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

 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)


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


 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 (5.99e-06 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 
---------------------------------------------------------------
  
  

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

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

 TIME FOR THE TIME STEP                3:        0.31823E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP               57:        0.40459E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP               73:        0.43065E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              135:        0.42251E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              196:        0.44966E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              219:        0.45314E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              249:        0.44473E+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:    0.66013E+00



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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              274:        0.46478E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              282:        0.42926E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              299:        0.44742E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              449:        0.45893E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 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:    0.72378E+00



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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              517:        0.44057E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              721:        0.45604E+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 
---------------------------------------------------------------
  
  

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              749:        0.48019E+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:    0.70106E+00



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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

 TIME FOR THE TIME STEP              812:        0.44749E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP              873:        0.43748E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP              955:        0.45000E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP              961:        0.43959E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP              975:        0.45059E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP              996:        0.46769E+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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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 
---------------------------------------------------------------
  
  

 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:    0.76034E+00



   ** 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 
---------------------------------------------------------------
  
  

 TIME FOR THE TIME STEP             1000:        0.47640E+02

===============================================================



===============================================================



                 FINAL STAGE OF THE CALCULATION              
                 ==============================              


 =========================================================== 




   ** TIME FOR FINAL WRITING:    0.28950E-04
      -----------------------                                



 =========================================================== 




                      END OF CALCULATION                     
                      ==================                     


===============================================================

 Destroying structures and ending computation


Calculation time summary:

  User CPU time:          39811.840 s
  System CPU time:         4901.088 s

  Elapsed time:           44833.916 s
  CPU / elapsed time          0.997

Memory use summary:

  Total memory used:                             481.570 MiB
  Theoretical instrumented dynamic memory:       242.993 MiB
