e+05                             2
a  Local Time Step      1.0868e-05                         44453


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.62839          1.3579       0.0087597      3.6372e-06
v  Velocity[Y]                 -16.019          34.354          6.7442          20.055
v  Velocity[Z]                 -29.376          28.941       -0.002955        0.001396
v  ǁVelocityǁ                0.0086578          34.922          10.556          20.213
v  Pressure                    -389.83          349.61         -56.552          31.644
v  k                         5.275e-09          43.535          4.0282          1.7181
v  omega                         1e-24      1.6559e+07          8520.7          11.901
v  turbulent_viscosity      1.3273e-15          1.3491        0.015407         0.11462
v  CourantNb                   0.02836          2015.3          44.647          1.3779
v  FourierNb                   0.01087           14759           94.61         0.70546
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14858        0.010813        0.045683


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14811          139.26          2.0833


 TIME FOR THE TIME STEP              959:        0.44662E+02

===============================================================


 INSTANT    0.960000000E+02   TIME STEP NUMBER             960
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.639110512E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31637E+02 0.23211E+02
   Friction velocity        uet   :  0.19158E-02 0.28104E+01
   Friction velocity        uk    :  0.13903E-01 0.30119E+01
   Dimensionless distance   yplus :  0.14983E+00 0.37856E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        542
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29411E+04    1779   0.45243E-02   0.40265E+00 
c  VelocityY    0.29411E+04    1779   0.45243E-02   0.00000E+00 
c  VelocityZ    0.29411E+04    1779   0.45243E-02   0.00000E+00 
c  Pressure     0.45957E+00    6999   0.30847E-01   0.21723E+00 
c  k            0.22652E+04    1354   0.55882E-04   0.96608E+00 
c  omega        0.10567E+08     316   0.39020E-04   0.16181E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0998e+05                             1
a  Local Time Step      1.1839e-05                         44427


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.61642          1.5135       0.0099279      3.5004e-08
v  Velocity[Y]                 -18.306          33.176          6.7026          20.056
v  Velocity[Z]                 -28.712          29.161       -0.060604       0.0022547
v  ǁVelocityǁ                0.0065414          33.184          10.539          20.214
v  Pressure                    -378.43          348.59         -56.165          31.254
v  k                        1.6152e-08          35.914          4.0148            1.72
v  omega                         1e-24      1.3229e+07          8292.5          11.886
v  turbulent_viscosity      1.4943e-14          1.3401        0.015371         0.11493
v  CourantNb                  0.023563          2009.6          44.499          1.3781
v  FourierNb                   0.01087           14740          93.897         0.70691
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010814        0.045657


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14802           138.4           2.085


 TIME FOR THE TIME STEP              960:        0.46265E+02

===============================================================


 INSTANT    0.961000000E+02   TIME STEP NUMBER             961
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.868969777E-18
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30095E+02 0.21081E+02
   Friction velocity        uet   :  0.25221E-02 0.26404E+01
   Friction velocity        uk    :  0.17208E-01 0.31758E+01
   Dimensionless distance   yplus :  0.79192E-01 0.28333E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        529
   Nb of faces within the viscous sub-layer     :       1036
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1691   0.44253E-02   0.42091E+00 
c  VelocityY    0.29408E+04    1691   0.44253E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1691   0.44253E-02   0.00000E+00 
c  Pressure     0.40549E+00    7006   0.28629E-01   0.19101E+00 
c  k            0.22548E+04    1389   0.58348E-04   0.10675E+01 
c  omega        0.10283E+08     237   0.50689E-04   0.15243E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.1321e+05                             3
a  Local Time Step      1.1545e-05                         44453


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.58541          1.6445        0.009263      -4.345e-06
v  Velocity[Y]                 -15.785          30.496          6.6844          20.056
v  Velocity[Z]                 -30.572          29.116        -0.10651       0.0030073
v  ǁVelocityǁ                 0.013732          36.028          10.536          20.214
v  Pressure                    -359.02          348.36         -54.447          31.263
v  k                        1.3363e-07          46.133          4.0261          1.7216
v  omega                         1e-24      1.4898e+07          8243.8          11.899
v  turbulent_viscosity       1.547e-14          1.3306        0.015363         0.11521
v  CourantNb                  0.029403          2017.3          44.443          1.3783
v  FourierNb                  0.010869           14655          93.069         0.70876
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010817        0.045693


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14727          137.51          2.0871


 TIME FOR THE TIME STEP              961:        0.43960E+02

===============================================================


 INSTANT    0.962000000E+02   TIME STEP NUMBER             962
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.237577323E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31157E+02 0.19711E+02
   Friction velocity        uet   :  0.73736E-03 0.29827E+01
   Friction velocity        uk    :  0.21543E-01 0.32634E+01
   Dimensionless distance   yplus :  0.22183E+00 0.27178E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        520
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29408E+04    1721   0.45555E-02   0.43210E+00 
c  VelocityY    0.29408E+04    1721   0.45555E-02   0.00000E+00 
c  VelocityZ    0.29408E+04    1721   0.45555E-02   0.00000E+00 
c  Pressure     0.41659E+00    7109   0.30361E-01   0.19586E+00 
c  k            0.22457E+04    1384   0.62268E-04   0.12256E+01 
c  omega        0.10321E+08     250   0.62836E-04   0.12486E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.5397e+05                             2
a  Local Time Step      1.2103e-05                         44491


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.58262          1.7316       0.0070769     -2.5708e-06
v  Velocity[Y]                 -15.093          31.674          6.6898          20.056
v  Velocity[Z]                 -32.131          29.256        -0.14898       0.0038785
v  ǁVelocityǁ                 0.013115          37.233          10.555          20.214
v  Pressure                    -386.05           347.1         -52.968          31.374
v  k                        1.8134e-08          57.076          4.0568          1.7228
v  omega                         1e-24      1.5914e+07          8128.8          11.876
v  turbulent_viscosity      3.4095e-14          1.3209        0.015395         0.11546
v  CourantNb                  0.011597          2013.3          44.376          1.3782
v  FourierNb                  0.010867           14522          91.887         0.71084
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14833        0.010818        0.045663


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.61606           14602          136.26           2.089


 TIME FOR THE TIME STEP              962:        0.43938E+02

===============================================================


 INSTANT    0.963000000E+02   TIME STEP NUMBER             963
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.173113848E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31458E+02 0.16125E+02
   Friction velocity        uet   :  0.21537E-02 0.31415E+01
   Friction velocity        uk    :  0.18055E-01 0.34336E+01
   Dimensionless distance   yplus :  0.13796E+00 0.27300E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :       1022
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29407E+04    1809   0.45606E-02   0.45014E+00 
c  VelocityY    0.29407E+04    1809   0.45606E-02   0.00000E+00 
c  VelocityZ    0.29407E+04    1809   0.45606E-02   0.00000E+00 
c  Pressure     0.42644E+00    7146   0.34107E-01   0.20068E+00 
c  k            0.22396E+04    1288   0.70725E-04   0.13812E+01 
c  omega        0.15639E+08     330   0.22915E-04   0.64113E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.7464e+05                             2
a  Local Time Step      1.2072e-05                         44505


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.72461          1.6106       0.0042507     -2.5921e-06
v  Velocity[Y]                 -15.233          33.223          6.7222          20.056
v  Velocity[Z]                 -33.622          29.057        -0.15386       0.0047842
v  ǁVelocityǁ                0.0060551          36.241          10.612          20.215
v  Pressure                     -435.9          345.21         -51.937           31.47
v  k                        6.5401e-09          67.407          4.0826          1.7235
v  omega                         1e-24       1.169e+07          8047.9          11.859
v  turbulent_viscosity       8.809e-14          1.3118        0.015454         0.11568
v  CourantNb                  0.022323            2450          44.188          1.3779
v  FourierNb                  0.010865           14574          92.173         0.71325
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14821        0.010821        0.045649


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40021           14614          136.36          2.0911


 TIME FOR THE TIME STEP              963:        0.45682E+02

===============================================================


 INSTANT    0.964000000E+02   TIME STEP NUMBER             964
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.524793229E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31124E+02 0.14679E+02
   Friction velocity        uet   :  0.12942E-02 0.32404E+01
   Friction velocity        uk    :  0.15399E-01 0.30944E+01
   Dimensionless distance   yplus :  0.78777E-01 0.27843E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        437
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29406E+04    1862   0.45985E-02   0.46740E+00 
c  VelocityY    0.29406E+04    1862   0.45985E-02   0.00000E+00 
c  VelocityZ    0.29406E+04    1862   0.45985E-02   0.00000E+00 
c  Pressure     0.42949E+00    7197   0.37437E-01   0.20214E+00 
c  k            0.22384E+04    1148   0.74987E-04   0.14698E+01 
c  omega        0.40691E+20       2   0.77368E-15   0.15467E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -5438.8                             1
a  Local Time Step      1.1213e-05                         44499


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                -0.93857          1.3161       0.0012551      -3.978e-07
v  Velocity[Y]                 -19.337          30.309          6.7625          20.056
v  Velocity[Z]                  -33.41          28.965        -0.11312       0.0053273
v  ǁVelocityǁ                0.0087374          35.227          10.659          20.215
v  Pressure                    -455.43          344.78         -51.589          31.521
v  k                        1.8369e-09          68.101          4.0867          1.7236
v  omega                         1e-24      7.3574e+07          8313.1          11.853
v  turbulent_viscosity      6.4253e-14          1.3025        0.015518         0.11586
v  CourantNb                   0.02888          2823.5           44.13          1.3776
v  FourierNb                  0.010862           14603          91.949         0.71539
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14772        0.010822        0.045633


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.40909           14645          136.08           2.093


 TIME FOR THE TIME STEP              964:        0.45290E+02

===============================================================


 INSTANT    0.965000000E+02   TIME STEP NUMBER             965
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.210261933E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30238E+02 0.15808E+02
   Friction velocity        uet   :  0.52579E-03 0.30152E+01
   Friction velocity        uk    :  0.19856E-01 0.31427E+01
   Dimensionless distance   yplus :  0.15534E+00 0.27848E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        404
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29404E+04    1843   0.46031E-02   0.45337E+00 
c  VelocityY    0.29404E+04    1843   0.46031E-02   0.00000E+00 
c  VelocityZ    0.29404E+04    1843   0.46031E-02   0.00000E+00 
c  Pressure     0.46140E+00    7079   0.36450E-01   0.21756E+00 
c  k            0.22388E+04    1299   0.78402E-04   0.16293E+01 
c  omega        0.30840E+08     228   0.42383E-04   0.60546E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1357e-05                         44518


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.0794          1.1907      -0.0013161     -2.0142e-06
v  Velocity[Y]                 -24.678          30.118          6.7713          20.056
v  Velocity[Z]                 -33.083           28.78       -0.048733       0.0058355
v  ǁVelocityǁ                  0.02177          34.247           10.67          20.214
v  Pressure                     -451.9          344.59         -51.994          31.392
v  k                        6.2932e-10          56.558          4.0687          1.7231
v  omega                         1e-24      3.7515e+07          8263.4          11.934
v  turbulent_viscosity      1.2455e-15          1.2925        0.015568           0.116
v  CourantNb                   0.05245          2685.2          44.191          1.3776
v  FourierNb                  0.010858           14752          91.989         0.71703
v  total_pressure           1.0087e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14778        0.010824        0.045656


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.52973           14802          136.18          2.0946


 TIME FOR THE TIME STEP              965:        0.44853E+02

===============================================================


 INSTANT    0.966000000E+02   TIME STEP NUMBER             966
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.791492070E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31183E+02 0.14414E+02
   Friction velocity        uet   :  0.85464E-03 0.29071E+01
   Friction velocity        uk    :  0.13833E-01 0.28194E+01
   Dimensionless distance   yplus :  0.12444E+00 0.27778E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        413
   Nb of faces within the viscous sub-layer     :       1037
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29403E+04    1829   0.45500E-02   0.41714E+00 
c  VelocityY    0.29403E+04    1829   0.45500E-02   0.00000E+00 
c  VelocityZ    0.29403E+04    1829   0.45500E-02   0.00000E+00 
c  Pressure     0.43350E+00    7013   0.32549E-01   0.20542E+00 
c  k            0.22390E+04    1379   0.78923E-04   0.15668E+01 
c  omega        0.12078E+08     238   0.88421E-04   0.64067E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1194e-05                         44533


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.2937         0.99734       -0.001938     -8.8391e-07
v  Velocity[Y]                 -30.694           29.99          6.7171          20.056
v  Velocity[Z]                 -30.606          28.749        0.011722       0.0060785
v  ǁVelocityǁ                 0.019985          33.241          10.654          20.215
v  Pressure                    -431.18          344.27         -52.643          31.351
v  k                        1.9477e-10          53.646          4.0503           1.722
v  omega                         1e-24      2.3089e+07          8425.3          11.945
v  turbulent_viscosity      5.7026e-15          1.2832        0.015528         0.11611
v  CourantNb                  0.033196          2062.6          44.367          1.3776
v  FourierNb                  0.010855           14767          91.859         0.71764
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14787        0.010824        0.045644


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.78257           14826          136.23          2.0952


 TIME FOR THE TIME STEP              966:        0.45113E+02

===============================================================


 INSTANT    0.967000000E+02   TIME STEP NUMBER             967
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.433394003E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31868E+02 0.21283E+02
   Friction velocity        uet   :  0.11114E-03 0.28661E+01
   Friction velocity        uk    :  0.13228E-01 0.28637E+01
   Dimensionless distance   yplus :  0.63467E-01 0.27248E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        411
   Nb of faces within the viscous sub-layer     :       1034
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29401E+04    1764   0.45347E-02   0.39640E+00 
c  VelocityY    0.29401E+04    1764   0.45347E-02   0.00000E+00 
c  VelocityZ    0.29401E+04    1764   0.45347E-02   0.00000E+00 
c  Pressure     0.42173E+00    6993   0.30895E-01   0.19881E+00 
c  k            0.22317E+04    1435   0.94154E-04   0.14737E+01 
c  omega        0.10237E+08     335   0.57918E-04   0.33707E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4636e+05                             1
a  Local Time Step      1.1248e-05                         44526


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4291         0.91872      -0.0015216      8.9938e-07
v  Velocity[Y]                 -23.828          29.919          6.6431          20.056
v  Velocity[Z]                 -28.752          29.044        0.043148       0.0059286
v  ǁVelocityǁ                 0.006688          33.331          10.673          20.215
v  Pressure                    -411.32          343.12         -53.773          31.251
v  k                        1.3371e-08          88.749          4.0871          1.7203
v  omega                         1e-24        1.43e+07            8127          11.915
v  turbulent_viscosity      2.0094e-15           1.274        0.015505         0.11617
v  CourantNb                  0.044448          2054.5          44.342          1.3776
v  FourierNb                   0.01085           14806          92.419         0.71847
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14737        0.010824         0.04564


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.84354           14872          136.76           2.096


 TIME FOR THE TIME STEP              967:        0.45155E+02

===============================================================


 INSTANT    0.968000000E+02   TIME STEP NUMBER             968
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.687443089E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32103E+02 0.18615E+02
   Friction velocity        uet   :  0.11328E-02 0.26898E+01
   Friction velocity        uk    :  0.19725E-01 0.35091E+01
   Dimensionless distance   yplus :  0.11302E+00 0.33106E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        441
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29400E+04    1835   0.45978E-02   0.39283E+00 
c  VelocityY    0.29400E+04    1835   0.45978E-02   0.00000E+00 
c  VelocityZ    0.29400E+04    1835   0.45978E-02   0.00000E+00 
c  Pressure     0.42946E+00    7009   0.35512E-01   0.20272E+00 
c  k            0.22189E+04    1439   0.12341E-03   0.13491E+01 
c  omega        0.88126E+07     518   0.55482E-04   0.12986E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.0465e+05                             1
a  Local Time Step      1.0237e-05                         44514


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7284          1.0151     -0.00098572      5.1932e-07
v  Velocity[Y]                 -36.266           30.26          6.6473          20.056
v  Velocity[Z]                 -28.758          28.895        0.073416       0.0058526
v  ǁVelocityǁ                 0.010021           36.82          10.678          20.216
v  Pressure                    -411.78          341.78         -55.197          31.543
v  k                        5.1727e-09          92.658          4.1297          1.7184
v  omega                         1e-24      1.1785e+07            7838          11.885
v  turbulent_viscosity      2.2894e-14          1.2652        0.015477          0.1162
v  CourantNb                 0.0040242          2033.6          44.504          1.3777
v  FourierNb                  0.010846           14865          92.889         0.71913
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14763        0.010823        0.045636


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14940          137.39          2.0969


 TIME FOR THE TIME STEP              968:        0.45036E+02

===============================================================


 INSTANT    0.969000000E+02   TIME STEP NUMBER             969
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.240601032E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.38719E+02 0.13703E+02
   Friction velocity        uet   :  0.34009E-02 0.34152E+01
   Friction velocity        uk    :  0.18605E-01 0.41750E+01
   Dimensionless distance   yplus :  0.14808E+00 0.39906E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        389
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29399E+04    1861   0.45740E-02   0.39185E+00 
c  VelocityY    0.29399E+04    1861   0.45740E-02   0.00000E+00 
c  VelocityZ    0.29399E+04    1861   0.45740E-02   0.00000E+00 
c  Pressure     0.44279E+00    7033   0.38506E-01   0.20831E+00 
c  k            0.22053E+04    1409   0.11548E-03   0.12609E+01 
c  omega        0.85872E+07     423   0.65018E-04   0.20555E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0704e+05                             2
a  Local Time Step      1.1226e-05                         44482


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6795          1.0599     -0.00090767     -8.0152e-08
v  Velocity[Y]                 -22.181            30.8          6.6899          20.056
v  Velocity[Z]                 -28.771          29.134        0.091771       0.0055363
v  ǁVelocityǁ                0.0024795          33.678           10.66          20.216
v  Pressure                    -411.18          342.31         -56.426          31.774
v  k                        2.1341e-09          44.065          4.1189           1.716
v  omega                         1e-24      2.4788e+07            7857          11.877
v  turbulent_viscosity      8.3415e-15          1.2567        0.015463         0.11618
v  CourantNb                  0.063828          3110.3          44.934           1.378
v  FourierNb                  0.010842           14934          92.432         0.71926
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14881        0.010822         0.04564


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15012          137.37          2.0972


 TIME FOR THE TIME STEP              969:        0.45019E+02

===============================================================


 INSTANT    0.970000000E+02   TIME STEP NUMBER             970
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.260674300E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30668E+02 0.13512E+02
   Friction velocity        uet   :  0.37251E-03 0.26287E+01
   Friction velocity        uk    :  0.13358E-01 0.31566E+01
   Dimensionless distance   yplus :  0.75662E-01 0.28482E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        434
   Nb of faces within the viscous sub-layer     :       1041
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29397E+04    1874   0.46912E-02   0.39202E+00 
c  VelocityY    0.29397E+04    1874   0.46912E-02   0.00000E+00 
c  VelocityZ    0.29397E+04    1874   0.46912E-02   0.00000E+00 
c  Pressure     0.46126E+00    7053   0.35244E-01   0.21696E+00 
c  k            0.21930E+04    1371   0.73841E-04   0.11232E+01 
c  omega        0.91206E+07     299   0.26403E-03   0.20522E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.1306e-05                         44431


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7602         0.90286     -0.00028334     -1.2528e-06
v  Velocity[Y]                 -17.794          31.153          6.7337          20.057
v  Velocity[Z]                 -29.225          29.039         0.08392       0.0048234
v  ǁVelocityǁ                0.0058422          33.863          10.622          20.216
v  Pressure                     -410.4          344.15         -56.501          32.024
v  k                        4.2155e-08          54.575          4.1572          1.7135
v  omega                         1e-24      5.6555e+07          8754.3          11.943
v  turbulent_viscosity        2.92e-15          1.2488        0.015467         0.11612
v  CourantNb                 0.0074413          2694.3          45.045          1.3781
v  FourierNb                  0.010838           15000           92.99         0.71931
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14867        0.010823        0.045696


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15043          138.04          2.0974


 TIME FOR THE TIME STEP              970:        0.47457E+02

===============================================================


 INSTANT    0.971000000E+02   TIME STEP NUMBER             971
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.441320312E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31082E+02 0.13513E+02
   Friction velocity        uet   :  0.65469E-03 0.29104E+01
   Friction velocity        uk    :  0.15088E-01 0.27979E+01
   Dimensionless distance   yplus :  0.77811E-01 0.29021E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        501
   Nb of faces within the viscous sub-layer     :       1120
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29396E+04    1981   0.44868E-02   0.40260E+00 
c  VelocityY    0.29396E+04    1981   0.44868E-02   0.00000E+00 
c  VelocityZ    0.29396E+04    1981   0.44868E-02   0.00000E+00 
c  Pressure     0.46835E+00    7092   0.32023E-01   0.21927E+00 
c  k            0.21827E+04    1333   0.74195E-04   0.11517E+01 
c  omega        0.23865E+08     346   0.13629E-03   0.34033E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4975e+05                             2
a  Local Time Step       1.168e-05                         44321


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.8085         0.81941       0.0012905     -2.8744e-07
v  Velocity[Y]                 -16.481          33.497          6.7694          20.057
v  Velocity[Z]                 -28.785            29.3        0.058519       0.0041191
v  ǁVelocityǁ                0.0032118           33.61          10.587          20.216
v  Pressure                    -407.85          345.52         -55.889          31.921
v  k                        2.6405e-07          52.243          4.1783          1.7105
v  omega                         1e-24      7.7451e+07          9360.4          12.001
v  turbulent_viscosity      1.2644e-14           1.241        0.015501         0.11603
v  CourantNb                  0.013225          2058.1          44.882          1.3781
v  FourierNb                  0.010834           15226          95.551         0.71951
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010824        0.045725


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15278          140.43          2.0976


 TIME FOR THE TIME STEP              971:        0.47825E+02

===============================================================


 INSTANT    0.972000000E+02   TIME STEP NUMBER             972
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.169503667E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31786E+02 0.15786E+02
   Friction velocity        uet   :  0.21720E-02 0.29432E+01
   Friction velocity        uk    :  0.15146E-01 0.28655E+01
   Dimensionless distance   yplus :  0.16754E+00 0.31365E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        514
   Nb of faces within the viscous sub-layer     :       1095
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29395E+04    1777   0.44174E-02   0.42585E+00 
c  VelocityY    0.29395E+04    1777   0.44174E-02   0.00000E+00 
c  VelocityZ    0.29395E+04    1777   0.44174E-02   0.00000E+00 
c  Pressure     0.44369E+00    7055   0.29928E-01   0.20662E+00 
c  k            0.21722E+04    1342   0.75279E-04   0.11997E+01 
c  omega        0.40037E+08     310   0.54714E-04   0.19700E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -14643                             1
a  Local Time Step      1.1886e-05                         44275


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7972         0.87839       0.0033429      4.6271e-07
v  Velocity[Y]                 -15.122          33.188          6.7704          20.057
v  Velocity[Z]                 -29.038          29.137        0.013034       0.0030591
v  ǁVelocityǁ                0.0047707          33.438          10.568          20.217
v  Pressure                    -395.33           345.2         -55.696          31.553
v  k                        2.9779e-08          46.161           4.157          1.7074
v  omega                         1e-24      7.8794e+07            8984          11.965
v  turbulent_viscosity       4.057e-14          1.2334        0.015543          0.1159
v  CourantNb                  0.013026          2074.5          44.729          1.3781
v  FourierNb                  0.010831           15453          97.753         0.71978
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14799        0.010824         0.04572


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15513          142.48          2.0979


 TIME FOR THE TIME STEP              972:        0.45182E+02

===============================================================


 INSTANT    0.973000000E+02   TIME STEP NUMBER             973
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.370780070E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32043E+02 0.21153E+02
   Friction velocity        uet   :  0.27024E-03 0.28046E+01
   Friction velocity        uk    :  0.21965E-01 0.31857E+01
   Dimensionless distance   yplus :  0.14029E+00 0.40041E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        550
   Nb of faces within the viscous sub-layer     :       1065
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29393E+04    1533   0.46385E-02   0.43678E+00 
c  VelocityY    0.29393E+04    1533   0.46385E-02   0.00000E+00 
c  VelocityZ    0.29393E+04    1533   0.46385E-02   0.00000E+00 
c  Pressure     0.45993E+00    6933   0.29466E-01   0.21494E+00 
c  k            0.21616E+04    1428   0.67053E-04   0.11400E+01 
c  omega        0.28561E+08     247   0.41319E-04   0.11503E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4023e+05                             1
a  Local Time Step      1.1272e-05                         44306


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7886          1.0098       0.0052459       1.055e-07
v  Velocity[Y]                 -16.043            33.6          6.7447          20.056
v  Velocity[Z]                 -28.697          29.088        -0.02936       0.0022695
v  ǁVelocityǁ                0.0084675          33.798          10.564          20.216
v  Pressure                    -380.04          344.37         -55.707          30.977
v  k                        2.7952e-07          44.296          4.1375          1.7042
v  omega                         1e-24      4.0158e+07            8558          11.931
v  turbulent_viscosity      1.5604e-14          1.2259        0.015569         0.11574
v  CourantNb                  0.014682          2078.5          44.508          1.3783
v  FourierNb                  0.010829           15617          97.586         0.71939
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1481        0.010824        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15689          142.09          2.0977


 TIME FOR THE TIME STEP              973:        0.41836E+02

===============================================================


 INSTANT    0.974000000E+02   TIME STEP NUMBER             974
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.161984298E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31126E+02 0.20260E+02
   Friction velocity        uet   :  0.21053E-02 0.26933E+01
   Friction velocity        uk    :  0.12314E-01 0.32678E+01
   Dimensionless distance   yplus :  0.10161E+00 0.31413E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        525
   Nb of faces within the viscous sub-layer     :       1046
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29392E+04    1647   0.45056E-02   0.45349E+00 
c  VelocityY    0.29392E+04    1647   0.45056E-02   0.00000E+00 
c  VelocityZ    0.29392E+04    1647   0.45056E-02   0.00000E+00 
c  Pressure     0.44755E+00    6978   0.27836E-01   0.21061E+00 
c  k            0.21531E+04    1456   0.66483E-04   0.11934E+01 
c  omega        0.20005E+08     196   0.31665E-04   0.35397E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.6725e+05                             2
a  Local Time Step      1.1974e-05                         44386


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7745          1.1154       0.0064361       2.457e-06
v  Velocity[Y]                 -15.277          30.495          6.7428          20.057
v  Velocity[Z]                 -30.047          29.022       -0.053271       0.0012897
v  ǁVelocityǁ                0.0026557          35.225          10.565          20.216
v  Pressure                    -361.89          344.55         -54.459          31.277
v  k                        3.9704e-08          44.538          4.1279           1.701
v  omega                         1e-24      2.1584e+07          8182.5          11.894
v  turbulent_viscosity      2.3996e-14            1.22          0.0156         0.11556
v  CourantNb                  0.017168          2070.7          44.479          1.3787
v  FourierNb                  0.010827           15645          96.325         0.71834
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14805        0.010823        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15725           140.8          2.0971


 TIME FOR THE TIME STEP              974:        0.42981E+02

===============================================================


 INSTANT    0.975000000E+02   TIME STEP NUMBER             975
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.217664157E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30243E+02 0.20112E+02
   Friction velocity        uet   :  0.17584E-02 0.28521E+01
   Friction velocity        uk    :  0.13071E-01 0.30863E+01
   Dimensionless distance   yplus :  0.14627E+00 0.27814E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        494
   Nb of faces within the viscous sub-layer     :       1038
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29391E+04    1764   0.45400E-02   0.45506E+00 
c  VelocityY    0.29391E+04    1764   0.45400E-02   0.00000E+00 
c  VelocityZ    0.29391E+04    1764   0.45400E-02   0.00000E+00 
c  Pressure     0.45961E+00    7030   0.29155E-01   0.21667E+00 
c  k            0.21478E+04    1390   0.66418E-04   0.13237E+01 
c  omega        0.99903E+07     246   0.44672E-04   0.65752E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4997e+05                             2
a  Local Time Step      1.2124e-05                         44481


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6989          1.1943       0.0066734      3.4645e-06
v  Velocity[Y]                 -15.264          30.458          6.7656          20.057
v  Velocity[Z]                  -31.77          28.975       -0.063195     -0.00018282
v  ǁVelocityǁ                0.0060526           36.66          10.582          20.217
v  Pressure                    -357.46          345.87         -53.245           31.46
v  k                        1.5835e-08           52.16          4.1361          1.6979
v  omega                         1e-24      1.8002e+07          8163.6          11.922
v  turbulent_viscosity      9.5661e-15          1.2308        0.015633         0.11535
v  CourantNb                  0.045933          2053.6          44.564          1.3788
v  FourierNb                  0.010826           15793          94.962         0.71672
v  total_pressure           1.0097e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14832        0.010824        0.045679


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15838          139.53          2.0955


 TIME FOR THE TIME STEP              975:        0.45060E+02

===============================================================


 INSTANT    0.976000000E+02   TIME STEP NUMBER             976
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.354139314E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31359E+02 0.15475E+02
   Friction velocity        uet   :  0.80376E-03 0.31021E+01
   Friction velocity        uk    :  0.16493E-01 0.30364E+01
   Dimensionless distance   yplus :  0.49015E-01 0.28027E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        436
   Nb of faces within the viscous sub-layer     :       1032
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29389E+04    1816   0.44998E-02   0.45269E+00 
c  VelocityY    0.29389E+04    1816   0.44998E-02   0.00000E+00 
c  VelocityZ    0.29389E+04    1816   0.44998E-02   0.00000E+00 
c  Pressure     0.43737E+00    7069   0.33121E-01   0.20555E+00 
c  k            0.21480E+04    1079   0.74518E-04   0.14946E+01 
c  omega        0.12895E+08     227   0.11259E-02   0.59738E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3999e+05                             2
a  Local Time Step      1.1892e-05                         44528


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6576          1.2448       0.0064307       7.007e-07
v  Velocity[Y]                 -15.113          31.508          6.8054          20.056
v  Velocity[Z]                 -33.284          28.749       -0.047565      -0.0013139
v  ǁVelocityǁ                0.0046438          36.937          10.626          20.216
v  Pressure                    -415.95           348.2         -52.014          31.753
v  k                        1.1852e-09          64.045          4.1452          1.6948
v  omega                         1e-24       4.913e+08           11351          12.119
v  turbulent_viscosity      1.2514e-14           1.244        0.015685         0.11512
v  CourantNb                  0.061053          2238.1          44.486          1.3786
v  FourierNb                  0.010826           15954          94.861         0.71544
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14888        0.010821        0.045694


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16004          139.35          2.0941


 TIME FOR THE TIME STEP              976:        0.44226E+02

===============================================================


 INSTANT    0.977000000E+02   TIME STEP NUMBER             977
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.429746227E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30966E+02 0.13980E+02
   Friction velocity        uet   :  0.11418E-02 0.31616E+01
   Friction velocity        uk    :  0.24630E-01 0.28774E+01
   Dimensionless distance   yplus :  0.95935E-01 0.27981E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        469
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1851   0.44819E-02   0.45367E+00 
c  VelocityY    0.29388E+04    1851   0.44819E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1851   0.44819E-02   0.00000E+00 
c  Pressure     0.44450E+00    7043   0.37419E-01   0.20950E+00 
c  k            0.21554E+04    1337   0.78233E-04   0.15929E+01 
c  omega        0.12158E+10     108   0.59684E-05   0.16424E+10 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.2853e+05                             2
a  Local Time Step       1.206e-05                         44600


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6559          1.6388       0.0056871      4.4221e-07
v  Velocity[Y]                 -16.255          30.278          6.8522          20.057
v  Velocity[Z]                 -32.534          28.536       0.0043908      -0.0022418
v  ǁVelocityǁ                 0.014192          34.505          10.671          20.217
v  Pressure                    -442.91          349.33         -51.312          31.915
v  k                        6.2033e-08          67.463          4.1365          1.6916
v  omega                         1e-24      2.4572e+08           10025          12.006
v  turbulent_viscosity       2.481e-15           1.254        0.015737         0.11489
v  CourantNb                  0.027643          2730.6          44.431          1.3784
v  FourierNb                  0.010826           16028          94.933         0.71408
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14888        0.010819        0.045703


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           16086          139.36          2.0925


 TIME FOR THE TIME STEP              977:        0.44558E+02

===============================================================


 INSTANT    0.978000000E+02   TIME STEP NUMBER             978
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.249898675E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31910E+02 0.14531E+02
   Friction velocity        uet   :  0.16881E-02 0.30223E+01
   Friction velocity        uk    :  0.24733E-01 0.29311E+01
   Dimensionless distance   yplus :  0.14029E+00 0.27830E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :       1040
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29388E+04    1734   0.46086E-02   0.44544E+00 
c  VelocityY    0.29388E+04    1734   0.46086E-02   0.00000E+00 
c  VelocityZ    0.29388E+04    1734   0.46086E-02   0.00000E+00 
c  Pressure     0.43743E+00    7097   0.37396E-01   0.20601E+00 
c  k            0.21664E+04    1537   0.79573E-04   0.16575E+01 
c  omega        0.30580E+09      80   0.11866E-04   0.42946E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8872e+05                             3
a  Local Time Step      1.1678e-05                         44629


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6734          2.5776       0.0043426      2.9343e-06
v  Velocity[Y]                 -22.973          30.093          6.8727          20.057
v  Velocity[Z]                 -32.044           28.64        0.063908      -0.0029152
v  ǁVelocityǁ                 0.012327          33.307          10.666          20.217
v  Pressure                    -445.53          349.56         -50.991          32.025
v  k                         4.711e-09           59.74          4.0955          1.6885
v  omega                         1e-24      1.2305e+08          8992.5          11.953
v  turbulent_viscosity      4.9995e-15          1.2657        0.015765         0.11464
v  CourantNb                   0.04346          2686.3          44.511          1.3784
v  FourierNb                  0.010827           15960          95.357         0.71245
v  total_pressure           1.0088e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14854        0.010817        0.045687


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           16026          139.87          2.0909


 TIME FOR THE TIME STEP              978:        0.44988E+02

===============================================================


 INSTANT    0.979000000E+02   TIME STEP NUMBER             979
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.371281862E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30939E+02 0.13982E+02
   Friction velocity        uet   :  0.11693E-02 0.28259E+01
   Friction velocity        uk    :  0.32014E-01 0.31649E+01
   Dimensionless distance   yplus :  0.10561E+00 0.27230E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        370
   Nb of faces within the viscous sub-layer     :       1012
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1557   0.45752E-02   0.40976E+00 
c  VelocityY    0.29387E+04    1557   0.45752E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1557   0.45752E-02   0.00000E+00 
c  Pressure     0.43737E+00    7101   0.33936E-01   0.20581E+00 
c  k            0.21763E+04    1551   0.80453E-04   0.17119E+01 
c  omega        0.77627E+08     109   0.26622E-04   0.15715E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.0091e+05                             1
a  Local Time Step      1.1895e-05                         44632


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7019          3.3341       0.0030507      4.6772e-06
v  Velocity[Y]                 -28.983          29.952          6.8233          20.057
v  Velocity[Z]                 -29.622          28.638         0.11867      -0.0038698
v  ǁVelocityǁ                 0.019361           32.77          10.627          20.218
v  Pressure                    -430.28          349.45         -50.937          32.179
v  k                        4.1652e-11          54.644          4.0457          1.6853
v  omega                         1e-24      6.1941e+07          8885.4          11.939
v  turbulent_viscosity      4.3129e-16          1.2774        0.015739         0.11439
v  CourantNb                  0.036219          2129.6          44.594          1.3785
v  FourierNb                  0.010828           15671          94.746         0.71024
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14759        0.010817        0.045698


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15745          139.34          2.0887


 TIME FOR THE TIME STEP              979:        0.42616E+02

===============================================================


 INSTANT    0.980000000E+02   TIME STEP NUMBER             980
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.299424294E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30524E+02 0.20559E+02
   Friction velocity        uet   :  0.18232E-02 0.27474E+01
   Friction velocity        uk    :  0.26425E-01 0.28427E+01
   Dimensionless distance   yplus :  0.15811E+00 0.26835E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        327
   Nb of faces within the viscous sub-layer     :       1011
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1586   0.44743E-02   0.38116E+00 
c  VelocityY    0.29386E+04    1586   0.44743E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1586   0.44743E-02   0.00000E+00 
c  Pressure     0.43101E+00    7075   0.31424E-01   0.20293E+00 
c  k            0.21800E+04    1494   0.99083E-04   0.16563E+01 
c  omega        0.22328E+08     218   0.47436E-04   0.56925E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -86220                             1
a  Local Time Step      1.1821e-05                         44630


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7532          3.5194       0.0027902      3.5116e-06
v  Velocity[Y]                  -24.47          29.801          6.7371          20.057
v  Velocity[Z]                 -30.099          28.616         0.13146      -0.0047086
v  ǁVelocityǁ                0.0099172          33.068          10.618          20.218
v  Pressure                    -404.26          348.26         -51.342          32.027
v  k                        3.3225e-09          83.971          4.0529          1.6823
v  omega                         1e-24      3.1814e+07            8395          11.925
v  turbulent_viscosity      1.0844e-17          1.2865        0.015698         0.11414
v  CourantNb                  0.032863          2016.1          44.515          1.3784
v  FourierNb                  0.010831           15752          94.149         0.70814
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14798        0.010816        0.045724


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15795          138.66          2.0866


 TIME FOR THE TIME STEP              980:        0.44023E+02

===============================================================


 INSTANT    0.981000000E+02   TIME STEP NUMBER             981
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.553183553E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31325E+02 0.17880E+02
   Friction velocity        uet   :  0.10722E-02 0.26164E+01
   Friction velocity        uk    :  0.17520E-01 0.30857E+01
   Dimensionless distance   yplus :  0.18767E+00 0.30659E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        298
   Nb of faces within the viscous sub-layer     :       1018
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1760   0.43643E-02   0.36620E+00 
c  VelocityY    0.29383E+04    1760   0.43643E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1760   0.43643E-02   0.00000E+00 
c  Pressure     0.44764E+00    7062   0.34113E-01   0.21110E+00 
c  k            0.21765E+04    1375   0.11592E-03   0.15461E+01 
c  omega        0.10598E+08     482   0.45368E-04   0.24067E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8771e+05                             1
a  Local Time Step      1.1665e-05                         44612


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7806           3.148       0.0036554      3.0081e-06
v  Velocity[Y]                 -38.248          30.169          6.7056          20.056
v  Velocity[Z]                  -28.84          28.567         0.13959      -0.0054768
v  ǁVelocityǁ                0.0090465          38.685          10.617          20.217
v  Pressure                    -407.57          348.97         -52.133          32.151
v  k                        2.1257e-08          89.711          4.0829          1.6796
v  omega                         1e-24      1.7551e+07          8170.1          11.914
v  turbulent_viscosity      7.6851e-16          1.2937         0.01566         0.11388
v  CourantNb                  0.048294          2005.1          44.619          1.3784
v  FourierNb                  0.010834           15821           93.49         0.70614
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14862        0.010818         0.04578


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15862          138.11          2.0845


 TIME FOR THE TIME STEP              981:        0.45377E+02

===============================================================


 INSTANT    0.982000000E+02   TIME STEP NUMBER             982
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.445339417E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.46412E+02 0.14078E+02
   Friction velocity        uet   :  0.10662E-02 0.35029E+01
   Friction velocity        uk    :  0.19021E-01 0.38993E+01
   Dimensionless distance   yplus :  0.16747E+00 0.39072E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        357
   Nb of faces within the viscous sub-layer     :       1029
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1905   0.45786E-02   0.35441E+00 
c  VelocityY    0.29382E+04    1905   0.45786E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1905   0.45786E-02   0.00000E+00 
c  Pressure     0.41434E+00    7064   0.37197E-01   0.19284E+00 
c  k            0.21705E+04    1005   0.11773E-03   0.14652E+01 
c  omega        0.90191E+07     454   0.64156E-04   0.17394E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -74366                             1
a  Local Time Step      1.0795e-05                         44579


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.7507          3.3532       0.0051394      4.3083e-06
v  Velocity[Y]                 -27.409          30.574          6.7046          20.056
v  Velocity[Z]                 -28.961          28.787          0.1247      -0.0059518
v  ǁVelocityǁ                 0.013854          33.599          10.596          20.217
v  Pressure                    -408.82           350.2         -53.146          32.395
v  k                        1.5564e-08           42.33          4.0661          1.6771
v  omega                         1e-24      1.7388e+07          8072.3          11.888
v  turbulent_viscosity      8.1863e-15          1.2988        0.015647         0.11364
v  CourantNb                  0.034569          2979.8          44.968          1.3784
v  FourierNb                  0.010836           15783          93.208         0.70446
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01          0.1483        0.010818        0.045785


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15829          138.18          2.0829


 TIME FOR THE TIME STEP              982:        0.44987E+02

===============================================================


 INSTANT    0.983000000E+02   TIME STEP NUMBER             983
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.519954318E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30956E+02 0.13841E+02
   Friction velocity        uet   :  0.64753E-03 0.29448E+01
   Friction velocity        uk    :  0.22923E-01 0.31680E+01
   Dimensionless distance   yplus :  0.78562E-01 0.28675E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        426
   Nb of faces within the viscous sub-layer     :       1036
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1948   0.45012E-02   0.35246E+00 
c  VelocityY    0.29384E+04    1948   0.45012E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1948   0.45012E-02   0.00000E+00 
c  Pressure     0.41394E+00    7107   0.36204E-01   0.19327E+00 
c  k            0.21658E+04    1251   0.76373E-04   0.13298E+01 
c  omega        0.89141E+07     328   0.29782E-03   0.65828E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.4218e+05                             2
a  Local Time Step      1.1275e-05                         44569


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6977           4.046       0.0061325      6.2883e-06
v  Velocity[Y]                 -17.578          32.596          6.7129          20.057
v  Velocity[Z]                 -29.034          28.558        0.085486      -0.0064077
v  ǁVelocityǁ                 0.012462          33.625          10.561          20.219
v  Pressure                    -409.95           350.7         -53.675          32.726
v  k                        4.2278e-10          54.217          4.0925           1.675
v  omega                         1e-24      1.2825e+08          9011.9          11.971
v  turbulent_viscosity      8.4661e-15          1.3029        0.015651         0.11339
v  CourantNb                  0.033174          2970.2          44.955          1.3783
v  FourierNb                  0.010838           15827          92.517          0.7024
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14767        0.010817        0.045739


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.82602           15880          137.47          2.0807


 TIME FOR THE TIME STEP              983:        0.45601E+02

===============================================================


 INSTANT    0.984000000E+02   TIME STEP NUMBER             984
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.348596066E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30410E+02 0.13837E+02
   Friction velocity        uet   :  0.95557E-03 0.29856E+01
   Friction velocity        uk    :  0.14123E-01 0.27822E+01
   Dimensionless distance   yplus :  0.12731E+00 0.28458E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        518
   Nb of faces within the viscous sub-layer     :       1031
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1984   0.44722E-02   0.36355E+00 
c  VelocityY    0.29384E+04    1984   0.44722E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1984   0.44722E-02   0.00000E+00 
c  Pressure     0.42681E+00    7003   0.33619E-01   0.19985E+00 
c  k            0.21631E+04    1465   0.78612E-04   0.13389E+01 
c  omega        0.14637E+09     121   0.26284E-04   0.50027E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -86963                             1
a  Local Time Step      1.1305e-05                         44544


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6234           4.582       0.0066947      4.5433e-06
v  Velocity[Y]                 -16.963          33.922          6.7316          20.057
v  Velocity[Z]                 -28.723          29.153        0.025884      -0.0063448
v  ǁVelocityǁ                0.0077542          34.204          10.524          20.219
v  Pressure                    -409.21          350.39         -53.568          32.537
v  k                        3.6634e-10          53.394          4.1274          1.6731
v  omega                         1e-24      1.1672e+08            9442          11.969
v  turbulent_viscosity      7.1599e-16          1.3051        0.015693         0.11316
v  CourantNb                  0.045081          2025.8          44.571           1.378
v  FourierNb                   0.01084           15843          93.454         0.70126
v  total_pressure           1.0092e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14922        0.010815        0.045747


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15905          138.03          2.0793


 TIME FOR THE TIME STEP              984:        0.45711E+02

===============================================================


 INSTANT    0.985000000E+02   TIME STEP NUMBER             985
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.157503626E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31833E+02 0.15321E+02
   Friction velocity        uet   :  0.16752E-02 0.30060E+01
   Friction velocity        uk    :  0.18408E-01 0.30380E+01
   Dimensionless distance   yplus :  0.89256E-01 0.32349E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        515
   Nb of faces within the viscous sub-layer     :       1057
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    1883   0.46411E-02   0.37830E+00 
c  VelocityY    0.29384E+04    1883   0.46411E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    1883   0.46411E-02   0.00000E+00 
c  Pressure     0.40852E+00    6962   0.32126E-01   0.19237E+00 
c  k            0.21611E+04    1538   0.82766E-04   0.14714E+01 
c  omega        0.71188E+08     270   0.24683E-04   0.20757E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8335e+05                             1
a  Local Time Step      1.1574e-05                         44516


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5413          4.7326       0.0069482      3.2239e-06
v  Velocity[Y]                 -16.095          33.931          6.7464          20.057
v  Velocity[Z]                 -28.743          28.555       -0.036803      -0.0065637
v  ǁVelocityǁ                0.0091568          34.481          10.495          20.219
v  Pressure                    -399.63          348.78         -53.758          32.194
v  k                        1.5635e-08          51.159          4.1129          1.6715
v  omega                         1e-24      5.8836e+07          8862.3          11.938
v  turbulent_viscosity      6.9174e-16          1.3052        0.015748         0.11293
v  CourantNb                  0.040541          2017.3          44.127          1.3778
v  FourierNb                  0.010841           15686          95.336         0.70064
v  total_pressure           1.0093e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14944        0.010814        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15757          139.46          2.0784


 TIME FOR THE TIME STEP              985:        0.44902E+02

===============================================================


 INSTANT    0.986000000E+02   TIME STEP NUMBER             986
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.347293261E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31867E+02 0.13697E+02
   Friction velocity        uet   :  0.15722E-02 0.29173E+01
   Friction velocity        uk    :  0.12106E-01 0.29944E+01
   Dimensionless distance   yplus :  0.99889E-01 0.35812E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        487
   Nb of faces within the viscous sub-layer     :        999
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1852   0.47604E-02   0.39454E+00 
c  VelocityY    0.29383E+04    1852   0.47604E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1852   0.47604E-02   0.00000E+00 
c  Pressure     0.44324E+00    6991   0.30634E-01   0.20850E+00 
c  k            0.21579E+04    1497   0.77061E-04   0.14148E+01 
c  omega        0.29858E+08     278   0.30400E-04   0.60455E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -34113                             1
a  Local Time Step      1.0861e-05                         44549


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.4314          4.5329       0.0065853      3.4433e-06
v  Velocity[Y]                 -15.438          34.362          6.7163          20.057
v  Velocity[Z]                 -28.614          28.821        -0.10342       -0.006782
v  ǁVelocityǁ                0.0046456          34.725          10.484          20.219
v  Pressure                    -386.11          346.94         -53.697          31.903
v  k                        6.4584e-08          39.643          4.0969          1.6703
v  omega                         1e-24      3.0406e+07          8455.4          11.916
v  turbulent_viscosity      8.1967e-15          1.3081        0.015768         0.11272
v  CourantNb                  0.024047            1997          43.963          1.3777
v  FourierNb                  0.010843           15635          95.189         0.69934
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14926        0.010813        0.045726


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15676          139.15           2.077


 TIME FOR THE TIME STEP              986:        0.44878E+02

===============================================================


 INSTANT    0.987000000E+02   TIME STEP NUMBER             987
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.646893207E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31772E+02 0.19970E+02
   Friction velocity        uet   :  0.30245E-02 0.27889E+01
   Friction velocity        uk    :  0.42206E-02 0.31679E+01
   Dimensionless distance   yplus :  0.36433E-01 0.32619E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        467
   Nb of faces within the viscous sub-layer     :        992
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1908   0.44848E-02   0.40425E+00 
c  VelocityY    0.29382E+04    1908   0.44848E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1908   0.44848E-02   0.00000E+00 
c  Pressure     0.44010E+00    6999   0.28347E-01   0.20837E+00 
c  k            0.21554E+04    1374   0.74185E-04   0.14542E+01 
c  omega        0.11694E+08     229   0.56742E-04   0.28705E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.9973e+05                             3
a  Local Time Step      1.1636e-05                         44495


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -1.451          3.8134       0.0063009      1.8832e-06
v  Velocity[Y]                  -15.17          31.122          6.6964          20.057
v  Velocity[Z]                  -29.94          28.494          -0.147      -0.0065719
v  ǁVelocityǁ                 0.011396          34.573          10.492          20.219
v  Pressure                    -372.24          347.67         -53.421          31.581
v  k                        2.4925e-07          40.384          4.0836          1.6694
v  omega                         1e-24      1.7178e+07          8348.7          11.899
v  turbulent_viscosity      3.6968e-15          1.3086        0.015777         0.11252
v  CourantNb                  0.042971          2012.9          43.705          1.3778
v  FourierNb                  0.010846           15703           94.64         0.69783
v  total_pressure           1.0095e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14848        0.010814        0.045734


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15745          138.35          2.0756


 TIME FOR THE TIME STEP              987:        0.45050E+02

===============================================================


 INSTANT    0.988000000E+02   TIME STEP NUMBER             988
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.175046315E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.29963E+02 0.19909E+02
   Friction velocity        uet   :  0.22367E-02 0.28065E+01
   Friction velocity        uk    :  0.13983E-01 0.29459E+01
   Dimensionless distance   yplus :  0.15136E+00 0.28491E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        465
   Nb of faces within the viscous sub-layer     :        996
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1992   0.46242E-02   0.41288E+00 
c  VelocityY    0.29381E+04    1992   0.46242E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1992   0.46242E-02   0.00000E+00 
c  Pressure     0.45103E+00    7041   0.27713E-01   0.21318E+00 
c  k            0.21542E+04    1052   0.75665E-04   0.15794E+01 
c  omega        0.92646E+07     236   0.43478E-04   0.19170E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.627e+05                             2
a  Local Time Step      1.1189e-05                         44489


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5557          3.5452       0.0059448      1.5382e-06
v  Velocity[Y]                 -15.055          30.519          6.7089          20.057
v  Velocity[Z]                 -31.941          28.769        -0.18566      -0.0061938
v  ǁVelocityǁ                0.0048368          36.687          10.511          20.219
v  Pressure                    -351.73           350.3         -51.952          31.766
v  k                         5.808e-08          53.096          4.0927          1.6689
v  omega                         1e-24      1.2294e+07          8156.6          11.878
v  turbulent_viscosity      5.3411e-14           1.306        0.015798         0.11233
v  CourantNb                   0.03591          2039.6          43.843          1.3778
v  FourierNb                  0.010848           15773          94.453          0.6965
v  total_pressure           1.0097e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14794        0.010816         0.04576


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier           1.011           15822           138.3          2.0743


 TIME FOR THE TIME STEP              988:        0.45086E+02

===============================================================


 INSTANT    0.989000000E+02   TIME STEP NUMBER             989
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.691934597E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31367E+02 0.16931E+02
   Friction velocity        uet   :  0.30309E-02 0.31007E+01
   Friction velocity        uk    :  0.21909E-01 0.32477E+01
   Dimensionless distance   yplus :  0.11857E+00 0.28425E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        395
   Nb of faces within the viscous sub-layer     :        997
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    1924   0.45094E-02   0.41733E+00 
c  VelocityY    0.29380E+04    1924   0.45094E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    1924   0.45094E-02   0.00000E+00 
c  Pressure     0.46026E+00    7071   0.31997E-01   0.21775E+00 
c  k            0.21559E+04    1390   0.83244E-04   0.17480E+01 
c  omega        0.90099E+07     253   0.48357E-04   0.11572E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.8109e+05                             3
a  Local Time Step      1.1904e-05                         44521


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6231          3.1706       0.0058905       2.303e-06
v  Velocity[Y]                 -15.208          32.604          6.7471          20.057
v  Velocity[Z]                 -32.226           28.64        -0.19989      -0.0053853
v  ǁVelocityǁ                 0.013838          36.551          10.568          20.219
v  Pressure                    -411.08          351.47         -51.198          31.809
v  k                        1.0097e-09           64.62          4.1004          1.6686
v  omega                         1e-24      1.1705e+07          8049.1          11.853
v  turbulent_viscosity        6.02e-14          1.3003        0.015827         0.11215
v  CourantNb                  0.044681          2094.9          43.874          1.3776
v  FourierNb                   0.01085           15794          93.868          0.6953
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14834        0.010816        0.045758


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier         0.89773           15853          137.74          2.0729


 TIME FOR THE TIME STEP              989:        0.45301E+02

===============================================================


 INSTANT    0.990000000E+02   TIME STEP NUMBER             990
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.362128379E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31248E+02 0.16398E+02
   Friction velocity        uet   :  0.67228E-03 0.31953E+01
   Friction velocity        uk    :  0.23932E-01 0.29737E+01
   Dimensionless distance   yplus :  0.10405E+00 0.28211E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        414
   Nb of faces within the viscous sub-layer     :        980
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29380E+04    1884   0.45004E-02   0.43148E+00 
c  VelocityY    0.29380E+04    1884   0.45004E-02   0.00000E+00 
c  VelocityZ    0.29380E+04    1884   0.45004E-02   0.00000E+00 
c  Pressure     0.44309E+00    7048   0.37183E-01   0.20802E+00 
c  k            0.21627E+04    1565   0.87458E-04   0.18540E+01 
c  omega        0.12548E+08     250   0.18444E-03   0.16353E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.4845e+05                             1
a  Local Time Step      1.1061e-05                         44553


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.6179          2.8985       0.0062394      4.8813e-06
v  Velocity[Y]                 -15.186          32.544          6.7976          20.056
v  Velocity[Z]                 -33.376           29.02        -0.17287      -0.0048425
v  ǁVelocityǁ                 0.019438            35.5          10.625          20.218
v  Pressure                     -441.3          351.62         -50.603          31.903
v  k                        3.1741e-08          69.648          4.1015          1.6685
v  omega                         1e-24      6.8619e+07          8558.4          11.889
v  turbulent_viscosity       3.443e-15          1.2954        0.015847         0.11199
v  CourantNb                  0.050221          2690.2          43.897          1.3775
v  FourierNb                  0.010852           15732          93.369         0.69416
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14846        0.010813         0.04575


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15799          137.27          2.0717


 TIME FOR THE TIME STEP              990:        0.46281E+02

===============================================================


 INSTANT    0.991000000E+02   TIME STEP NUMBER             991
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.397867257E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31912E+02 0.17226E+02
   Friction velocity        uet   :  0.24649E-03 0.32203E+01
   Friction velocity        uk    :  0.15302E-01 0.30928E+01
   Dimensionless distance   yplus :  0.11495E+00 0.27528E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        398
   Nb of faces within the viscous sub-layer     :        983
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29381E+04    1918   0.46419E-02   0.43710E+00 
c  VelocityY    0.29381E+04    1918   0.46419E-02   0.00000E+00 
c  VelocityZ    0.29381E+04    1918   0.46419E-02   0.00000E+00 
c  Pressure     0.44334E+00    7146   0.39671E-01   0.20869E+00 
c  k            0.21732E+04    1577   0.89920E-04   0.18953E+01 
c  omega        0.26628E+08     199   0.41336E-04   0.55441E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                    -53884                             1
a  Local Time Step      1.1527e-05                         44587


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.5954           2.749       0.0070176      5.6211e-06
v  Velocity[Y]                 -22.489          30.255          6.8266          20.056
v  Velocity[Z]                 -33.238          28.745        -0.10658      -0.0040502
v  ǁVelocityǁ                 0.013613          34.517          10.645          20.218
v  Pressure                    -449.43          350.38         -50.748           31.95
v  k                        2.4396e-09          64.275          4.0857          1.6684
v  omega                         1e-24      3.5055e+07          8183.7          11.864
v  turbulent_viscosity      5.8051e-14          1.2913        0.015853         0.11185
v  CourantNb                  0.024371          2837.4          43.955          1.3774
v  FourierNb                  0.010854           15536          93.394         0.69303
v  total_pressure           1.0088e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14882        0.010813        0.045737


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15611          137.35          2.0705


 TIME FOR THE TIME STEP              991:        0.46895E+02

===============================================================


 INSTANT    0.992000000E+02   TIME STEP NUMBER             992
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.207746576E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31286E+02 0.15282E+02
   Friction velocity        uet   :  0.76447E-03 0.29304E+01
   Friction velocity        uk    :  0.28717E-01 0.30621E+01
   Dimensionless distance   yplus :  0.11661E+00 0.27231E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        379
   Nb of faces within the viscous sub-layer     :        988
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29382E+04    1906   0.44345E-02   0.41447E+00 
c  VelocityY    0.29382E+04    1906   0.44345E-02   0.00000E+00 
c  VelocityZ    0.29382E+04    1906   0.44345E-02   0.00000E+00 
c  Pressure     0.45197E+00    7093   0.37111E-01   0.21276E+00 
c  k            0.21825E+04    1493   0.89552E-04   0.19240E+01 
c  omega        0.11212E+08     262   0.79548E-04   0.48417E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.3801e+05                             1
a  Local Time Step      1.0548e-05                         44623


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.0243          2.7697       0.0067407      3.4886e-06
v  Velocity[Y]                 -26.965          30.096          6.7958          20.057
v  Velocity[Z]                  -32.05          28.956       -0.041942      -0.0025433
v  ǁVelocityǁ                  0.01263          32.959          10.624          20.219
v  Pressure                    -437.01          348.87          -50.98          32.055
v  k                        2.3366e-07          50.076          4.0607          1.6683
v  omega                         1e-24      2.3771e+07          8208.1          11.883
v  turbulent_viscosity      4.3962e-16          1.2867        0.015837         0.11173
v  CourantNb                  0.014936          2417.4           44.12          1.3776
v  FourierNb                  0.010856           15387          93.889         0.69245
v  total_pressure           1.0089e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14876        0.010813        0.045742


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15427          138.01            2.07


 TIME FOR THE TIME STEP              992:        0.45843E+02

===============================================================


 INSTANT    0.993000000E+02   TIME STEP NUMBER             993
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.330837470E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30596E+02 0.17601E+02
   Friction velocity        uet   :  0.18780E-02 0.27671E+01
   Friction velocity        uk    :  0.27098E-01 0.31414E+01
   Dimensionless distance   yplus :  0.12755E+00 0.27747E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        405
   Nb of faces within the viscous sub-layer     :        979
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    1994   0.45345E-02   0.39765E+00 
c  VelocityY    0.29383E+04    1994   0.45345E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    1994   0.45345E-02   0.00000E+00 
c  Pressure     0.43371E+00    7099   0.33233E-01   0.20401E+00 
c  k            0.21866E+04    1313   0.10150E-03   0.18806E+01 
c  omega        0.96413E+07     254   0.53396E-04   0.38612E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                   -5966.2                             1
a  Local Time Step      1.1277e-05                         44593


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.3525          2.3646       0.0054881      1.3743e-06
v  Velocity[Y]                 -36.869          29.991          6.7096          20.056
v  Velocity[Z]                 -30.531          28.918      -0.0023256      -0.0013328
v  ǁVelocityǁ                0.0063909           37.05           10.62          20.218
v  Pressure                    -410.48          348.86          -51.58          31.912
v  k                        2.8463e-08          82.431          4.0717          1.6681
v  omega                         1e-24      1.4609e+07            8072          11.877
v  turbulent_viscosity      4.8248e-14          1.2832        0.015797         0.11162
v  CourantNb                  0.037746            2031          44.216          1.3777
v  FourierNb                  0.010858           15300          93.415         0.69195
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14901        0.010815        0.045769


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15340          137.63          2.0696


 TIME FOR THE TIME STEP              993:        0.46210E+02

===============================================================


 INSTANT    0.994000000E+02   TIME STEP NUMBER             994
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.524796733E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31259E+02 0.25193E+02
   Friction velocity        uet   :  0.86318E-03 0.31218E+01
   Friction velocity        uk    :  0.14897E-01 0.29979E+01
   Dimensionless distance   yplus :  0.12590E+00 0.30241E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        397
   Nb of faces within the viscous sub-layer     :        957
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29383E+04    2095   0.46551E-02   0.39717E+00 
c  VelocityY    0.29383E+04    2095   0.46551E-02   0.00000E+00 
c  VelocityZ    0.29383E+04    2095   0.46551E-02   0.00000E+00 
c  Pressure     0.45932E+00    7077   0.34194E-01   0.21547E+00 
c  k            0.21824E+04    1109   0.13167E-03   0.17111E+01 
c  omega        0.90515E+07     449   0.34160E-04   0.28667E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega          
a  Local Time Step      1.0625e-05                         44528


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.6323          1.7114        0.004963      1.8576e-06
v  Velocity[Y]                 -38.621          30.054          6.6546          20.056
v  Velocity[Z]                 -29.117          29.012        0.028896     -0.00017989
v  ǁVelocityǁ                 0.015965          41.279          10.625          20.218
v  Pressure                    -413.47          349.49         -53.002          31.969
v  k                        2.6875e-08          103.34          4.1096           1.668
v  omega                         1e-24      1.2276e+07          7920.2          11.866
v  turbulent_viscosity      3.5592e-14          1.2771        0.015753         0.11154
v  CourantNb                  0.045208          2067.6          44.401          1.3778
v  FourierNb                   0.01086           15276            93.4         0.69172
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14709        0.010813        0.045771


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15322           137.8          2.0696


 TIME FOR THE TIME STEP              994:        0.47182E+02

===============================================================


 INSTANT    0.995000000E+02   TIME STEP NUMBER             995
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.168598550E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.56763E+02 0.14022E+02
   Friction velocity        uet   :  0.17931E-02 0.35953E+01
   Friction velocity        uk    :  0.31965E-01 0.49399E+01
   Dimensionless distance   yplus :  0.15670E+00 0.40199E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        373
   Nb of faces within the viscous sub-layer     :        963
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29385E+04    2057   0.46860E-02   0.40107E+00 
c  VelocityY    0.29385E+04    2057   0.46860E-02   0.00000E+00 
c  VelocityZ    0.29385E+04    2057   0.46860E-02   0.00000E+00 
c  Pressure     0.44453E+00    7055   0.38683E-01   0.21149E+00 
c  k            0.21732E+04    1293   0.13083E-03   0.15584E+01 
c  omega        0.92145E+07     496   0.13286E-03   0.59645E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.1696e+05                             1
a  Local Time Step      1.1276e-05                         44509


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7737          1.4244       0.0057246      2.4591e-06
v  Velocity[Y]                 -30.776          30.491          6.6629          20.057
v  Velocity[Z]                 -28.787          28.787        0.052923       0.0013391
v  ǁVelocityǁ                0.0099379          33.584           10.62          20.219
v  Pressure                    -412.87          350.04         -54.599          32.389
v  k                        2.7463e-08          57.733          4.1034          1.6682
v  omega                         1e-24      5.3025e+07            8153          11.885
v  turbulent_viscosity      3.0977e-14           1.268        0.015719         0.11147
v  CourantNb                  0.061278          2067.1          44.666          1.3781
v  FourierNb                  0.010862           15281          93.345         0.69183
v  total_pressure           1.0091e+05      1.0168e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14826        0.010813        0.045744


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15336          138.01          2.0699


 TIME FOR THE TIME STEP              995:        0.47585E+02

===============================================================


 INSTANT    0.996000000E+02   TIME STEP NUMBER             996
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.316878003E-17
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31080E+02 0.14197E+02
   Friction velocity        uet   :  0.13746E-02 0.29796E+01
   Friction velocity        uk    :  0.18499E-01 0.31002E+01
   Dimensionless distance   yplus :  0.10908E+00 0.28233E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        408
   Nb of faces within the viscous sub-layer     :        960
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    2009   0.46822E-02   0.40794E+00 
c  VelocityY    0.29386E+04    2009   0.46822E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    2009   0.46822E-02   0.00000E+00 
c  Pressure     0.44543E+00    7010   0.38249E-01   0.21082E+00 
c  k            0.21639E+04    1434   0.84265E-04   0.14133E+01 
c  omega        0.14458E+08     329   0.25147E-03   0.40664E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega                -1.475e+05                             1
a  Local Time Step      1.1272e-05                         44481


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.7496          1.3017       0.0067618      2.7517e-06
v  Velocity[Y]                 -17.796          30.757          6.6886          20.056
v  Velocity[Z]                 -28.557          29.241        0.056397       0.0027941
v  ǁVelocityǁ                0.0072425          33.477          10.601          20.219
v  Pressure                    -412.11          349.82         -55.703          32.397
v  k                        7.3786e-10          48.186          4.1114          1.6683
v  omega                         1e-24      7.7702e+07          9604.9          11.951
v  turbulent_viscosity      1.1674e-14            1.26        0.015705         0.11142
v  CourantNb                    0.0366          3019.2           44.99          1.3782
v  FourierNb                  0.010865           15301          93.331         0.69227
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14853        0.010813        0.045728


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15365          138.32          2.0705


 TIME FOR THE TIME STEP              996:        0.46770E+02

===============================================================


 INSTANT    0.997000000E+02   TIME STEP NUMBER             997
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.174225165E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30669E+02 0.14308E+02
   Friction velocity        uet   :  0.40661E-03 0.27727E+01
   Friction velocity        uk    :  0.22002E-01 0.28457E+01
   Dimensionless distance   yplus :  0.12316E+00 0.27794E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        478
   Nb of faces within the viscous sub-layer     :        972
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    2038   0.44305E-02   0.41973E+00 
c  VelocityY    0.29386E+04    2038   0.44305E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    2038   0.44305E-02   0.00000E+00 
c  Pressure     0.44409E+00    7009   0.34222E-01   0.21040E+00 
c  k            0.21561E+04    1475   0.76644E-04   0.13413E+01 
c  omega        0.40457E+08     243   0.40621E-04   0.15358E+09 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -2.7189e+05                             2
a  Local Time Step      1.1377e-05                         44474


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                  -2.666          1.1962       0.0070214      2.0875e-06
v  Velocity[Y]                 -17.324          32.239          6.7177          20.056
v  Velocity[Z]                  -28.58          28.828        0.040357       0.0039763
v  ǁVelocityǁ                  0.01941          33.894          10.575          20.219
v  Pressure                    -410.42          348.82         -55.835          32.388
v  k                        3.5324e-09          52.705          4.1447          1.6684
v  omega                         1e-24      3.9463e+07          8921.4          11.915
v  turbulent_viscosity      1.3413e-15          1.2515        0.015703         0.11138
v  CourantNb                    0.0368          2022.5          44.866          1.3782
v  FourierNb                  0.010866           15206          94.241         0.69271
v  total_pressure           1.0091e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14777        0.010814        0.045718


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15278          139.11          2.0709


 TIME FOR THE TIME STEP              997:        0.46890E+02

===============================================================


 INSTANT    0.998000000E+02   TIME STEP NUMBER             998
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.207255380E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.32038E+02 0.14215E+02
   Friction velocity        uet   :  0.67582E-03 0.28936E+01
   Friction velocity        uk    :  0.30336E-01 0.29992E+01
   Dimensionless distance   yplus :  0.16259E+00 0.30866E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        491
   Nb of faces within the viscous sub-layer     :        982
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29387E+04    1991   0.45699E-02   0.43696E+00 
c  VelocityY    0.29387E+04    1991   0.45699E-02   0.00000E+00 
c  VelocityZ    0.29387E+04    1991   0.45699E-02   0.00000E+00 
c  Pressure     0.42266E+00    7049   0.30816E-01   0.19980E+00 
c  k            0.21494E+04    1428   0.77672E-04   0.14332E+01 
c  omega        0.16716E+08     416   0.46661E-04   0.43863E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.3398e+05                             1
a  Local Time Step      1.0724e-05                         44493


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.4668          1.1214       0.0059238       1.812e-06
v  Velocity[Y]                 -15.512          32.988          6.7407          20.056
v  Velocity[Z]                 -28.709          28.872        0.011425       0.0047624
v  ǁVelocityǁ                0.0048474          33.816          10.548          20.218
v  Pressure                    -403.44          346.79         -55.642           32.21
v  k                        1.2885e-07          53.191          4.1267          1.6685
v  omega                         1e-24      2.0997e+07          8436.8           11.88
v  turbulent_viscosity      8.5905e-15          1.2425        0.015707         0.11135
v  CourantNb                  0.056057          2005.2          44.578          1.3782
v  FourierNb                  0.010868           15010          95.886          0.6933
v  total_pressure           1.0092e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010816        0.045677


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           15089          140.46          2.0715


 TIME FOR THE TIME STEP              998:        0.46678E+02

===============================================================


 INSTANT    0.999000000E+02   TIME STEP NUMBER             999
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680        -0.123801211E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.31775E+02 0.14716E+02
   Friction velocity        uet   :  0.23462E-02 0.28333E+01
   Friction velocity        uk    :  0.11673E-01 0.31818E+01
   Dimensionless distance   yplus :  0.95927E-01 0.32634E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        456
   Nb of faces within the viscous sub-layer     :        930
   Total number of wall faces                   :       7680
------------------------------------------------------------



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29386E+04    1968   0.46418E-02   0.45500E+00 
c  VelocityY    0.29386E+04    1968   0.46418E-02   0.00000E+00 
c  VelocityZ    0.29386E+04    1968   0.46418E-02   0.00000E+00 
c  Pressure     0.42240E+00    6933   0.30754E-01   0.19863E+00 
c  k            0.21415E+04    1289   0.77440E-04   0.13891E+01 
c  omega        0.99028E+07     338   0.42566E-04   0.15940E+08 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.2829e+05                             2
a  Local Time Step      1.1569e-05                         44538


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -2.2145          1.0422       0.0038118      5.3015e-07
v  Velocity[Y]                 -15.243          32.983          6.7152          20.056
v  Velocity[Z]                 -29.231          28.873        -0.02208       0.0052754
v  ǁVelocityǁ                 0.011263          33.949          10.543          20.218
v  Pressure                    -384.15          345.43         -55.679           31.76
v  k                        6.9249e-08           41.85          4.0984          1.6686
v  omega                         1e-24      1.2995e+07          8177.6           11.85
v  turbulent_viscosity      1.3146e-14          1.2353         0.01569         0.11134
v  CourantNb                  0.010111          1996.1          44.365          1.3782
v  FourierNb                  0.010869           14919          95.949         0.69357
v  total_pressure           1.0094e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14791        0.010817        0.045654


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14960          140.31          2.0717


 TIME FOR THE TIME STEP              999:        0.45706E+02

===============================================================


 INSTANT    0.100000000E+03   TIME STEP NUMBER            1000
 ============================================================= 




   ** BOUNDARY MASS FLOW INFORMATION
      ------------------------------

---------------------------------------------------------------
Boundary type          Code    Nb faces           Mass flow
---------------------------------------------------------------
Inlet                     2         200        -0.135933244E+03
Smooth wall               5        7680         0.514006856E-16
Rough wall                6           0         0.000000000E+00
Symmetry                  4      377144        -0.546021129E-15
Free outlet               3         200         0.135933244E+03
Free inlet               13           0         0.000000000E+00
Undefined                 1           0         0.000000000E+00
---------------------------------------------------------------


   ** BOUNDARY CONDITIONS FOR SMOOTH WALLS
   ---------------------------------------
------------------------------------------------------------
                                         Minimum     Maximum
------------------------------------------------------------
   Rel velocity at the wall uiptn : -0.30328E+02 0.23981E+02
   Friction velocity        uet   :  0.17839E-02 0.27197E+01
   Friction velocity        uk    :  0.94800E-02 0.31387E+01
   Dimensionless distance   yplus :  0.85260E-01 0.37847E+02
   ------------------------------------------------------
   Nb of reversal of the velocity at the wall   :        477
   Nb of faces within the viscous sub-layer     :        890
   Total number of wall faces                   :       7680
------------------------------------------------------------




 Write final restart files
   checkpoint at iteration       1000, Physical time    0.10000E+03


   ** Writing the main restart file
      -----------------------------

 Start writing
   End writing the dimensions                           
   End writing the options                              
   End writing the main variables                       
 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                            
   End writing the mass fluxes                          
   End writing the boundary conditions                  
   End writing the wall distance                        
 End writing


 Time for restart files:    0.18649E+01



   ** INFORMATION ON CONVERGENCE
      --------------------------
---------------------------------------------------------------
   Variable    Rhs norm      N_iter  Norm. residual      derive
---------------------------------------------------------------
c  VelocityX    0.29384E+04    2044   0.46796E-02   0.46745E+00 
c  VelocityY    0.29384E+04    2044   0.46796E-02   0.00000E+00 
c  VelocityZ    0.29384E+04    2044   0.46796E-02   0.00000E+00 
c  Pressure     0.44841E+00    6974   0.29852E-01   0.21228E+00 
c  k            0.21344E+04     946   0.72112E-04   0.13825E+01 
c  omega        0.90968E+07     281   0.32498E-04   0.91185E+07 
---------------------------------------------------------------
  
  

  ** Clippings for computed fields
     -----------------------------

   field               initial min     initial max  clips to min  clips to max
-  ---------------  --------------  --------------  ------------  ------------
a  k              
a  omega               -1.5152e+05                             2
a  Local Time Step      1.1637e-05                         44554


  ** Computed fields on cells
     ------------------------

   field                       minimum         maximum        set mean    spatial mean
-  -------------------  --------------  --------------  --------------  --------------
v  Velocity[X]                 -1.9251          1.1222       0.0013958      6.0411e-07
v  Velocity[Y]                 -17.511          31.614          6.6866          20.056
v  Velocity[Z]                 -29.376          29.075       -0.033836       0.0058781
v  ǁVelocityǁ                0.0060749          33.279          10.538          20.218
v  Pressure                    -369.96           346.6         -54.947          31.704
v  k                        2.4453e-07          42.268          4.0741          1.6687
v  omega                         1e-24       1.175e+07          8011.9          11.825
v  turbulent_viscosity       1.729e-14          1.2303        0.015664         0.11133
v  CourantNb                  0.054519          2005.4          44.105          1.3783
v  FourierNb                   0.01087           14943          94.635         0.69304
v  total_pressure           1.0096e+05      1.0167e+05      1.0127e+05      1.0136e+05
v  Local Time Step                0.01         0.14947        0.010819        0.045686


  ** Computed values on cells
     ------------------------

   criterion               minimum         maximum        set mean    spatial mean
   ---------------  --------------  --------------  --------------  --------------
   Courant/Fourier          1.0109           14992          138.74          2.0714


 TIME FOR THE TIME STEP             1000:        0.47640E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.96060E-02
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          40560.477 s
  System CPU time:         4099.070 s
  Total CPU time:        312946.403 s

  Elapsed time:           44833.916 s
  CPU / elapsed time          0.996

Memory use summary:

  Total memory used:                               3.290 GiB
                             local minimum:      448.387 MiB  (rank 5)
                             local maximum:      515.105 MiB  (rank 2)
  Theoretical instrumented dynamic memory:         1.587 GiB
                             local minimum:      210.509 MiB  (rank 6)
                             local maximum:      261.473 MiB  (rank 2)
